GOVERNMNENT LICENSE RIGHTS
[0001] This invention was made with U.S. government support under contract no. W31P4Q-09-C-0348
awarded by the U.S. Army. The U.S. government has certain rights in the invention.
BACKGROUND
[0002] Atomic sensors, like cold atom clocks and ring laser gyroscopes, use external components
to control light and optical signals as they enter the body of the atomic sensor and
to sense light and signals as they exit the body of the atomic sensor. Because the
external components receive and control light and other signals, the components must
be in the correct location relative to the body of the atomic sensor to accurately
receive and control the light and other signals. To secure the external components
in the correct location, the components are attached to the body of the atomic sensor
using adhesives. Alternatively, an external mechanical structure can secure the atomic
sensor and external components in the desired locations relative to one another. However,
when the external components are secured using either an adhesive or an external mechanical
structure, vibrations and shocks cause the components and the atomic sensor to move
in relation to one another. This movement in relation to one another affects the operative
quality of the sensor. Further, mounting the external components using adhesive or
an external mechanical structure requires multiple steps during fabrication of the
atomic sensor.
SUMMARY
[0003] The embodiments of the present invention provide systems and methods for external
frit mounted components and will be understood by reading and studying the following
specification.
[0004] Embodiments of the present invention provide improved systems and methods for external
frit mounted components on a sensor device. In one embodiment, a method for fabricating
a sensor device comprises securing at least one component stack on a sensor body over
at least one opening in the sensor body, wherein the at least one component stack
comprises a plurality of components and applying a frit to the plurality of components
in the at least one component stack and the sensor body. The method further comprises
heating the frit, the at least one component stack, and the sensor body such that
the frit melts and cooling the frit, the at least one component stack, and the sensor
body such that the at least one component stack is secured to the sensor body.
DRAWINGS
[0005] Embodiments of the present invention can be more easily understood and further advantages
and uses thereof more readily apparent, when considered in view of the description
of the preferred embodiments and the following figures in which:
[0006] Figure 1 is a cross section diagram illustrating externally mounted components attached
with frit to a sensor body in one embodiment of the present invention;
[0007] Figure 2 is a block diagram illustrating multiple components in a component stack
in one embodiment of the present invention;
[0008] Figure 3 is a block diagram illustrating a fixture for securing a component stack
to a sensor body in one embodiment of the present invention;
[0009] Figure 4 is a block diagram illustrating a detailed view of the fixture when securing
a component stack to a sensor body in one embodiment of the present invention;
[0010] Figure 5 is a block diagram showing an exemplary implementation of an atomic clock
in one embodiment of the present invention; and
[0011] Figure 6 is a flow diagram illustrating a method for attaching externally mounted
components to a sensor body using frit in one embodiment of the present invention.
[0012] In accordance with common practice, the various described features are not drawn
to scale but are drawn to emphasize specific features relevant to the exemplary embodiments.
DETAILED DESCRIPTION
[0013] In the following detailed description, reference is made to the accompanying drawings
that form a part hereof, and in which is shown by way of specific illustrative embodiments
in which the invention may be practiced. These embodiments are described in sufficient
detail to enable those skilled in the art to practice the invention, and it is to
be understood that other embodiments may be utilized and that logical, mechanical
and electrical changes may be made without departing from the scope of the present
invention. The following detailed description is, therefore, not to be taken in a
limiting sense.
[0014] Embodiments of the present invention provide systems and methods for externally mounting
components on an atomic sensor using frit. This is accomplished by placing the external
components in the correct location in relation to the body of the atomic sensor and
applying frit around the external components such that when the atomic sensor, the
external components and frit are heated, the frit welds the external components to
each other and to the body of the atomic sensor. By using frit, the external components
become rigidly attached to the body of the atomic sensor such that the external components
move with the atomic sensor when the system is vibrated or shocked. Further, the external
components can be joined to the body of the atomic sensor at the same time that other
components are joined to the body of the atomic sensor. Because multiple components
can be joined at various locations on the body of the atomic sensor simultaneously
using frit, the use of frit uses less fabrication steps to join the body of the atomic
sensor to the external components.
[0015] Figure 1 is a cross section diagram of sensor 100 where external components are attached
with frit 104 to a sensor body 106 of the atomic sensor 100. Sensor 100 is an optical
sensor (such as an accelerometer, a gyroscope, an atomic clock, and the like). In
certain embodiments, sensor 100 includes a sensor body 106 that includes a cavity
108 that encompasses a hermetically sealed environment, where the environment type
aids sensor 100 in operating correctly. For example, when sensor 100 is a ring laser
gyroscope, the cavity 108 will contain a desired gas that is hermetically sealed within
the sensor body 106. In an alternative implementation, where the sensor is an atomic
clock, the cavity 108 encompasses a vacuum that is hermetically sealed within the
sensor body 106.
[0016] In certain implementations, measurement information obtained by sensor 100 is obtained
by observing patterns of optical energy contained within cavity 108. For that reason,
sensor 100 provides openings 110 to allow measurement information produced within
cavity 108 to be used by an external system connected to sensor 100. Openings 110
are locations on sensor body 106 that allow optical energy to leave or enter the sensor
body 106, and allow an external system to analyze the patterns of optical energy within
cavity 108.
[0017] As shown in Figure 1, components that interface with sensor body 106 are combined
together to form one or more component stacks 102. Sensor 100 can have multiple component
stacks 102 that are associated with different openings 110 in sensor body 106. For
example, when sensor 100 is an atomic clock, the sensor body 106 can have one or more
openings 110 that introduce light into cavity 108 and one or more openings 110 for
light to be transmitted out of cavity 108. In one exemplary embodiment of a component
stack 102 associated with directing light into cavity 108, component stack 102 may
include a light source (such as a laser, for example), a lens, a beam splitter (that
is, a device that directs portions of light to separate openings), a beam expander,
and the like. In an exemplary embodiment of a component stack 102 associated with
receiving light from cavity 108, component stack 102 includes a photodetector, a lens,
and the like. Further, to preserve a vacuum within the cavity 108, in one embodiment,
component stack 102 includes a getter. In one embodiment where sensor 100 is a ring
laser gyroscope, the component stack 102 will include a light emitting diode for starting
the operation of the ring laser gyroscope. In one embodiment, openings 110 around
cavity 108 may include optical elements 112 that may comprise, transparent window
elements, reflective mirror elements, or elements that are partially transparent and
partially reflective.
[0018] In at least one embodiment, frit 104 or glass solder is used to join the individual
components in component stack 102 to each other. The word "frit," as used herein,
refers to a fused or a partially fused substance that can be heated into glass. In
conjunction with bonding the individual components to one another, frit 104 is also
used to bond the component stack 102 to the sensor body 106. In some implementations,
frit 104 is used to bond mirrors and windows 112 to sensor body 106. In some embodiments
where optical elements 112 are bonded to sensor body 106, the component stack 102
is bonded to optical elements 112. For example, an optical element 112 may be bonded
to the sensor body 106 using frit 104, such that the frit 104 forms a hermetic seal
between the optical element 112 and the sensor body 106. In an alternative embodiment
where an opening 110 does not include an optical element 112, a component stack 102
is directly joined to the sensor body 106 over an openings 110 using frit 104 to form
a hermetic seal between the component stack 102 and sensor body 106.
[0019] By using frit 104 to join component stacks 102 (either in conjunction with optical
elements 112, or not) to the sensor body 106, the components in the component stack
102 become securely bonded to the sensor body 106 such that the effects of shocks
and vibrations to sensor 100 on the accuracy of sensor 100 is reduced. Further, by
using frit 104 to join the components in component stack 102 to one another and the
component stack 102 to the sensor body 106, the components in the sensor 100 can be
located at their respective locations in relation to the sensor body 106 and bonded
to one another and to the sensor body 106 simultaneously. Figure 2 is a block diagram
illustrating a sensor 200 with multiple components in multiple component stacks. In
one embodiment, sensor 200 comprises a sensor 100 such as described above. As such,
the description of alternate embodiments provided herein with respect to Figure 2
may be applied to embodiments described in Figure 1 and
vice versa. In the embodiment illustrated in Figure 2, sensor 200 is an atomic clock. Sensor
200 includes at least three component stacks, 202, 222, and 242. Component stack 202
and 222 function together to introduce light into the cavity 208 within sensor 200.
Sensor 200 includes a sensor body 206 that includes a cavity 208 comprising a vacuum
chamber cavity that holds alkali metal atoms such as rubidium or cesium (for example,
Rb-87) in a passive vacuum. An arrangement of mirrors 210 and windows 212 allow beams
of light to be directed into and around the sensor body 206, where the mirrors 210
reflect the beams around the interior of the sensor body 206. In some embodiments,
the component stacks 202, 222, and 242 are directly bonded to sensor body 206 and
not bonded to an interceding window 212. In other embodiments, one or more of component
stacks 202, 222, and 242 may be bonded to an interceding window.
[0020] Component stack 202, 222, and 242 include lenses 203, 223, and 243. Lenses 203, 223,
and 243 are each placed at their respective locations such that they abut against
sensor body 206, whereupon, lenses 203, 223, and 243 are secured to the sensor body
206 using frit. By securing the lenses 203, 223, and 243 as close as possible to the
sensor body 206 using frit, the lenses 203, 223, and 243 in conjunction with the frit
are able to hermetically seal the interior cavity of sensor body 206 and preserve
a vacuum environment within the cavity 208. In some embodiments, one or more of lenses
203, 223, and 243 are convex lenses placed against sensor body 206. In such embodiments,
the convex portion of the lens may be arranged to face the interior cavity 208 of
sensor body 206 so that they are able to effectively transmit from component stacks
202 and 222 and focus the light at a particular location within cavity. In one embodiment,
lens 243 receives light from within sensor body 206 and focuses it onto receiving
electronics 244 in component stack 242.
[0021] In one embodiment, component stack 202 includes components that receive a light beam
250 and adjust the light beam 250 before it enters the interior cavity 208 of sensor
body 206. To adjust light beam 250, component stack 202 includes a collimating lens
217, an optical isolator 213, a series of wave plates 209, a beam splitter 211, and
a beam expander 207. Component stack 202 also includes support structures 215 and
205 to set the various components at the appropriate distances from one another to
correctly adjust the properties of light beam 250.
[0022] In operation, component stack 202 first receives the light through a collimating
lens 217. Collimating lens 217 receives light beam 250 from a light source (like a
laser, or other light producing device) and adjusts light beam 250 such that the rays
of light that compose light beam 250 are parallel to one another. The light then leaves
collimating lens 217 to enter optical isolator 213. In some embodiments, the collimating
lens 217 is offset from optical isolator 213 a defined distance before the collimated
light enters the optical isolator 213. To support the collimating lens 217 at the
offset distance from optical isolator 213, support structure 215 attaches between
collimating lens 217 and optical isolator 213. In at least the embodiment shown, support
structure 215 is made from glass and rigidly connects to both collimating lens 217
and optical isolator 213 during the fabrication process. In at least one embodiment,
the bonded combination of the collimating lens 217, optical isolator 213, and support
structure 215 enclose a hermetically sealed chamber through which light beam 250 travels
after collimation.
[0023] Optical isolator 213 allows light to travel through component stack 202 in only one
direction and functions as an optical diode. After the light beam 250 passes through
optical isolator 213, light beam 250 enters a beam splitter 211 and a combination
of wave plates 209. As shown in the exemplary embodiment of Figure 2, beam splitter
211 is sandwiched between two wave plates 209. The wave plates 209 alter the polarity
of the light beam as it travels through component stack 202 to a desired polarity
for entry into the sensor body 206. As shown, a first wave plate 209 alters the polarity
of light beam 250 before it passes through beam splitter 211. Beam splitter 211 splits
light beam 250 into two separate light beams 250a and 250b. Light beam 250b is reflected
by beam splitter out of component stack 202 for use in an external application or
for use by a different component stack such as component stack 222. In contrast to
light beam 250b, light beam 250a passes through further components in component stack
202 before it passes into sensor body 206. For example, after passing through beam
splitter 211, light beam 250a passes through a second wave plate 209 to further adjust
the polarity of light beam 250a before light beam 250a enters into the sensor body
206.
[0024] When the polarity of light beam 250a has been adjusted by wave plates 209, light
beam 250a passes through a beam expander 207 and lens 203, where lens 203 is substantially
described above and forms a hermetic seal with sensor body 206. Beam expander 207
refracts the collimated and polarized light such that light beam 250a expands before
passing through lens 203. To allow the refracted light beam 250a to expand, beam expander
207 is offset away from lens 203 by a distance that provides substantially enough
space between beam expander 207 and lens 203 for light beam 250a to expand to a desired
diameter before light beam 250a passes through lens 203. To offset beam expander 203
from lens 207, a support structure 205 rigidly bonds to both lens 203 and beam expander
207. In one implementation, support structure 205 is fabricated from glass and bonds
to both beam expander 207 and lens 203 using a frit seal. In one implementation, the
frit seal bonding support structure 205 to beam expander 207 and lens 203 is a hermetic
seal to prevent foreign substances from entering the space within support structure
205 and interfering with light beam 250a. After passing through lens 203, light beam
250a is reflected by a series of mirrors 210 to direct the light at a group of atoms
in the middle of the sensor body 206.
[0025] In one embodiment, light beam 250b, which is reflected out of component stack 202
by beam splitter 211, is reflected by one or more mirrors 230 to enter component stack
222. Component stack 222 includes wave plate 229, beam expander 227, and lens 223.
In one embodiment, the components in component stack 222 are supported by support
structure 225. The different components in component stack 222 function similarly
to corresponding components in component stack 202. For example, wave plate 229 functions
similarly to the second wave plate in wave plates 209, beam expander 227 functions
similarly to beam expander 207, lens 223 functions similarly to lens 203, and support
structure 225 functions similarly to support structure 205. The different locations
of component stacks 202 and 222 on the external surface of sensor body 206 aid in
providing different beams of light that are reflected by mirrors 210. For example,
mirrors 210 reflect light beams 250a and 250b in such a way that different reflected
light beams within sensor body 206 intersect along three orthogonal axes while illuminating
atoms located at the center of cavity 208.
[0026] As described above, sensor 200 includes component stack 242 which includes a photodetector
244 and a lens 243. In some instances, where light is reflected out of the cavity
208 by a mirror 210, that light is reflected to component stack 242. Component stack
242 also includes a support structure 245 to hold photodetector 244 at a prescribed
distance from lens 243. Support structure 245 functions similarly to the other support
structures 225 and 205 in component stacks 202 and 222. Specifically, support structure
225 functions to place space between optical components while bonding to the optical
components. Support structure 225 can also bond to both photodetector 244 and lens
243 with a frit seal. Further, the frit seal that bonds support structure 225 to photodetector
244 and lens 243 hermetically isolates the space between photodetector 244 and lens
243.
[0027] As described above, component stacks 202, 222, and 242 each include multiple components
that are placed at precise locations in relation to sensor body 206 to allow light
to correctly propagate in, around, and out of sensor body 206. The components in component
stacks 202, 222, and 242 are bonded together and to sensor body 206 using frit to
rigidly maintain the precise location of the components in relation to the sensor
body 206. The use of frit to bond the components in component stacks 202, 222, and
242 to the sensor body 206 reduces the movement of the components in relation to the
sensor body 206 during the operation of the sensor 200. By reducing the movement of
the components in relation to sensor 200, the use of frit to bond the components within
component stacks 202, 222, and 242 together and to bond the component stacks 202,
222, and 242 to sensor body 206 also reduces errors in measurements by sensor 200
due to reduced movement of the components in relation to the sensor body 206.
[0028] Figure 3 is a block diagram illustrating a fixture 304 for securing a component stack
302 (such as any of sensor stacks 102, 202, 222, or 242) to a sensor body 306 (such
as sensors body 106 or 206). As was stated above, one advantage of using a fritting
process is that all of the various components of the sensor can be bonded to the sensor
body 306 at the same time. To bond the various components in the component stack 302,
mirrors, windows, and the like to sensor body 306, sensor body 306 is mounted within
a fixture 304. The term "fixture," as used herein, refers to a rigid structure that
holds components in a precise location during fabrication. For example, when the sensor
body 306 is mounted within the fixture 304, the fixture holds the components at a
desired location in relation to the sensor body 306. In one embodiment, fixture 304
uses plungers 310 to hold the different components of component stack 302 in place.
In another exemplary implementation, fixture 304 is composed of multiple parts that
are assembled together at the time the sensor body 306 and components are assembled
together. For example, fixture 304 has a top portion 308 that is secured to a lower
portion 312 of fixture 304 after the sensor body 306 has been placed within fixture
304. Fixture 304 secures all the components to sensor body such that frit can be applied
to the multiple components and the sensor body. Further, fixture 304, the components,
sensor body 306, and the frit joining the sensor body 306 and the components can be
heated at the same time such that the frit simultaneously bonds all the assembled
pieces held in place by fixture 304. When the frit has bonded the various components
to the sensor body 306, the sensor body 306 and adjoining components are removed from
fixture 304.
[0029] Figure 4 is a block diagram illustrating a detailed view of a fixture 404 when securing
a component stack 402 (such as component stack 302) to a sensor body 406 (such as
body 306). When component stack 402 is secured to sensor body 406, the various components
in sensor body 406 are first prepped for assembly by cleaning the separate components.
When the different components in component stack 402 are ready for assembly to sensor
body 406, the different pieces are placed together one by one onto sensor body 406.
In at least one embodiment, sensor body 406 and fixture 404 are rotated such that
sensor body 406 is directly below component stack 402. By orienting sensor body 406
below component stack 402, gravity can aid in the stacking of the different components
in component stack 402 before the components are secured in place with a plunger 410
connected to fixture 404.
[0030] In certain embodiments, when the component stack 402 is substantially similar to
component stack 202 described in Figure 2, in the assembly of component stack 402,
a lens 403 is fitted into sensor body 406. The other components in component stack
402 are then subsequently stacked on top of one another as the components move away
from sensor body 406. For example, support structure 405 is placed on the lens, the
beam expander 407 is then placed on the support structure 405, the second wave plate
409 is placed on the beam expander 407, the beam splitter 411 is placed on the second
wave plate 409, and the first wave plate 409 is placed on the beam splitter 411. Further,
the optical isolator 413 is placed on the first wave plate 409, a support structure
415 is placed on optical isolator 413, and a collimating lens 417 is placed on support
structure 415. When all the components in component stack 402 are placed on top of
one another, a plunger 410 is then placed on collimating lens 417 and support structure
415 to secure component stack 402 to sensor body 406.
[0031] When the components of component stack 402 are in place and secured to sensor body
406, frit is applied to the component stack 402 to join the different components in
component stack 402 together. In one embodiment, frit is applied to hermetically seal
the space between components. Alternatively, frit is also applied to the different
components such that the components are bonded to one another but the space between
the different components is not hermetically sealed. The frit is then heated and cooled
to bond the different components together. When the different components in component
stack 402 are bonded to one another through the frit, the plunger 410 in fixture 404
is removed and the sensor is removed from fixture 404.
[0032] In certain embodiments, as has been described above, the atomic sensor is an atomic
clock. The use of frit enables the manufacture of atomic clocks that can be manufactured
in fewer steps and are less susceptible to errors caused by vibrations and shocks.
Further, the atomic clocks described above can be used to provide a reference frequency
signal to frequency dependent applications as part of Global Positioning System satellites,
unmanned aerial vehicles, navigation systems, and the like. Figure 5 illustrates the
implementation of an atomic clock 502 in a system 500. In certain embodiments, atomic
clock 502, constructed implementing the fritted component stacks as described above,
is small enough to be used in micro-electromechanical systems (MEMS). For example,
atomic clock 502 is mounted as part of a MEMS device 504. Atomic clock 502 produces
a reference frequency and provides the reference frequency to a frequency dependent
device 506. The reference frequency provided by atomic clock 502 increases the operational
stability and accuracy of frequency dependent device 506. For example, when frequency
dependent device 506 is a component of a Global Positioning System satellite, the
atomic clock 502 allows the satellite to provide more accurate reference times for
the accurate calculation of positions.
[0033] Figure 6 is a flow diagram illustrating a method 600 for attaching externally mounted
components to a sensor body using frit. Method 600 begins at 602 with securing at
least one component stack on a sensor body over at least one opening in the sensor
body, wherein the at least one component stack comprises a plurality of components.
In one embodiment, the opening includes an optical element such as a window or mirror
over the opening. In such embodiments, the component stack is secured over the optical
element. In one embodiment, as described above in relation to Figures 3 and 4, a fixture
secures a component stack comprising a plurality of different components to a sensor
body. The fixture includes a rigid frame that secures the positions of both the component
stack and the sensor body at fixed positions in relation to each other. In one embodiment,
the fixture includes a plunger that applies pressure against the component stack,
which pressure secures the component stack to the sensor body.
[0034] Method 600 proceeds at 604 with applying a frit to the plurality of components in
the at least one component stack and the sensor body. In one example, frit is applied
around the opening in the sensor body and the adjoining component stack. Further,
frit is applied around the different components in the component stack. In one embodiment,
frit is applied to a window or mirror over and opening in the sensor body and the
adjoining component stack.
[0035] Method 600 proceeds at 606 with heating the frit, the at least one component stack,
and the sensor body such that the frit melts. For example, a fixture that secures
the component stacks to the sensor body is passed through an oven that gradually heats
frit on the sensor body and component stacks to a frit melting temperature. (For example,
the oven heats the frit to 420° Celsius). At this temperature, the frit will melt
and bond to the adjoining surfaces. Method 600 proceeds at 608 with cooling the frit,
the at least one component stack, and the sensor body such that the component stack
is secured to the sensor body. For example, the sensor body and component stack within
the fixture is gradually cooled to prevent the sensor body and components from cracking
due to a rapid temperature change. When the frit cools, the component stack will be
rigidly bonded to the sensor body. And the sensor body and connected component stack
can be removed from the fixture.
EXAMPLE EMBODIMENTS
[0036] Example 1 includes a sensor device, the device comprising a sensor body, the sensor
body comprising a cavity, wherein the sensor body comprises at least one opening in
the body providing access to the cavity; and at least one component stack mounted
to the sensor body over the at least one opening using a frit, wherein the component
stack comprises a plurality of components that are attached to one another with the
frit.
[0037] Example 2 includes the device of Example 1, wherein the at least one opening further
comprises at least one optical element attached to the at least one opening, wherein
the at least one optical element is attached to the sensor body with the frit such
that the frit hermetically seals the cavity within the sensor body.
[0038] Example 3 includes the device of Example 2, wherein the component stack is mounted
to the at least one optical element by the frit.
[0039] Example 4 includes the device of any of Examples 1-3, wherein the plurality of components
comprises at least one of an optical component, a structural support, a sensor, or
an electronics device.
[0040] Example 5 includes the device of any of Examples 1-4, wherein the component stack
is mounted to the sensor body with a frit seal such that the frit seal between the
component stack and the sensor body hermetically seals the cavity within the sensor
body.
[0041] Example 6 includes the device of any of Examples 1-5, wherein the sensor device comprises
at least one of an atomic clock; and a ring laser gyroscope.
[0042] Example 7 includes the device of any of Examples 1-6, wherein the plurality of components
in the component stack are hermetically sealed to one another.
[0043] Example 8 includes a method for fabricating a sensor device, the method comprising
securing at least one component stack on a sensor body over at least one opening in
the sensor body, wherein the at least one component stack comprises a plurality of
components; applying a frit to the plurality of components in the at least one component
stack and the sensor body; heating the frit, the at least one component stack, and
the sensor body such that the frit melts; and cooling the frit, the at least one component
stack, and the sensor body such that the at least one component stack is secured to
the sensor body.
[0044] Example 9 includes the method of Example 8, wherein the at least one component stack
is secured to the sensor body using a fixture, wherein a fixture comprises a device
that securely maintains the at least one component stack and the sensor body at fixed
positions in relation to one another.
[0045] Example 10 includes the method of Example 9, wherein the fixture comprises at least
one plunger to secure the at least one component stack to the sensor body.
[0046] Example 11 includes the method of any of Examples 9-10, further comprising separating
the sensor body and the at least one component stack from the fixture.
[0047] Example 12 includes the method of any of Examples 8-11, wherein securing the at least
one component stack on the sensor body further comprises placing at least one optical
element over the at least one light reception opening; placing the at least one component
stack on the at least one optical element; and securing the at least one component
stack and the at least one optical element to the sensor body.
[0048] Example 13 includes the method of Example 12, wherein the at least one optical element
comprises at least one of either a mirror or a window, the method further comprising
applying the frit around the at least one optical element such that the frit will
form a hermetic seal around the at least one opening when the frit is heated and cooled.
[0049] Example 14 includes the method of any of Examples 8-13, wherein the frit applied
to the plurality of components and the sensor body is applied such that the frit will
form a hermetic seal around the at least one opening when the frit is heated and cooled.
[0050] Example 15 includes the method of any of Examples 8-14, wherein heating the frit,
the at least one component stack, and the sensor body comprises gradually heating
the frit, the at least one component stack, and the sensor body to a frit melting
temperature.
[0051] Example 16 includes a system for providing a reference frequency, the system comprising:
an atomic clock, the atomic clock configured to produce a reference frequency signal,
wherein the atomic clock comprises: a clock body comprising a cavity, wherein light
is introduced into the cavity through a plurality of openings in the clock body; and
a plurality of component stacks mounted to the sensor body over the at least one opening
using a glass frit, wherein a component stack comprises a plurality of optical components
that are attached to one another with frit, wherein the optical components control
light before it enters the cavity and after it leaves the cavity.
[0052] Example 17 includes the system of Example 16, wherein a first component stack in
the plurality of component stacks comprises components that adjust a received light
beam before the light beam enters the cavity.
[0053] Example 18 includes the system of Example 17, wherein a component in the first component
stack splits the received light beam into a first part and second part, wherein the
second part is reflected into a second component stack in the plurality of component
stacks.
[0054] Example 19 includes the system of Example 18, wherein the first component stack and
the second component stack are positioned on the clock body such that the first part
and the second part of the light beam are orthogonal to one another when the first
part and the second part of the light beam enter the cavity.
[0055] Example 20 includes the system of any of Examples 16-19, wherein the plurality of
optical components in a respective component stack in the plurality of component stacks
are hermetically sealed to one another.
[0056] A number of embodiments of the invention defined by the following claims have been
described. Nevertheless, it will be understood that various modifications to the described
embodiments may be made without departing from the spirit and scope of the claimed
invention. Accordingly, other embodiments are within the scope of the following claims.
1. A sensor device, the device comprising:
a sensor body (106), the sensor body (106) comprising a cavity (108), wherein the
sensor body (106) comprises at least one opening (110) in the body (106) providing
access to the cavity (108); and
at least one component stack (102) mounted to the sensor body (106) over the at least
one opening (110) using a frit (104), wherein the component stack (102) comprises
a plurality of components that are attached to one another with the frit (104).
2. The device of claim 1, wherein the at least one opening (110) further comprises at
least one optical element (112) attached to the at least one opening (110), wherein
the at least one optical element (112) is attached to the sensor body (106) with the
frit (104) such that the frit (104) hermetically seals the cavity (108) within the
sensor body (106).
3. The device of claim 2, wherein the component stack (102) is mounted to the at least
one optical element (112) by the frit (104).
4. The device of claim 1, wherein the plurality of components comprises at least one
of:
an optical component, a structural support, a sensor, or an electronics device.
5. A method for fabricating a sensor device, the method comprising:
securing at least one component stack (102) on a sensor body (106) over at least one
opening (110) in the sensor body (106), wherein the at least one component stack (102)
comprises a plurality of components;
applying a frit (104) to the plurality of components in the at least one component
stack (102) and the sensor body (106);
heating the frit (104), the at least one component stack (102), and the sensor body
(106) such that the frit (104) melts; and
cooling the frit (104), the at least one component stack (102), and the sensor body
(106) such that the at least one component stack (102) is secured to the sensor body
(106).
6. The method of claim 5, wherein the at least one component stack (102) is secured to
the sensor body (106) using a fixture (304), wherein a fixture (304) comprises a device
that securely maintains the at least one component stack (102) and the sensor body
(106) at fixed positions in relation to one another.
7. The method of claim 6, wherein the fixture (304) comprises at least one plunger (310)
to secure the at least one component stack (102) to the sensor body (106).
8. The method of claim 6, further comprising separating the sensor body (106) and the
at least one component stack (102) from the fixture (304).
9. The method of claim 5, wherein securing the at least one component stack (102) on
the sensor body (106) further comprises:
placing at least one optical element (112) over the at least one light reception opening;
placing the at least one component stack (102) on the at least one optical element
(112); and
securing the at least one component stack (102) and the at least one optical element
(112) to the sensor body (106).
10. The method of claim 9, wherein the at least one optical element (112) comprises at
least one of either a mirror or a window, the method further comprising:
applying the frit (104) around the at least one optical element (112) such that the
frit (104) will form a hermetic seal around the at least one opening (110) when the
frit (104) is heated and cooled.