[0001] The present disclosure relates techniques for operating an oscillation blade device.
BACKGROUND
[0002] Oscillation blade devices are known. One typical example of an oscillation blade
device is a cantilever fan, typically used in electric or electronic equipment where
components in the equipment heat up during operation and need to be cooled off. Another
example of oscillation blade devices is a flexible wing structure typically used in
micro-aerial vehicles, sometimes referred to as drones. Oscillation blade devices
are typically considered to be particularly useful where space is an issue due to
small size and compactness of the equipment. In the case of cantilever fans, the oscillation
of the blade, or cantilever, causes the surrounding air to move, thereby generating
airflow which is used for cooling the component. In the case of flexible wing structures,
the oscillation of the blade acts as a flapping wing which causes the surrounding
air to move, thereby propelling the body to which the wing structure is attached,
e.g. a drone.
[0003] In some examples an oscillation blade devices may use a piezoelectric element to
oscillate a planar body, whereas in some other examples it may use an electromagnetic
element to oscillate a planar body. Other examples may also exist. The planar body
is sometimes referred to as blade or cantilever. Oscillation blade devices typically
use an alternating driving force from a driver to cause the blade to oscillate. This
driving force may be obtained by activating a driver element, for example the piezoelectric
element or the electromagnetic element in the examples above.
SUMMARY
[0004] Some embodiments feature an apparatus comprising:
- a power source configured for generating a plurality of alternating electric excitation
signals; and
- a current meter configured to measure a current value supplied by the power source;
wherein the apparatus is configured to:
- apply, by the power source, a plurality of alternating electric excitation signals
to an oscillation blade device at a corresponding plurality of excitation frequencies;
- measure, by the current meter, a plurality of current values supplied by the power
source to the oscillation blade device, each current value from the plurality of current
values corresponding to a respective excitation frequency from the plurality of excitation
frequencies, said plurality of current values comprising a peak current value corresponding
to a first excitation frequency and a trough current value corresponding to a second
excitation frequency; and
- provide said plurality of current values and said plurality of excitation frequencies
to a processor for determining a third excitation frequency.
[0005] According to some specific embodiments, said third excitation frequency is located
mid-way between the first excitation frequency and the second excitation frequency
and corresponds to a resonant oscillation frequency of a planar body comprised in
the oscillation blade device.
[0006] According to some specific embodiments, said third excitation frequency is located
mid-way between the first excitation frequency and the second excitation frequency
and corresponds to a second harmonic of a resonant oscillation frequency of a planar
body comprised in the oscillation blade device.
[0007] According to some specific embodiments the apparatus is configured to drive said
oscillation blade device at a frequency matching the third excitation frequency.
[0008] Some embodiments feature a system comprising the apparatus of any one of the preceding
paragraphs, further comprising:
- an oscillation blade device having a driver electrically coupled to the power source
and configured to generate a driving force in response to receiving an alternating
electric excitation signal from the power source, and a planar body attached to the
driver and configured to oscillate in response to the driving force generated by the
driver; and
- a processor configured to receive the plurality of current values and the plurality
of excitation frequencies and determine said third excitation frequency.
[0009] According to some specific embodiments, the processor is configured to determine
said third excitation frequency value as a frequency located at mid-way between a
first excitation frequency and the second excitation frequency. According to some
specific embodiments, the processor is configured to send a command to the power source
to cause the power source to change the frequency of the alternating electric excitation
signal to match the third excitation frequency.
[0010] Some embodiments feature a cooling assembly comprising the system as disclosed herein.
[0011] Some embodiments feature a micro-aerial vehicle comprising the system as disclosed
herein.
[0012] Some embodiments feature a method for operating an apparatus, the apparatus comprising:
- a power source configured for generating a plurality of alternating electric excitation
signals; and
- a current meter configured to measure a current value supplied by the power source;
wherein the method comprises:
- applying, by the power source, a plurality of alternating electric excitation signals
to an oscillation blade device at a corresponding plurality of excitation frequencies;
- measuring, by the current meter, a plurality of current values supplied by the power
source to the oscillation blade device, each current value from the plurality of current
values corresponding to a respective excitation frequency from the plurality of excitation
frequencies, said plurality of current values comprising a peak current value corresponding
to a first excitation frequency and a trough current value corresponding to a second
excitation frequency; and
- providing said plurality of current values and said plurality of excitation frequencies
to a processor for determining a third excitation frequency, said third excitation
frequency having a value between the first excitation frequency and the second excitation
frequency.
[0013] According to some specific embodiments the method further comprises:
- determining said third excitation frequency located at mid-way between the first excitation
frequency and the second excitation frequency, the third excitation frequency corresponding
to a resonant oscillation frequency of a planar body comprised in the oscillation
blade device.
[0014] According to some specific embodiments the method further comprises:
- determining said third excitation frequency located at mid-way between the first excitation
frequency and the second excitation frequency, the third excitation frequency corresponding
to a second harmonic of a resonant oscillation frequency of a planar body comprised
in the oscillation blade device.
[0015] According to some specific embodiments the method further comprises:
- driving said oscillation blade device at a frequency matching the third excitation
frequency.
[0016] According to some specific embodiments the method further comprises sending a command
by the processor to the power source to cause the power source to change the frequency
of the alternating electric excitation signal to match the third excitation frequency.
[0017] These and further features and advantages of the present invention are described
in more detail, for the purpose of illustration and not limitation, in the following
description as well as in the claims with the aid of the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
[0018]
Figure 1 is an exemplary schematic representation of an assembly comprising an apparatus
according to some embodiments.
Figure 2 is an exemplary schematic representation of the assembly comprising an apparatus
of figure 1 operating under faulty condition.
Figure 3 is an exemplary schematic representation of oscillation characteristics of
the blade comprised in the apparatus of figure 1 and a corresponding graphical representation
of variation of input current as a function of frequency of oscillation of the blade.
Figure 4A is an exemplary schematic representation of an oscillation blade in a heat
sink operating at a first oscillation frequency and figure 4B is a representation
of the oscillation blade of figure 4A oscillating at a second frequency according
to some embodiments.
Figure 5 is an exemplary schematic representation of oscillation characteristics of
the blade comprised in the apparatus of figure 2 oscillating with a frequency that
matches the second harmonic of the resonant frequency of said blade and a corresponding
graphical representation of variation of input current as a function of frequency
of oscillation of said blade.
Figure 6A is an exemplary schematic representation of an oscillation blade in a heat
sink operating at a first resonant frequency; figure 6B is a representation of the
oscillation blade of figure 6A oscillating at a second frequency; and figure 6C is
a representation of the oscillation blade of figure 6A oscillating at a third frequency,
according to some embodiments.
DETAILED DESCRIPTION OF EXEMPLARY EMBODIMENTS
[0019] In the following reference will be made to piezoelectric fans. However the disclosure
is not so limited and the solution proposed herein is likewise applicable to other
known types of oscillation blade such as fans using electromagnetic elements to oscillate
a planar body, or devices such as flexible wing structures useable for example in
micro-aerial vehicles.
[0020] The term planar as used herein with reference to planar body is to be understood
to refer to a generally flat three-dimensional structure, wherein one dimension of
the structure is substantially smaller (e.g. one or more orders of magnitude smaller)
than the other two dimensions of the structure.
[0021] Herein, the term harmonic is to be understood to refer to a component frequency of
oscillation which is an integer multiple of the fundamental frequency of oscillation.
Accordingly the term second harmonic of the resonant frequency is to be understood
to have a frequency which is twice the fundamental resonant frequency of oscillation
of the blade. Furthermore, the term fundamental resonant frequency will herein also
be referred to simply as resonant frequency.
[0022] Typically a piezoelectric fan, herein also referred to as piezofan, uses a piezoelectric
element to drive a planar body. The piezoelectric element comprises a body of a solid
material having the property of generating an electric signal (by accumulating electric
charge) when a mechanical stress such as a pressure is applied thereupon. Conversely,
such piezoelectric element exhibits a mechanical movement in response to an electric
excitation signal (current or voltage) applied thereto. Some examples of materials
exhibiting piezoelectric property are certain crystals or ceramics.
[0023] The piezoelectric element is physically attached, e.g. bonded, to an end of a planar
body (blade). The other end of the planar body is free and movable. When an alternating
electric voltage (or current) is applied to the piezoelectric element, the latter
exhibits an oscillating movement, causing the planar body, or blade, to oscillate
at a frequency matching the drive frequency of the alternating electric signal. If
the frequency of the alternating voltage (or current) is equal to the resonant frequency
of the blade, the latter produces an oscillating movement at the free end thereof
at said resonant frequency. The oscillation of the free end of the blade produces
an air flow in a similar manner as a conventional hand fan.
[0024] It is desirable to cause these fans to operate at the resonant frequency of the blade
because oscillation at such resonant frequency typically provides the largest displacement
amplitude of the free end (tip) of the blade, which results in the generation of the
maximum volume of airflow by the blade.
[0025] The oscillation amplitude of the blade is extremely sensitive to a number of parameters
including operating frequency, the mass and rigidity of the blade. Over the lifetime
of oscillation blade fans fouling may occur on the exterior of the blade due to dust,
dirt, blocking objects and the like. Adherence of dust and dirt to the body of the
blade can cause a change in the mass of the blade. As a result of such change in the
mass of the blade the resonant frequency of the blade may change and therefore the
deflection amplitude of the blade during oscillation may be drastically reduced. Similarly,
a change or degradation in the mechanical properties of the fan over the lifetime
can also alter the blade resonant frequency. For example, if the rigidity of the blade
changes (i.e. due to degradation of the blade material or degradation of the bonding
materials), this also alters the resonant frequency.
[0026] This reduction in the deflection of the tip considerably reduces the fan's air moving
capabilities. An oscillation blade fan hampered with this problem would likely fail
to provide an efficient cooling performance. As a result of such inefficient cooling
performance, the components to be cooled may overheat and therefore component failures
may occur. To ensure maximum air flow from the fan, it is therefore important to maintain
operation at the resonant frequency of the blade. One approach to maintain operation
at resonant frequency of the blade is to clean the blade from dust and dirt or other
objects adhered thereto. Manual cleaning, which is sometimes used for cleaning rotating
fan units, is not considered as an effective solution for cleaning piezofans (or other
oscillation blade fans) due their relatively small size. Furthermore, even if manual
cleaning were to be considered as an option, it would incur additional operating costs
and potential equipment downtime.
[0027] It is therefore desired to provide a solution for dynamically determining the resonant
frequency of an oscillation blade fan. Such determination would allow for maintaining
the blade at maximum performance even if the blade is operating under faulty condition.
Determining the resonant frequency of the oscillation blade fan would further allow
for determining the second harmonic of such resonant frequency under faulty condition.
As a consequence the blade may be made to oscillate at said second harmonic frequency
and thereby fouling adhered to the blade may be removed. Such solution would reduce
operating costs, and would allow for automatically maintaining the aerodynamic performance
of the oscillation blade fan without the need to turn the fan off.
[0028] As used herein, the term "faulty condition" is to be understood to refer to a condition
of operation of a blade in which an adverse effect causes a degradation or interruption
in the otherwise normal operation of the blade. Some examples of such faulty conditions
are adherence of dirt and/or dust on the body of the blade, blockage caused by an
external object present on the oscillation path of the blade, or degradation of the
mechanical properties of the blade over the lifetime. Figure 1 is an exemplary schematic
representation of an apparatus 1 including a power source 10, an oscillation blade
fan 11 and a current meter 12. Oscillation blade fan 11 comprises a driver 111 and
a planar body (blade) 112. The driver is, in this example, a piezoelectric element.
The power source 10 may be configured to generate alternating electric excitation
signal (voltage or current) at a port 110 thereof. The port 110 is electrically connected
to a corresponding port 113 of the piezofan 11 by electric connection path 131. The
current meter 12 is configured to measure the current supplied by the power source
10 to the driver 111 of the oscillation blade fan 11 and provide values of the measured
current corresponding to frequencies of the alternating electric excitation signal
generated by the power source to drive the driver 111 of the oscillation blade fan
11. Such measured current values may be provided to a processor as will be described
further below. The current driver may be a device which is independent from the power
source 10 as represented in the figure and coupled at any convenient point to the
electric connection path 131 or it may be integrated inside the power source (not
shown in the figure).
[0029] The connection path 131 is represented in the figure by a single line. However, this
is only done for simplicity of illustration and is not intended to represent a limitation
to a one way, or single wire, connection. The connection path 131 may be provided
in any convenient manner, for example using two wires, one for forward connection
and one for return connection between the power source 10 and the piezofan 11. In
the latter case, ports 110 and 113 may likewise each comprise a pair of contact points,
one for forward connection and another for the return connection, and each pair of
contact points may be considered to represent one port.
[0030] Under normal operation, namely in the absence of fouls or when fouls exist but their
presence does not substantially degrade the operation of the piezofan, the power source
10 may generate an alternating electric signal which is output from port 110 and is
input into the piezoelectric element 111 through port 113. The electric signal causes
the piezoelectric element to undergo mechanical stress in the form of movements which
are transferred to the blade 112 attached to the piezoelectric element 111. As a consequence,
the blade 112 is caused to oscillate at the free end 112a thereof, thereby generating
a flow of air in the vicinity of the free end 112a. The blade 112 oscillates at the
frequency of the alternating electric signal generated by the power source 10. If
the frequency of the alternating electric signal matches the resonant frequency of
the blade 112, the blade reaches its maximum deflection for the applied electric signal.
Therefore, the resonant frequency of the blade, either under normal condition (free
of foul) or under faulty condition, may be considered to be the frequency at which
maximum deflection of the tip of the blade is achieved.
[0031] In the embodiment of figure 1, the blade 112 is shown in two positions, one position
is shown by a solid line and the other position is shown by a broken line. It is assumed
that the two positions of the blade show respective maximum deflections of the tip
of the blade as the blade oscillates from one position to the other. This maximum
deflection is schematically shown in the figure by double-headed arrow A
1. The maximum deflection is achieved when the frequency of the alternating electric
signal matches the resonant frequency of the blade 112. In this mode of oscillation,
the oscillation pattern of the blade presents one node which is represented in the
figure by reference N.
[0032] The current meter 12 is configured to measure the current I being supplied by the
power source 10 to the driver 111. This measured current value is then provided, through
a connection path 141 to a processor 13 in a suitable manner and in the form of data
useable by the processor 13, as known in the art, so as to enable the processor 13
to analyze the data received and provide commands based on such analysis, as will
be described further below with reference to figure 3.
[0033] The power source is also configured to provide, through a connection path 142, to
the processor 13, information related to the frequency of the alternating electric
excitation signal. This information is provided to the processor 13 in a suitable
manner and in the form of data useable by the processor 13, as known in the art, so
as to enable the processor 13 to analyze the data received and provide commands based
on such analysis, as will be described further below with reference to figure 3.
[0034] The processor may be of any known type of programmable device comprising hardware
such as an ASIC, or a combination of hardware and software means, e.g. an ASIC and
an FPGA, or at least one microprocessor and at least one memory with software modules
located therein.
[0035] Figure 2 is an exemplary schematic representation of the apparatus 1 of figure 1
with the difference that particles such as dust and/or dirt, or the like, have been
adhered to the body of the blade as is represented in the figure by reference numerals
121 and 122.
[0036] As mentioned above, the adherence of such particles 121, 122 to the blade, changes
the mass of the blade.
[0037] It is to be noted that that in a faulty condition as described above, the power source
10 may still be applying an alternating electric signal with a frequency matching
the nominal (non-faulty) resonant frequency of the blade 122, however due to the change
in the mass of the blade, the resulting (new) resonant frequency of oscillation of
the bade changes to a different value, which is not the frequency of the alternating
current applied to the fan. As a result, the blade under faulty condition would not
perform maximum deflection, and therefore, as seen in figure 2, the amplitude of deflection
A
2 of the tip of the blade in the presence of foul is smaller than the maximum deflection
A
1 of the tip of the blade when the blade oscillates without the presence of foul, namely
A
2 < A
1. The reduction in the maximum deflection of the tip of the blade results in reduction
in the volume of the airflow toward the heat generating components (not shown) and
thus may give rise to overeating of such components.
[0038] Similar to the scenario of figure 1, in this situation the oscillation pattern of
the blade also presents one node N.
[0039] Referring now to figure 3, certain oscillation characteristics of a blade used in
an oscillation blade fan, for example a piezofan, are illustrated. In this figure,
like elements have been provided with like reference numerals as those of figures
1 and 2. For simplicity, only the blade is shown and other elements of the oscillation
blade fan, such as the driver, are not shown.
[0040] The lower part of figure 3 shows a non-limiting example of variation of input current
as a function of the frequency of the alternating electric excitation signal applied
to the fan (also herein referred to as excitation frequency).
[0041] The inventors have realized that for a fixed alternating input voltage, the oscillation
blade fan draws a current which is dependent on the oscillating frequency of the blade
which in turn is equal to the frequency of the alternating electric excitation signal
applied to the fan. As can be observed in the example of figure 3 (lower part), the
excitation frequency, shown in the abscissa is changed from lower values (e.g. 30
Hz) to higher values (e.g. 100 Hz). With the change of excitation frequency, the current
drawn (or demanded) by the oscillation blade fan from the power source 10 (figure
1) varies as illustrated in the figure.
[0042] The trend in current variation with (depending on) frequency may enable to determine
whether the fan is operating at, or out of, resonant frequency and what would be the
value of the resonant frequency of a particular blade under normal or faulty conditions.
[0043] According to the present disclosure, and as shown in figure 3, the resonant frequency
of the blade F
r (be it operating under non-faulty or under faulty condition) is located between a
first frequency value corresponding to a current peak I
p and a second frequency value corresponding to a current trough I
t in the above current variation curve and its value is determined to be the frequency
value located at mid-way between the first frequency value and the second frequency
value.
[0044] Herein the term mid-way is to be understood to comprise not only the frequency value
located at the exact mathematical middle point between the first frequency value and
the second frequency value, but also the frequency values having a deviation from
the exact middle point, such deviation being within a range of +/-0.1 Hz. For example
if the frequency value located at the exact mathematical middle point between the
first frequency value and the second frequency value is 70Hz, then the resonant frequency
of the blade Fr may be considered to comprise any value between 69.9 Hz and 70.1 Hz.
This range is believed to provide an acceptable performance for the operation of the
apparatus.
[0045] The above solution for determining the resonant frequency allows for maintaining,
or if needed adjusting, the drive frequency of the fan such that maximum displacement
of the tip of the blade is ensured thereby ensuring optimum performance.
[0046] The upper part of figure 3 shows deflection amplitudes of the blade 112 in various
operating conditions. As can be seen in the upper part of figure 3, maximum deflection
of the tip of the blade is obtained at the resonant frequency F
r of the blade and operations at frequencies higher and lower than the resonant frequency
provides poor air flow.
[0047] Therefore, by varying the frequency of the driving alternating electric signal supplied
by the power source 10 over a relatively small frequency band, a range of values for
the current drawn by the fan can be measured by the current meter 12 (figure 1), where
a measured current value corresponds to a respective drive frequency (or a respective
oscillation frequency).
[0048] Each measured current value from the above range of values is provided by the current
meter 12 to the processor 13. Likewise, the corresponding drive (excitation) frequency
value of the alternating electric excitation signal is provided by the power source
10 to the processor 13. Upon receipt of such range of current-frequency pair values
the processor is configured to store such values and generate an assessment chart
with a current peak I
p and a current trough I
t. Such assessment chart may be in any convenient form for example in the form of a
table of corresponding values or in the form of a graph similar to that of figure
3.
[0049] The processor is further configured to find the frequency located at mid-way (+/-0.1
Hz) between a first frequency value corresponding to the current peak I
p and a second frequency value corresponding to the current trough I
t of said graph. Once the resonant frequency of the blade is determined by the processor
13, the latter sends a command to the power source 10, through connection path 143,
to cause the power source to change the frequency of the alternating electric excitation
signal to match the newly determined resonant frequency of the blade. In this manner,
the resonant frequency point may be determined while the fan continues to operate.
This enables dynamic adjustment of fan frequency to achieve the first mode of oscillation
(fundamental resonant frequency) for maximum airflow.
[0050] The proposed solution therefore overcomes issues that may occur in practical operating
conditions which may include adherence of dirt and/ or dust to the fan blade and degradation
of performance over time as it enables operation of the fan under the actual resonant
frequency of the blade even if it is operating under faulty condition.
[0051] Figures 4A and 4B are exemplary schematic representations of an oscillation blade
in a heat sink. In these figures, unless otherwise provided, like elements have been
given like reference numerals as those of previous figures 1-3, and for simplicity
only the blade of the oscillation blade fan is shown. However in this case, it is
assumed that the fan is installed in a heat sink 15. Under normal (non-faulty) condition
and oscillating at a frequency matching the resonant frequency of the blade 112, the
blade would perform the maximum deflection as shown by a broken lines 112 and broken
arrow A
r in figure 4A. However, as seen in figure 4A, dust and dirt 121 floating in the surrounding
air are adhered to the blade 112 thereby causing the blade to oscillate under faulty
condition with an amplitude of deflection A
f which is smaller than the maximum deflection A
r of the tip of the blade, as shown by solid lines 112 and solid arrow A
f. The adhered dust or dirt particle is shown in the figure by reference numeral 121-a.
As mentioned above, this situation is undesirable because of significant degradation
in the cooling performance of the fan.
[0052] To overcome this problem, the technique described with reference to figure 3 may
be employed to determine the new resonant frequency of the blade, namely the resonant
frequency of the blade under the faulty condition. Once this new resonant frequency
is determined, the frequency of the alternating driving signal (provided by the power
source 10 of figure 1) may be adjusted to the new determined resonant frequency thereby
causing the blade 112 to oscillate at maximum deflection again. This latter scenario
is shown in figure 4B wherein the blade, with foul 121-a adhered thereto oscillates
at the adjusted driving frequency (matching the newly determined resonant frequency
of the blade) thereby performing the maximum deflection, as shown by solid lines 112
and solid arrow A
r.
[0053] In this manner, the performance of the oscillation blade fan may be maintained, or
if needed corrected, in a dynamic fashion without the need to stop the operation of
the fan.
[0054] Figure 5 is an exemplary schematic representation of oscillation characteristics
of the blade oscillating with a frequency that matches the second harmonic of its
fundamental resonant frequency. In this figure like elements have been given like
reference numerals as those of the previous figures, and here again, for simplicity,
only the blade is shown.
[0055] The lower part of figure 5 shows a non-limiting example of variation of input current
as a function of excitation frequency applied to the fan. However, differently from
the scenario of figure 3, the fan is driven at excitation frequencies which are in
the vicinity of the second harmonic of the resonant frequency of the blade.
[0056] Similar to the scenario of figure 3, it is shown that for a fixed alternating input
voltage, the oscillation blade fan draws a current which is dependent on the oscillating
frequency of the blade. As can be observed in the example of figure 5 (lower part),
the excitation frequency applied to the fan, shown in the abscissa, may change from
lower values (e.g. 150 Hz) to higher values (e.g. 500 Hz). With the change of the
excitation frequency, the current drawn (or demanded) by the oscillation blade fan
from the power source 10 (figure 1) varies as illustrated in the figure.
[0057] Therefore the trend in current variation with (depending on) frequency would enable
to determine whether the fan is operating at, or out of, the second harmonic of the
resonant frequency and what would be the value of the second harmonic of the resonant
frequency of a particular blade under normal or faulty conditions.
[0058] As shown in figure 5, the second harmonic of the resonant frequency of the blade
F
r2 is located between a first frequency value corresponding to a current peak I
p and a second frequency value corresponding to a current trough I
t in the above current variation curve and its value is determined to be the frequency
value located at mid-way between the first frequency value and the second frequency
value (with deviations similar as those discussed with reference to figure 3).
[0059] The upper part of figure 5 shows deflection amplitudes of the blade 112 in various
operating conditions. As can be seen in the upper part of figure 5, broader deflection
of the tip of the blade is obtained at the frequency matching the second harmonic
of the resonant frequency F
r2 of the blade and operations at frequencies higher and lower than the second harmonic
of the resonant frequency provides poor blade deflection and thus poor air flow. Furthermore,
when the blade 112 is driven at a frequency which matches the second harmonic of the
resonant frequency of the blade under faulty condition, the oscillation pattern of
the blade defines a standing waveform W with at least two nodes N
1 and N
2 as shown in figure 5.
[0060] Therefore, by varying the frequency of the driving alternating electric signal supplied
by the power source 10 over a relatively small frequency band, a range of values for
the current drawn by the fan can be measured by the current meter 12 (figure 1), where
a measured current value corresponds to a respective drive frequency (or a respective
oscillation frequency).
[0061] Each measured current value from the above range of values is provided by the current
meter 12 to the processor 13. Likewise, the corresponding drive (excitation) frequency
value of the alternating electric excitation signal is provided by the power source
10 to the processor 13. Upon receipt of such range of current-frequency pair values
the processor is configured to store such values and generate an assessment chart.
Such assessment chart may be in any convenient form for example in the form of a table
of corresponding values or in the form of a graph in the form of a graph similar to
that of figure 5.
[0062] The processor is further configured to find the frequency located at mid-way (+/-0.1
Hz) between a first frequency value corresponding to the current peak I
p and a second frequency value corresponding to the current trough I
t of said graph. Once the second harmonic of the resonant frequency of the blade is
determined by the processor 13, the latter sends a command to the power source 10,
through connection path 143, to cause the power source to change the frequency of
the alternating electric excitation signal to match the newly determined second harmonic
of the resonant frequency of the blade.
[0063] In this manner the second harmonic of the resonant frequency point may be determined
while the fan continues to operate. This operation is advantageous as it may allow
for cleaning the blade from foul adhered thereto or removing blockage from the blade's
displacement path as will be described with reference to figures 6A, 6B, 6C and 7.
[0064] Figures 6A, 6B and 6C are exemplary schematic representations of an oscillation blade
in a heat sink according to some embodiments. In these figures, unless otherwise provided,
like elements have been given like reference numerals as those of previous figures,
and for simplicity only the blade of the oscillation blade fan is shown. Here again,
similar to the scenario of figures 4A and 4B, it is assumed that the fan is installed
in a heat sink 15. Under normal (non-faulty) condition and oscillating at a frequency
matching the resonant frequency of the blade 112, the blade would perform the maximum
deflection as shown by broken lines 112 and broken arrow A
r in figure 6A. However, dust and dirt 121 floating in the surrounding air may adhere
to the blade 112 thereby causing the blade to oscillate under faulty condition with
an amplitude of deflection A
f which is smaller than the maximum deflection A
r of the tip of the blade, as shown by solid lines 112 and solid arrow A
f. The particle of dust or dirt is shown in the figure by reference numeral 121-a.
[0065] To overcome this problem, the technique described with reference to figure 5 may
be employed to determine the second harmonic of the new resonant frequency of the
blade under the faulty condition. Once the second harmonic of the new resonant frequency
is determined, the frequency of the alternating driving signal (provided by the power
source 10 of figure 1) may be adjusted to the new determined second harmonic resonant
frequency thereby causing the blade 112 to oscillate at such second harmonic resonant
frequency. This latter scenario is shown in figure 6B.
[0066] This oscillation of the blade at a second harmonic of the resonant frequency of the
blade under faulty condition may exert an ejecting force on the particles which are
adhered to the blade thereby resulting in their removal, as shown in the figure by
reference numeral 121-b.
[0067] Furthermore, as seen in figure 6B (and also figure 5) when the blade 112 is driven
at a frequency which matches the second harmonic of the resonant frequency of the
blade under faulty condition, the oscillation pattern of the blade defines a standing
waveform W with two nodes N
1 and N
2 (figure 5). This solution provides advantages for cleaning the blade from adhered
particles because the generated standing waveform W with two nodes defines the broadest
deflection amplitude as compared to the deflection at frequencies that are higher
or lower than said second harmonic frequency, as can be seen in the upper part of
figure 5. This broad deflection amplitude in conjunction with the higher rate of agitation
of the blade (as compared to agitation under its fundamental resonant frequency) produce
an optimized effect for ejecting on the particles 121-a thereby assisting the overall
cleaning operation of the blade 112.
[0068] Once this blade is free of particles adhered thereto, or at least it is cleaner than
its status prior to the agitation at the second harmonic frequency, the frequency
of the alternating driving signal (provided by the power source 10 of figure 1) may
be adjusted to the fundamental resonant frequency of the blade thereby causing the
blade 112 to oscillate at its maximum deflection again. This latter scenario is shown
in figure 6C wherein the blade, free of foul adhered thereto oscillates at the adjusted
driving frequency (matching the resonant frequency of the blade) thereby performing
the maximum deflection, as shown by solid lines 112 and solid arrow A
r.
[0069] It is to be noted that oscillating the blade at the second harmonic of its resonant
frequency under faulty condition may or may not remove all the particles adhered to
the body of the blade. In case, such operation removes all the particles from the
blade, the blade may then be driven at its nominal resonant frequency (i.e. under
clean or normal conditions) to obtain maximum deflection. On the other hand, if oscillating
the blade at the second harmonic of its resonant frequency under faulty condition
does not remove all the particles from the blade and certain particles still remain
thereon, then the technique described with reference to figure 3 may be employed in
order to determine the resonant frequency of the blade under such new faulty condition
(being different from the faulty condition prior to such oscillation at said second
harmonic frequency). Once the new resonant frequency of the blade is determined, the
blade may then be driven at its new resonant frequency to obtain maximum deflection.
[0070] In the scenario of figures 6A, 6B and 6C, the processor may be programmed to follow
a similar procedure as described with reference to figure 5 and further be programmed
to send an additional (second) command signal to the power source to cause the power
source to return to the operation in which the frequency of the alternating electric
excitation signal matches the fundamental resonant frequency of the blade. In order
to determine when such second command may be sent, a number of solutions may be employed.
Some non-limiting examples are provided below.
[0071] According to one possible scenario, the processor may be programmed to send the second
command signal to the power source after a certain time period has elapsed during
which it is expected that the blade is free of particles or at least it is cleaner
than its status prior to the agitation at the second harmonic frequency. Once the
second command has been sent and the frequency of the alternating electric excitation
signal is adjusted accordingly, the same operation as described with reference to
the embodiment of figure 3 may be repeated to assess whether the blade is oscillating
at a frequency which enables maximum deflection of the tip of the blade. Should this
be the case, then no further adjustment would be needed, at least as long as new adhered
particles do not alter the performance of the blade; otherwise, the same operation
is repeated and further adjustments to the frequency of the alternating excitation
signal are performed until the new actual resonant frequency of the blade is found
and applied as driving frequency so as to ensure maximum blade deflection. According
to another possible scenario, the processor may be configured to assess the performance
of the blade as it oscillates according to the second harmonic of its resonant frequency
with the particles adhered thereon. As the particles are removed from the blade, the
second harmonic of the resonant frequency of the blade may change and therefore the
processor may detect, according to the procedure described with reference to figure
5, that the blade is no longer oscillating at its current (modified) second harmonic
frequency. This would indicate removal of at least some particles from the blade.
In this situation, the processor may send a command to the power source to adjust
the frequency of the alternating electric excitation signal to the fundamental resonant
frequency of the blade as the particles (or some of the particles) adhered to the
blade have been removed.
[0072] Alternatively the processor may be programmed to send a command to the power source
to adjust the frequency of the alternating electric excitation signal to the current
(modified) second harmonic of the resonant frequency of the blade and assess again
whether additional variation in the determined oscillation frequency of the blade
is detected due to the possibility of further particles being removed from the blade.
This operation may be repeated until the processor does not detect further significant
variation in the oscillation performance of the blade as it oscillates at the second
harmonic of its resonant frequency which may be indicative that the blade is now substantially
free of particles. At this point the processor may determine the new (fundamental)
resonant frequency of the blade from the latter second harmonic resonant frequency
at which no further significant variation is detected in the performance of the blade
In this manner, the proposed solution provides the additional advantage of dynamically
cleaning the blade without the need to stop the operation of the fan. Depending on
the environment in which an equipment may be installed, e.g. outdoors or indoors,
not only dust and dirt, but also larger objects may get introduced inside the housing
of the equipment and therefore reach the oscillation blade fan. Such larger objects
may not get directly adhered to the blade but they may block its oscillation path
and thereby degrade the cooling performance of the fan. In some cases, it may not
be possible to address a faulty condition involving a large object solely by adjusting
the frequency of the driving electric signal to match the resonant frequency of the
blade.
[0073] Figure 7 shows an example of such scenario. In this figure, unless otherwise provided,
like elements have been given like reference numerals as those of previous figures,
and for simplicity only the blade of the oscillation blade fan is shown. Here again,
it is assumed that the fan is installed in a heat sink 15. Under normal (non-faulty)
condition and oscillating at a frequency matching the resonant frequency of the blade
112, the blade would perform the maximum deflection as shown by broken lines 112 and
broken arrow A
r in figure 6A.
[0074] As shown in figure 7, objects 124, 125, having larger sizes than the particles 121
are introduced inside the heat sink 15, and in particular, a large object 125 is located
adjacent to the blade 112 blocking the oscillation path of the blade. Blockages which
suppress the movement of the blade 121 may also alter the current demand of the oscillation
blade fan for a fixed voltage input. By measuring this change in current and providing
the measured value to the processor 13 (in a similar fashion as in the embodiment
of figure 3), it may be possible to detect a blockage and send a warning signal which
can notify operators about contingency requirements (i.e. inspection/maintenance or
replacement).
[0075] To overcome such blockage situation, the blade 112 may be driven at a frequency rate
which is higher than the resonant frequency of the blade. For example the frequency
of the electric signal applied to the oscillation blade fan may be increased to values
close to the second harmonic of the resonant frequency of the blade until the blade
starts to oscillate in its second mode of oscillation being at the second harmonic
of the resonant frequency of the blade thereby generating a wave pattern having two
nodes, similar to the scenario of figure 5. This mode of operation may cause not only
the removal of all, or at least some, of the particles adhered to the blade, but also
may cause the removal of the blocking object 125 from the oscillation path of the
blade 112. This removal may be achieved as a result of the combination of the following
two effects: firstly, the blade oscillates at a higher frequency for the secondary
mode to exist as compared to the single mode drive frequency; and secondly, the oscillating
shape is different as two nodes are present in the wave pattern of the oscillation
instead of just one. The sudden changes involving alteration in the oscillation pattern
and velocity (oscillation frequency) of the blade may agitate and disturb the large
object 125 and may ultimately clear it away from the oscillation path of the blade.
After the removal of the large object is completed, the fan may be returned to its
normal operation under resonant frequency of the blade.
[0076] As mentioned above, the proposed solution is not limited only to oscillation blade
fans and is also applicable to other structures using an oscillation blade device
such as flexible wing structures. For example in the case of flexible wing structures,
the oscillation blade device is typically used for enabling a micro-aerial vehicle
to fly and not for cooling an electronic component. However, it is also of utmost
importance that the oscillating blade device in micro-aerial vehicles also operates
at its resonant frequency to maintain an optimum performance for the device which
would otherwise degrade the flying capabilities of the micro-aerial vehicle. Therefore,
similar solutions as those described with reference to the embodiments related to
an oscillation blade fan, are also applicable,
mutatis mutandis, to the oscillation blade device used as a flexible wing structure.
[0077] The proposed solution offers various advantages as it allows for determining the
oscillation resonant frequency of the blade under normal (non-faulty) or faulty conditions
by measuring the current demand, determining the resonant frequency of the blade and
accordingly adjusting the frequency of the driving alternating electric signal to
match such resonant frequency at all times and while the device is in operation. In
an oscillation blade fan, this solution enables the cooling mechanism to operate optimally
in various environments, even under faulty conditions; whereas in a flexible wing
structure, the solution enables an optimum flying performance of the micro-aerial
vehicle.
[0078] Secondly, the proposed solution also enables a new "self cleaning" capability that,
to the knowledge of the inventors, was not available in oscillation blade devices
to remove dust and/or dirt and therefore reduce maintenance requirements over the
operational lifetime. Thirdly, the proposed solution allows for removing a blockage
caused by an object present on the oscillation path of the blade.
[0079] The various embodiments of the present disclosure may be combined as long as such
combination is compatible and/or complimentary.
[0080] Further it is to be noted that the list of structures corresponding to the claimed
means is not exhaustive and that one skilled in the art understands that equivalent
structures can be substituted for the recited structure without departing from the
scope of the disclosure.
[0081] It should be appreciated by those skilled in the art that any block diagrams herein
represent conceptual views of illustrative circuitry embodying the principles of the
disclosure.
[0082] It is also to be noted that the order of the steps of the method of the disclosure
as described and recited in the corresponding claims is not limited to the order as
presented and described and may vary without departing from the scope of the invention.
1. An apparatus comprising:
- a power source configured for generating a plurality of alternating electric excitation
signals; and
- a current meter configured to measure a current value supplied by the power source;
wherein the apparatus is configured to:
- apply, by the power source, a plurality of alternating electric excitation signals
to an oscillation blade device at a corresponding plurality of excitation frequencies;
- measure, by the current meter, a plurality of current values supplied by the power
source to the oscillation blade device, each current value from the plurality of current
values corresponding to a respective excitation frequency from the plurality of excitation
frequencies, said plurality of current values comprising a peak current value corresponding
to a first excitation frequency and a trough current value corresponding to a second
excitation frequency; and
- provide said plurality of current values and said plurality of excitation frequencies
to a processor for determining a third excitation frequency.
2. The apparatus of claim 1, wherein said third excitation frequency is located mid-way
between the first excitation frequency and the second excitation frequency and corresponds
to a resonant oscillation frequency of a planar body comprised in the oscillation
blade device.
3. The apparatus of claim 1, wherein said third excitation frequency is located mid-way
between the first excitation frequency and the second excitation frequency and corresponds
to a second harmonic of a resonant oscillation frequency of a planar body comprised
in the oscillation blade device.
4. The apparatus of any one of the preceding claims, configured to drive said oscillation
blade device at a frequency matching the third excitation frequency.
5. A system comprising the apparatus of any one of the preceding claims 1 to 4, further
comprising:
- an oscillation blade device having a driver electrically coupled to the power source
and configured to generate a driving force in response to receiving an alternating
electric excitation signal from the power source, and a planar body attached to the
driver and configured to oscillate in response to the driving force generated by the
driver; and
- a processor configured to receive the plurality of current values and the plurality
of excitation frequencies and determine said third excitation frequency.
6. The system of claim 5, wherein the processor is configured to determine said third
excitation frequency value as a frequency located at mid-way between a first excitation
frequency and the second excitation frequency.
7. The system of claim 5 or claim 6, wherein the processor is configured to send a command
to the power source to cause the power source to change the frequency of the alternating
electric excitation signal to match the third excitation frequency.
8. A cooling assembly comprising the system of any one of claims 5 to 7.
9. A micro-aerial vehicle comprising the system of any one of claims 5 to 7.
10. A method for operating an apparatus, the apparatus comprising:
- a power source configured for generating a plurality of alternating electric excitation
signals; and
- a current meter configured to measure a current value supplied by the power source;
wherein the method comprises:
- applying, by the power source, a plurality of alternating electric excitation signals
to an oscillation blade device at a corresponding plurality of excitation frequencies;
- measuring, by the current meter, a plurality of current values supplied by the power
source to the oscillation blade device, each current value from the plurality of current
values corresponding to a respective excitation frequency from the plurality of excitation
frequencies, said plurality of current values comprising a peak current value corresponding
to a first excitation frequency and a trough current value corresponding to a second
excitation frequency; and
- providing said plurality of current values and said plurality of excitation frequencies
to a processor for determining a third excitation frequency.
11. The method of claim 10, comprising:
- determining said third excitation frequency located at mid-way between the first
excitation frequency and the second excitation frequency, the third excitation frequency
corresponding to a resonant oscillation frequency of a planar body comprised in the
oscillation blade device.
12. The method of claim 8, comprising:
- determining said third excitation frequency located at mid-way between the first
excitation frequency and the second excitation frequency, the third excitation frequency
corresponding to a second harmonic of a resonant oscillation frequency of a planar
body comprised in the oscillation blade device.
13. The method of any one of the preceding claims 8 to 10 comprising:
- driving said oscillation blade device at a frequency matching the third excitation
frequency.
14. The method of any one of the preceding claims 8 to 11, comprising sending a command
by the processor to the power source to cause the power source to change the frequency
of the alternating electric excitation signal to match the third excitation frequency.