[0001] The present invention relates to apparatus for. generating high frequency high level
noise fields.
[0002] High intensity noise fields of specified spectral shapes are required for a number
of industrial and technical testing purposes an example of which is the provision
of a high level noise field to excite and test aerospace structures in a simulated
noise environment of rocket, jet engine and propeller noise. The production of such
noise fields in the frequency range above 1.25 KHz has been found to be either impractical
or expensive. Certain acoustic test facilities have been using commercially available
low or medium frequency noise generators. These generators suffer from high-frequency
roll-off above about 500 Hz. A few test facilities have been using aeroacoustic noise
sources such as impingement jets, shock cell noise, Hartmann generators or modified
Hartmann generators in place of conventional "high" frequency noise generators. The
Hartmann generator produces narrow band high level tones and if it is detuned could,
less effectively, produce broad band tones. In order to fill up the width of the frequency
spectrum with noise, many Hartmann generators would have to be added. However this
solution is impractical insofar as the cost of operating multiple Hartmann generators
makes the solution uneconomical and further the interaction of the Hartmann signals
does not always produce the desired spectrum, as tests have shown.
[0003] For a background on the noise testing of articles reference is made to the paper
entitled The Use of Hartmann Generators as Sources of High Intensity Sound in a Large
Absorption Flow Duct Facility, D.L. Martlew of the National Gas Turbine Establishment
at Farnborough, Hants, United Kingdom, (published in the A.I.A.A. March 1975). The
paper discusses a large scale noise test facility used in an aeroengine reduction
noise program. Another paper of interest is that of D.A. Webster and D.T. Blackstock,
Journal of the Acoustic Society of America 63(3), March 1978, pages 687-693 which
discusses the interaction of high level high frequency tones with low level broad
band noise by collinear propagation.
[0004] The problem facing the test facilities is to fill up the produced noise spectrum
between 500 Hz and say, 10 KHz in an economical practical fashion.
[0005] According to the present invention there is provided a system for producing noise
comprising a tube means, at least one high frequency high-level noise generator adapted
for communication with said tube means; a low frequency high-level noise source operatively
connected to said tube means and for interaction with said generator whereby, in operation,
said generator is excited by the generated low frequency noise to provide an output
of non-linearly modulated noise.
[0006] According to a preferred feature of the invention a system for producing noise for
sonic testing of an article in a reverberation chamber comprises tube means adapted
for communication with the inside of the chamber; at least one aeroacoustic high frequency
high-level noise generator in the tube means; a low frequency high-level noise source
operatively connected to the tube means whereby, in operation, the generator is excited
by the generated low frequency noise to provide an output of non-linearly modulated
noise. The source may be a broad band or a narrow band low-frequency noise source.
Conveniently the tube means may include an acoustic horn adapted for operative connection
to the source at its small end and for operative connection to the reverberation chamber
at its large end.
[0007] In one preferred form of the invention a system for producing noise for sonic testing
of an article in a reverberation chamber comprises a low frequency high-level broad
band noise source; a tube means including a section formed as an acoustic horn adapted
for operative connection at its small end to the source and at its large end to the
chamber, and at least one Hartmann-type aeroacoustic high-level noise generator located
inside the tube at a predetermined position whereby, in operation, the generator is
excited by the generated low frequency noise to provide- an output of non-linearly
modulated noise. In a modification, two Hartmann-type aeroacoustic high-level noise
generators may be located in the tube means at predetermined spaced positions therealong,
the generators being tuned to different frequencies.
[0008] The invention also provides a Hartmann-type noise generator comprising a tube; a
slot cut out of the tube wall to produce an air gap between a nozzle section of the
tube at one side of the gap and a reverberation cup formed in the tube on the other;
the nozzle section and the cup being united by an uncut portion of the tube wall spanning
the slot and an adjustable tuning plug means in the cup.
[0009] According to another feature of the invention a Hartmann-type noise generator comprises
a nozzle and an aligned acoustic tube spaced therefrom by an air gap; a reverberation
cup formed in the mouth of the tube facing the nozzle and bridge means extending between
nozzle and tube and spanning the air gap and being in contact with a section of a
peripheral wall of the nozzle and an aligned section of a peripheral wall of the tube;
and means for varying the depth of the reverberation cup.
[0010] The following is a description by way of example of certain embodiments of the present
invention reference being had to the accompanying drawings in which:-
Figure 1 is a schematic representation of an application of the invention to the testing
of an article in a reverberation chamber;
Figure 2 is the acoustic spectrum propagated into a test chamber from a Hartmann-type
generator, operated alone;
Figure 3 is the acoustic spectrum propagated into the same chamber from a low frequency
high-intensity tonal noise source, operating alone;
Figure 4 is the acoustic spectrum propagated into the same test chamber when the functioning
of the Hartmann type generator is modified by a high intensity tone from the low frequency
source;
Figure 5 is the wide broad band spectra propagated in the chamber and using a logarithmic
frequency scale, when the functioning of two differently tuned Hartmann-type generators
is modified by a low frequency broad band noise source;
Figure 6 is a detail of a tube modified to accept a plurality of aeroacoustic noise
sources;
Figure 7 is a section along the lines 7-7 of Figure 6 showing an aeroacoustic generator
of the Hartmann type;
Figure 8 is a cross-section similar to Figure 6 and showing a rectangular tube means;
Figure 9 is a detail of a tuning arrangement for the aeroacoustic noise generator
of Figure 7; and
Figure 10 is a detail of a second form of aeroacoustic noise generator.
[0011] Turning now to the drawings. In Figure 1 a pair of broad-band (or tonal) low-frequency
high level noise sources 10 and 11 are operatively connected through a Tee-piece with
a tube means 14 having a tubular section 15 which may be of circular cross-section,
or rectangular cross-section as seen in Figures 7 and 8 respectively. The noise sources
may conveniently be Wyle broad-band devices of the type known as WAS 3000. Equally
well, the noise sources could be of the Ling type, such as sold by Ling Altec Limited
under the model no. EPT-200, electro-pneumatic transducer. In noise sources of this
type, compressed air at up to about 30 PSIG is blown into a chamber where slotted
sleeves slide axially under the action of an electrodynamic coil. The soundwaves thus
generated are propagated through the Tee-piece and into the tube means 14.
[0012] The tube means 14 may include an acoustic horn 17 connected at its broad end to a
reverberation chamber 18.
[0013] Arranged at, say, four separate places along the length of the tubular section 15,
are receiving apertures (see also Figures 6, 7 and 8) for an aeroacoustic noise' generator,
or generators, such as Hartmann type generators 20. Hartmann type generators are well
known in the art and do not require detailed explanation here but generally speaking
air is delivered at high speeds through a converging nozzle 21 and impinges directly
into the open end of a resonance cup 23. The shock wave created responds to the acoustic
pressure waves in the resonance cup 23 and a high intensity sound is emitted. This
sound has a spectrum consisting of a fundamental tone 30 (Figure 2) and harmonics
32, 33. The fundamental tone is related to the depth of the resonance cup which may
be tuned by moving a plug 25 (Figures 7, 8 and 9) longitudinally within the resonance
tube, as will be explained more fully hereinafter.
[0014] For the sake of simplicity of understanding, consideration should be given to the
interaction between a single low frequency source 10, or 11, controlled to emit a
tonal sound spectrum somewhat similar to that shown in Figure 3 with a single Hartmann
type aeroacoustic noise generator 20 producing a sound spectrum similar to that shown
in Figure 2. The noise from the sound source 10 interacts with, and excites, the natural
unsteady oscilli- tory aerodynamic flow in the Hartmann type generator 20 to produce
noise output which is a non-linear modulation (see Figure 4) of the normal noise generation
of the Hartmann generator 20. It will be noted that the Hartmann type device, or devices
20 are preferably positioned along the tubular section 15 so as to be close to the
high noise levels generated by the sources 10, 11. However, it is to be understood
that if desired, the tube means 14 could have provision made in its horn section 17
to receive one or more noise generators 20.
[0015] The propagated sound precedes along the horn 17 into a reverberation chamber 18,
in which the air is preferably kept dry, and acts.upon a test piece 19 suspended in
the reverberation chamber 18.
[0016] Depending upon the nature of the sound envelope which it is desired to generate,
and this of course will be dictated by the nature of the test or function which is
to be conducted, one or more Hartmann-type generators 20 may be positioned along the
tubular section 15 and one or more Wyle, or the like, sources may be operated. Where
it is desired to produce a broad spectrum flat envelope, a Wyle WAS 3000 type device
may be combined with two Hartmann-type generators 20 tuned to different frequencies
to produce the sound spectrum seen in Figure 5. Such a sound envelope, because of
its high intensity over a wide spectrum, is particularly useful for testing of aerospace
equipment, satelites and the like.
[0017] The curve 5a in Figure 5, is that of a WAS 3000 alone tuned to provide a broad band,
low frequency, high intensity noise and the curves 5b-5e are of two Hartmann-type
generators 20 modulated by the WAS 3000 and operated at different supply pressures.
The peak 5p may be adjusted to higher or lower frequencies depending on the tunings
of the Hartmann generators 20 and can be shifted to the left (as seen in Figure 5)
to merge with the WAS 3000 broadband noise.
[0018] Turning now particularly to Figures 6 through 9, the novel Hartmann-type generator
shown differs from the standard Hartmann-type acoustic generator in that it does not
comprise a separate nozzle and resonator cup section. Rather a tube member 26 is provided
with a slot 27 which is cut into the tube member wall. In the rectangular cross-section
tube 26 shown, the slob is cut into three adjacent side walls leaving a top uncut
wall section 28 to span the slot. The tube member 26 is provided With a flange 26F
which is bolted to a flange 21f (Figure 7) of a converging nozzle section 21 which
connects to an air source. On the left of the gap 27 is the nozzle section 26n of
the tube and on the right hand side of the air gap 27 (as seen in Figure 7) is the
resonator cup 23. The tuning of the generator is accomplished by moving the plug 25
forwards or backwards in the cup 23 longitudinally of the tube 26. 'The movement of
the plug 25 can be accomplished in any desired fashion.
[0019] In Figure 9 there is shown a simple form or adjustment in which a series of holes
30 are drilled in line in the top wall of the tube member 26 and a series of co-operating
tapped holes are provided in the plug. The plug is moved backwards and forwards in
the tube 26 and positioned by inserting a cap screw or screws into the appropriate
holes in the tube 26 and into the corresponding threaded holes in the plug 25 to anchor
it. Obviously a more elaborate or even automatic system could be provided in which
hydraulic or pneumatic cylinders, or the like, could be provided to push or pull the
plug, within the tube 26, to position it. Thus the plug position, and consequently
the tuning of the generator, could be remotely controlled. In tubes with short resonant
cavities, the tube cross-sectional area and shape may often prove to be an important
factor in tuning the generator to the desired frequency. Thus, rectangular, square,
triangular, semi-circular, or other suitable cross-sectional shape may be selected
to produce the desired frequency for a given air flow.
[0020] In the inventive configuration shown, at least two advantages accrue. First the wall
28 serves to combine the cavity 23 and nozzle 26n in accurate alignment and as a unitary
structure. Second, the aerodynamic and acoustic frequency performances are virtually
that of a tube of twice the cross-sectional area, additionally the aerodynamic boundary
layer on the wall 28 may allow operation of the generator to be extended from supercritical
nozzle pressure ratio down to subcritical nozzle pressure ratios, thereby providing
a greater range of selectable spectrum shapes and noise levels.
[0021] In order to attach the Hartmann-type generator in position on the tube section 15,
one of the blanking yokes 29 (see Figure 6) is simply unbolted from its ledge 29A
and the tube 26 of the generator 20 is bolted on that ledge 29i.
[0022] Figure 10 shows a second form of modified Hartmann-type generator in which a circular
section nozzle 40 is aligned with an acoustic tube 41 in the mouth of which 42 is
formed a reverberation cup 43. An air gap 44 separates the nozzle 40 from the tube
41, in normal fashion. The gap 44 may be varied to accommodate different noise generation
conditions and suitable clamping means may be provided to connect nozzle 40 and tube
41 for relative movement and to permit them to be clamped in a variety of spacings.
[0023] A bridge member 45 spans the air gap 44 and is slidingly engaged within the.nozzle
40 and the tube 41, resting on aligned sections of the peripheral walls 46, 47 of
nozzle and tube respectively. The bridge section is of semi-circular cross-section
where it spans the air gap and has a flat 48 machined on its top side. At the nozzle
end of the bridge member, the flat 48 is curved away at 49 towards the nozzle to provide
for smooth passage of air from the nozzle. At the other end of the bridge member 45
is a plug 50 formed integrally with the bridge member 45 and being of circular section
to fit snugly within tube 41. A series of holes 52 in the upper section of the peripheral
wall 47 accommodates a threaded screw member 53 which can be engaged in a selected
one of a series of threaded holes 54 in the circular plug 50 when the bridge member
is moved backwards and forwards within the tube 41 and nozzle 40 to vary the depth
of the reverberation cup 43, between the mouth of the tube 41 and the flat face 55
formed on the plug at the point where it meets with the flat 48 on the bridge member.
It will be understood that any other suitable mechanism may be provided for sliding
and fixing the plug 50 in the tube 41.
[0024] As has been indicated, if desired suitable means may be provided to clamp the bridge
45 to the nozzle 40, for example a series of holes similar to 52 may be provided in
the lower section of peripheral wall 46 of nozzle 40, to accommodate a threaded screw
member 53b which can engage in one of a series of threaded holes, similar to holes
54, provided in the underside of bridge 45 where it enters nozzle 40.
[0025] By sliding the bridge 45 with its plug 50 within the tube 41 so as to vary the depth
of the reverberation cup 43, the Hartmann-type generator may be tuned to different
frequencies.
[0026] This novel version of generator has the advantages of that described above with reference
to Figures 7, 8 and 9 and additionally provides for a variable air gap. Where a variable
air gap is not desired, the bottom segment of the peripheral walls 46, 47 may be left
integral, that is to say as with the generator shown in Figures 7, 8 and 9, the gap
44 may be cut as a slot and a wall, like 28, left in place.
[0027] Although the invention has been described with reference to the operation of the
generated noise being used to sonic test a piece of space equipment, it will be understood
that noise generated in the tube and passed either directly from the tube section,
or through the acoustic horn, or some other suitable tubular arrangement, may be used
to shake dust particles from an environment, or to generate sonic waves in a fluid,
or the like, in order to accomplish a desired purpose.
1. Apparatus for producing noise characterised by a tube (14), a high frequency high-level
noise generator (20) coupled to the tube, a low frequency high-level noise generator
(10) coupled to the tube for interaction with the said generator whereby, in operation,
the high frequency generator is excited by the generated low frequency noise to provide
an output to non-linearly modulated noise.
2. Apparatus according to claim 1, characterised in that the tube (14) is adapted
for communication with the inside of a reverberation chamber (18) and the high frequency
generator (20) is an aeroacoustic high frequency high-level noise generator.
3. Apparatus according to claim 2, characterised in that the tube (14) includes an
acoustic horn (15, 17) adapted for connection to the low frequency generator (10)
at its small end and for connection to the reverberation chamber (18) at its large
end.
4. Apparatus according to claim 1, 2 or 3, characterised in that the low frequency
generator (10) is a broad band low-frequency noise source.
5. Apparatus according to claim 1, 2 or 3, characterised in that the low frequency
generator (10) is a narrow band low-frequency noise source.
6. Apparatus according to any of claims 1 to 5, characterised in that there is a plurality
of high frequency noise generators (20) spaced along the tube (14) and tuned to different
frequencies.
7. Apparatus according to any of claims 1 to 6, characterised in that the or each
high frequency generator (20) is a Hartmann-type noise generator.
8. Apparatus according to any of claims 1 to 7, characterised in that the low frequency
generator comprises at least one electropneumatic transducer (10, 11).
9. A Hartmann-type noise generator comprising a tube (26), a slot (27) cut out of
the tube wall to provide an air gap between a nozzle section (26 n) of the tube and
a reverberation cup (23) formed in the tube, the nozzle section and cup being joined
by an uncut portion (28) of the tube wall spanning the slot, and an adjustable tuning
plug (25) in the cup.
10. A noise generator according to claim 9, characterised in that the tube (26) is
rectangular in cross-section and the slot (27) is cut in three of the four wall sides.
11. The Hartmann-type noise generator comprising a nozzle (40), an aligned acoustic
tube (41) spaced therefrom by an air gap (44), a reverberation cup (43) formed in
the mouth of the tube facing the nozzle, a bridge (45) extending between the nozzle
and tube and spanning the air gap and being in contact with a section of a peripheral
wall of the nozzle and an aligned section of a peripheral wall of the tube, and means
(50) for varying the depth of the reverberation cup.
12. A noise generator according to claim 11, characterised in that the nozzle (40)
and tube (41) are of circular section and the bridge (45) is a member of semi-circular
section where it spans the air gap, the bridge extending into the nozzle and into
the acoustic tube.
13. A noise generator according to claim 12, characterised in that the means for varying
the depth of the reverberation cup (43) is a circular plug (50) formed integrally
with the end of the bridge (45) and located within the reverberation cup, and position
adjusting means (52-54) to positively locate the plug within the acoustic tube (41).
14. A noise generator according to claim 13, characterised by means (53) for securing
the bridge (45) to the nozzle (40) and to the tube (41) to permit relative movement
between the nozzle and tube to vary the air gap (44).
1. Apparatus for producing noise characterised by a tube (14), a high frequency high-level
noise generator (20) coupled to the tube, a low frequency high-level!noise generator
(10) coupled to the tube for interaction with the said generator whereby, in operation,
the high frequency generator is excited by the generated low frequency noise to provide
an output of non-linearly modulated noise.
2. Apparatus according to claim 1, characterised in that the tube (14) is adapted
for communication with the inside of a reverberation chamber (18) and the high frequency
generator (20) is an aeroacoustic high frequency high-level noise generator.
3. Apparatus according to claim 2, characterised in that the tube (14) includes an
acoustic horn (15, 17) adapted for connection to the low frequency generator (10)
at its small end and for connection to the reverberation chamber (18) at its large
end.
4. Apparatus according to claim 1, 2 or 3, characterised in that the low frequency
generator (10) is a broad band low-frequency high level noise source.
5. Apparatus according to claim 1, 2 or 3, characterised in that the low frequency
generator (10) is a narrow band low-frequency noise source.
6. Apparatus according to any of claims 1 to 5, characterised in that there is a plurality
of high frequency noise generators (20) spaced along the tube (14) and tuned to different
frequencies.
7. Apparatus according to any of claims 1 to 6, characterised in that the or each
high frequency generator (20) is a Hartmann-type noise generator.
8. Apparatus according to any of claims 1 to 7, characterised in that the low frequency
generator comprises at least one electro-
(41) to permit relative movement between the nozzle and tube to vary the air gap (44).
15. Use of apparatus according to any of claims 1 to 8 for sonic testing of an article.
16. Use of apparatus according to any of claims 1 to 8 for sonic testing of an article
in a reverberation chamber.