Novel hinge closed-loop high-reliability piezoelectric fast reflecting mirror
By adopting hinge closed-loop structure and aerospace rubber buffering technology, the problem of piezoelectric fast mirrors being easily damaged and insufficient stability during use is solved, achieving higher stability and reliability and extending the service life of piezoelectric ceramic components .
Patent Information
- Application Number
- CN202411884322.7
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-20
- Publication Date
- 2025-02-18
- Estimated Expiration
- 2044-12-20
AI Technical Summary
Existing piezoelectric fast mirrors are easily damaged during use and are difficult to ensure stability and reliability. Especially when withstanding lateral forces, the service life of piezoelectric ceramic components is relatively short.
The hinge closed-loop structural design is adopted to form a whole, and through the combination of screw and disc spring, it provides stable support and adjustment force. At the same time, rubber injection holes are set in the shell, and aerospace glue is used for force buffering and protection.
It improves the stability and reliability of the piezoelectric fast mirror, extends the service life of the piezoelectric ceramic components, and ensures that the components can continuously maintain the stress buffering function when they withstand lateral forces.
Smart Images

Figure CN119472017A_ABST
Abstract
Description
Technical Field
[0001] The invention relates to the field of piezoelectric fast-reflecting mirrors, and more specifically to a novel hinged closed-loop high-reliability piezoelectric fast-reflecting mirror. Background Art
[0002] The piezoelectric fast mirror is a fast micro-nano angle positioning mechanism that uses piezoelectric ceramics as a driving source, and is used to control the direction of the light beam. It combines a variety of advanced technical theories such as high-precision angle measurement technology, micro-displacement drive technology, and advanced control theory, and greatly improves the pointing control accuracy, control bandwidth, and angle resolution compared to the traditional frame structure. The piezoelectric fast mirror is also commonly called a deflection mirror or a precision aiming mirror, and is an important component in the optical positioning and scanning system. Its moving surface has a clamping mechanism for installing a fixed load, which can drive the load for micro-angle adjustment, and can be integrated into various types of high-precision equipment to provide micro-radian motion control and optical path control. In the prior art, for example, a high-reliability piezoelectric deflection mirror for aerospace applications with an application number of 202110486560.2 provides a piezoelectric deflection mirror with enhanced mechanical properties of the entire structure, but is not suitable for providing a hinged closed-loop piezoelectric fast mirror adopts a hinged closed-loop structure and forms a whole, which is not easy to be damaged and improves the stability and reliability when using the fast mirror. Summary of the invention
[0003] The purpose of the present invention is to provide a novel hinged closed-loop high-reliability piezoelectric fast-reflection mirror. The invention can provide a hinged closed-loop piezoelectric fast-reflection mirror which adopts a hinged closed-loop structure and forms an integral body, which is not easy to be damaged and improves the stability and reliability when using the fast-reflection mirror.
[0004] The objective of the present invention is achieved through the following technical solutions: a novel hinged closed-loop high-reliability piezoelectric fast-reflection mirror, comprising a hinged closed-loop piezoelectric fast-reflection mirror, a base and a shell, wherein a plurality of screw rods I are evenly arranged along the circumferential direction on the outer side of the hinged closed-loop piezoelectric fast-reflection mirror, a display board is fixedly connected to the top of the shell, and a plurality of upwardly protruding connection seats are evenly arranged on the display board along the circumferential direction, a plurality of screw rods I pass through the outer edge of the hinged closed-loop piezoelectric fast-reflection mirror and are installed on the corresponding connection seats, and the hinged closed-loop piezoelectric fast-reflection mirror is synchronously fixedly installed on the display board, the bottom of the shell is fixedly connected to the base, a support rod is fixedly connected to the middle of the base, the top of the support rod extends into the hinged closed-loop piezoelectric fast-reflection mirror, a screw rod II is installed on the top of the support rod, a disc spring is sleeved in the middle of the screw rod II, and the lower side of the disc spring contacts the inner side of the middle of the hinged closed-loop piezoelectric fast-reflection mirror, four piezoelectric ceramic components are evenly arranged along the circumferential direction on the upper surface of the middle of the base, and the four piezoelectric ceramic components are evenly arranged in the shell along the circumferential direction.
[0005] Preferably, a protective cover is provided on the upper side of the display board, and a plurality of screw rods III are evenly provided inside the protective cover along the circumferential direction, and the bottoms of the plurality of screw rods III are fixedly mounted on corresponding connecting seats, thereby fixing the protective cover on the upper side of the display board.
[0006] Preferably, a plurality of glue injection holes are evenly arranged in the middle of the shell along the circumferential direction.
[0007] Preferably, a fitting ring is fixedly connected to the middle part of the outer side of the shell, and a plurality of corresponding holes are evenly arranged on the fitting ring along the circumferential direction, which correspond to the plurality of glue injection holes one by one. A sliding ring is slidingly fitted on the outer side of the fitting ring, and a limit rod is fixedly connected to the left and right sides of the bottom of the sliding ring respectively, and the two limit rods are slidably connected to the two sides of the fitting ring respectively.
[0008] Preferably, a plurality of injection tubes are evenly fixed and connected on the sliding ring along the circumferential direction, the plurality of injection tubes are arranged one by one corresponding to the plurality of corresponding holes on the fitting ring, the bottoms of the plurality of injection tubes are evenly fixed and connected to the upper side of the storage frame along the circumferential direction, and an extrusion ring is slidably connected inside the storage frame.
[0009] Preferably, each of the injection tubes is a plastic telescopic tube.
[0010] Preferably, a cover is installed on the upper right half of the storage frame.
[0011] Preferably, a push plate is fixedly connected to the bottom of the extrusion ring.
[0012] Beneficial effects:
[0013] 1. The hinged closed-loop piezoelectric fast-reflecting mirror adopts a hinged closed-loop structure and forms an integral body, which is not easy to be damaged and improves the stability and reliability when using the fast-reflecting mirror;
[0014] 2. It is convenient for the four piezoelectric ceramic components in the housing to buffer the lateral force to the maximum extent, thereby ensuring the normal usability of the overall structure while extending the service life of the piezoelectric ceramic components;.
[0015] 3. It is convenient to add aerospace glue to the inside of the shell in time so that the piezoelectric ceramic components can continuously maintain the force buffering function. ; BRIEF DESCRIPTION OF THE DRAWINGS
[0016] The present invention is further described in detail below with reference to the accompanying drawings and specific implementation methods.
[0017] Figure 1 It is a partial structural schematic diagram of the hinged closed-loop piezoelectric fast-reflecting mirror of the present invention;.
[0018] Figure 2It is a schematic diagram of the upward-view structure of the hinged closed-loop piezoelectric fast-reflecting mirror of the present invention;.
[0019] Figure 3 It is a partial structural schematic diagram of the base of the present invention;.
[0020] Figure 4 It is a cross-sectional schematic diagram of the hinged closed-loop piezoelectric fast-reflecting mirror of the present invention;.
[0021] Figure 5 It is a partial structural schematic diagram of the housing of the present invention;.
[0022] Figure 6 It is a partial structural schematic diagram of the display board of the present invention;.
[0023] Figure 7 It is a partial structural schematic diagram of the protective cover of the present invention;.
[0024] Figure 8 It is a schematic diagram of the structure of the protective cover of the present invention when viewed from above.
[0025] Fig. 9 It is a partial structural schematic diagram of the piezoelectric ceramic component of the present invention;.
[0026] Fig.10 It is a partial structural schematic diagram of the fitting ring of the present invention;.
[0027] Fig.11 It is a partial structural schematic diagram of the sliding ring of the present invention;.
[0028] Fig.12 It is a partial structural schematic diagram of the storage frame of the present invention;.
[0029] Fig.13 It is a partial structural schematic diagram of the extrusion ring of the present invention;.
[0030] Fig.14 It is a schematic diagram of the overall structure of a novel hinged closed-loop high-reliability piezoelectric fast-reflecting mirror of the present invention;.
[0031] Fig.15 It is a top view half-section structure schematic diagram of a housing and a protective cover in a novel hinged closed-loop high-reliability piezoelectric fast-reflecting mirror of the present invention;.
[0032] Fig.16 The present invention is a schematic diagram of a half-section structure of a housing and a protective cover in a novel hinged closed-loop high-reliability piezoelectric fast-reflecting mirror, viewed from above.
[0033] In the figure: hinged closed-loop piezoelectric fast-reflecting mirror 101; screw rod I 102; screw rod II 103; support rod 104; base 105; disc spring 106; housing 201; display board 202; connecting seat 203; injection hole 204; protective cover 301; screw rod III 302; piezoelectric ceramic component 401; fitting ring 501; sliding ring 601; injection tube 602; storage frame 603; limit rod 604; cover 605; extrusion ring 701; push plate 702. ; DETAILED DESCRIPTION
[0034] A novel hinged closed-loop high-reliability piezoelectric fast-reflecting mirror comprises a hinged closed-loop piezoelectric fast-reflecting mirror 101, a base 105 and a shell 201, wherein a plurality of screws Ⅰ102 are evenly arranged on the outer side of the hinged closed-loop piezoelectric fast-reflecting mirror 101 along the circumferential direction, a display board 202 is fixedly connected to the top of the shell 201, and a plurality of upwardly protruding connection seats 203 are evenly arranged on the display board 202 along the circumferential direction, a plurality of screws Ⅰ102 pass through the outer edge of the hinged closed-loop piezoelectric fast-reflecting mirror 101 and are installed on the corresponding connection seats 203, and the hinged closed-loop piezoelectric fast-reflecting mirror 101 is synchronously fixedly installed on the display board 20 2, the bottom of the housing 201 is fixedly connected to the base 105, the middle of the base 105 is fixedly connected with a support rod 104, the top of the support rod 104 extends into the hinged closed-loop piezoelectric fast-reflecting mirror 101, the top of the support rod 104 is installed with a screw rod II 103, the middle of the screw rod II 103 is sleeved with a disc spring 106, the lower side of the disc spring 106 is in contact with the inner side of the middle of the hinged closed-loop piezoelectric fast-reflecting mirror 101, the upper surface of the middle of the base 105 is evenly provided with four piezoelectric ceramic components 401 along the circumferential direction, and the four piezoelectric ceramic components 401 are evenly placed in the housing 201 along the circumferential direction.
[0035] This part is based on Figure 1-16The working process expressed in the figure is: in order to provide a new hinged closed-loop piezoelectric fast-reflecting mirror with high reliability, in the process of using the piezoelectric fast-reflecting mirror, when the light beam is irradiated to the upper surface of the hinged closed-loop piezoelectric fast-reflecting mirror 101, the two piezoelectric ceramic components 401 at any desired position, front and rear, or left and right sides, can be energized, and then the piezoelectric ceramic components 401 on both sides are pushed from the bottom surface of the hinged closed-loop piezoelectric fast-reflecting mirror 101 to make the surface of the hinged closed-loop piezoelectric fast-reflecting mirror 101 tilted, thereby adjusting the angle of refraction of the light beam, and the hinged closed-loop piezoelectric fast-reflecting mirror 101 is refracted. When the angle is adjusted, the disc spring 106 in the middle thereof which is sleeved on the middle part of the screw rod II 103 will be directional squeezed synchronously. Therefore, the elasticity of the disc spring 106 provides a restoring force for the hinged closed-loop piezoelectric quick response mirror 101 to return to its original position after the angle is adjusted. Then, wrapped by the overall shell 201 and the base 105, the hinged closed-loop piezoelectric quick response mirror 101 located above the shell 201 is made more stable and reliable. The hinged closed-loop piezoelectric quick response mirror 101 adopts a hinged closed-loop structure and forms a whole. While not being easily damaged, it improves the stability and reliability when using the quick response mirror.
[0036] A protective cover 301 is provided on the upper side of the display board 202 , and a plurality of screw rods III 302 are evenly provided inside the protective cover 301 along the circumferential direction. The bottoms of the plurality of screw rods III 302 are fixedly mounted on the corresponding connecting seats 203 , thereby fixing the protective cover 301 on the upper side of the display board 202 .
[0037] This part is based on Figure 1-16 The working process expressed therein is: to ensure the complete stability of the overall structure, the protective cover 301 is fastened and installed on the multiple connecting seats 203 on the display board 202 through multiple screws III 302, and the protective cover 301 covers the outer circumferential position of the hinged closed-loop piezoelectric fast reflection mirror 101, and the middle refracted light beam position of the hinged closed-loop piezoelectric fast reflection mirror 101 is located at the middle opening of the protective cover 301.
[0038] The middle portion of the housing 201 is evenly provided with a plurality of glue injection holes 204 along the circumferential direction.
[0039] This part is based on Figure 1-16The working process expressed therein is: in order to facilitate the four piezoelectric ceramic components 401 in the shell 201 to buffer the lateral force to the maximum extent, thereby ensuring the normal usability of the overall structure and extending the service life of the piezoelectric ceramic components 401, when in use, a plurality of glue injection holes 204 are evenly processed in the middle of the shell 201 along the circumferential direction, and then a certain amount of aerospace glue is injected into the shell 201 through the plurality of glue injection holes 204 through the operation of the production staff, so that the aerospace glue wraps the plurality of piezoelectric ceramic components 401 located in the shell 201, and after a period of time, the glue elastically solidifies, and when the four piezoelectric ceramic components 401 in the shell 201 are subjected to lateral force, the lateral force suffered by each piezoelectric ceramic component 401 is transmitted to the solidified colloid wrapped on the piezoelectric ceramic component 401, so that the force suffered by the piezoelectric ceramic component 401 is buffered to the maximum extent, thereby ensuring the structural stability of the piezoelectric ceramic component 401 and improving the service life of the piezoelectric ceramic component 401, and the overall structure is stable, so that the reliability is further improved.
[0040] A fitting ring 501 is fixedly connected to the middle part of the outer side of the shell 201, and a plurality of corresponding holes are evenly arranged on the fitting ring 501 along the circumferential direction, which are arranged one by one corresponding to the plurality of injection holes 204. A sliding ring 601 is slidingly fitted on the outer side of the fitting ring 501, and a limit rod 604 is fixedly connected to the left and right sides of the bottom of the sliding ring 601, respectively. The two limit rods 604 are slidably connected to the two sides of the fitting ring 501.
[0041] A plurality of injection tubes 602 are evenly fixed and connected on the sliding ring 601 along the circumferential direction. The plurality of injection tubes 602 are arranged one-to-one corresponding to the plurality of corresponding holes on the fitting ring 501. The bottoms of the plurality of injection tubes 602 are evenly fixed and connected to the upper side of the storage frame 603 along the circumferential direction. The storage frame 603 is internally slidably connected with an extrusion ring 701.
[0042] Each of the injection tubes 602 is a plastic telescopic tube.
[0043] A cover 605 is installed on the upper right half of the storage frame 603 .
[0044] A push plate 702 is fixedly connected to the bottom of the extrusion ring 701 .
[0045] This part is based on Figure 1-16The working process expressed therein is: the multiple piezoelectric ceramic components 401 located inside the shell 201 are subjected to lateral force for a long time, and after the solidified aerospace glue wrapped therein is squeezed and pushed, it is inevitable that the contact position between the internal colloid and the piezoelectric ceramic component 401 will undergo certain deformation, so as to facilitate the timely replenishment of aerospace glue into the shell 201 so that the piezoelectric ceramic component 401 can continuously maintain the force buffering function. When in use, first pull out the cover 605 inserted on the storage frame 603 with a heat preservation function, and inject glue into the space formed by the cover 605 and the extrusion ring 701 for storage. In the initial state, the sliding ring 601 slides to the lower side of the fitting ring 501 by means of two limit rods 604. At this time, the corresponding holes on the fitting ring 501 do not affect the initial operation through the corresponding holes. The corresponding glue injection holes 204 are used for glue injection, and when it is necessary to replenish glue, the sliding ring 601 is moved upward and the multiple injection tubes 602 are adaptively expanded and contracted synchronously, so that the upper end openings of the multiple injection tubes 602 located thereon correspond to the multiple corresponding holes on the fitting ring 501, and then the user grasps the pushing plate 702 and pushes the extrusion ring 701 toward the storage frame 603, and then the glue in the storage frame 603 is squeezed by the extrusion ring 701 and flows into the corresponding injection tubes 602, and then the glue flows through the injection tubes 602 so that the glue passes through the corresponding holes and the glue injection holes 204 and is injected into the outer shell 201, so that it is convenient to replenish the aerospace glue to the inside of the outer shell 201 in time, so that the piezoelectric ceramic component 401 can continuously maintain the force buffering function, and the overall structure is simple and practical.
[0046] Working principle:
[0047] This part is based on Figure 1-16The working process expressed in the figure is: in order to provide a new hinged closed-loop piezoelectric fast-reflecting mirror with high reliability, in the process of using the piezoelectric fast-reflecting mirror, when the light beam is irradiated to the upper surface of the hinged closed-loop piezoelectric fast-reflecting mirror 101, the two piezoelectric ceramic components 401 at any desired position, front and rear, or left and right sides, can be energized, and then the piezoelectric ceramic components 401 on both sides are pushed from the bottom surface of the hinged closed-loop piezoelectric fast-reflecting mirror 101 to make the surface of the hinged closed-loop piezoelectric fast-reflecting mirror 101 tilted, thereby adjusting the angle of refraction of the light beam, and the hinged closed-loop piezoelectric fast-reflecting mirror 101 is refracted. When the angle is adjusted, the disc spring 106 in the middle thereof which is sleeved on the middle part of the screw rod II 103 will be directional squeezed synchronously. Therefore, the elasticity of the disc spring 106 provides a restoring force for the hinged closed-loop piezoelectric quick response mirror 101 to return to its original position after the angle is adjusted. Then, wrapped by the overall shell 201 and the base 105, the hinged closed-loop piezoelectric quick response mirror 101 located above the shell 201 is made more stable and reliable. The hinged closed-loop piezoelectric quick response mirror 101 adopts a hinged closed-loop structure and forms a whole. While not being easily damaged, it improves the stability and reliability when using the quick response mirror.
[0048] This part is based on Figure 1-16 The working process expressed therein is: to ensure the complete stability of the overall structure, the protective cover 301 is fastened and installed on the multiple connecting seats 203 on the display board 202 through multiple screws III 302, and the protective cover 301 covers the outer circumferential position of the hinged closed-loop piezoelectric fast reflection mirror 101, and the middle refracted light beam position of the hinged closed-loop piezoelectric fast reflection mirror 101 is located at the middle opening of the protective cover 301.
[0049] This part is based on Figure 1-16 The working process expressed therein is: in order to facilitate the four piezoelectric ceramic components 401 in the shell 201 to buffer the lateral force to the maximum extent, thereby ensuring the normal usability of the overall structure and extending the service life of the piezoelectric ceramic components 401, when in use, a plurality of glue injection holes 204 are evenly processed in the middle of the shell 201 along the circumferential direction, and then a certain amount of aerospace glue is injected into the shell 201 through the plurality of glue injection holes 204 through the operation of the production staff, so that the aerospace glue wraps the plurality of piezoelectric ceramic components 401 located in the shell 201, and after a period of time, the glue elastically solidifies, and when the four piezoelectric ceramic components 401 in the shell 201 are subjected to lateral force, the lateral force suffered by each piezoelectric ceramic component 401 is transmitted to the solidified colloid wrapped on the piezoelectric ceramic component 401, so that the force suffered by the piezoelectric ceramic component 401 is buffered to the maximum extent, thereby ensuring the structural stability of the piezoelectric ceramic component 401 and improving the service life of the piezoelectric ceramic component 401, and the overall structure is stable, so that the reliability is further improved.
[0050] This part is based on Figure 1-16 The working process expressed therein is: the multiple piezoelectric ceramic components 401 located inside the shell 201 are subjected to lateral force for a long time, and after the solidified aerospace glue wrapped therein is squeezed and pushed, it is inevitable that the contact position between the internal colloid and the piezoelectric ceramic component 401 will undergo certain deformation, so as to facilitate the timely replenishment of aerospace glue into the shell 201 so that the piezoelectric ceramic component 401 can continuously maintain the force buffering function. When in use, first pull out the cover 605 inserted on the storage frame 603 with a heat preservation function, and inject glue into the space formed by the cover 605 and the extrusion ring 701 for storage. In the initial state, the sliding ring 601 slides to the lower side of the fitting ring 501 by means of two limit rods 604. At this time, the corresponding holes on the fitting ring 501 do not affect the initial operation through the corresponding holes. The corresponding glue injection holes 204 are used for glue injection, and when it is necessary to replenish glue, the sliding ring 601 is moved upward and the multiple injection tubes 602 are adaptively expanded and contracted synchronously, so that the upper end openings of the multiple injection tubes 602 located thereon correspond to the multiple corresponding holes on the fitting ring 501, and then the user grasps the pushing plate 702 and pushes the extrusion ring 701 toward the storage frame 603, and then the glue in the storage frame 603 is squeezed by the extrusion ring 701 and flows into the corresponding injection tubes 602, and then the glue flows through the injection tubes 602 so that the glue passes through the corresponding holes and the glue injection holes 204 and is injected into the outer shell 201, so that it is convenient to replenish the aerospace glue to the inside of the outer shell 201 in time, so that the piezoelectric ceramic component 401 can continuously maintain the force buffering function, and the overall structure is simple and practical.
Claims
1. A novel hinged closed-loop high-reliability piezoelectric fast-reflecting mirror, comprising a hinged closed-loop piezoelectric fast-reflecting mirror (101), a base (105) and a housing (201), characterized in that: A plurality of screw rods I (102) are evenly arranged along the circumferential direction on the outer side of the hinged closed-loop piezoelectric fast-reflecting mirror (101); a display board (202) is fixedly connected to the top of the housing (201); a plurality of upwardly protruding connection seats (203) are evenly arranged along the circumferential direction on the display board (202); a plurality of screw rods I (102) pass through the outer edge of the hinged closed-loop piezoelectric fast-reflecting mirror (101) and are installed on the corresponding connection seats (203); the hinged closed-loop piezoelectric fast-reflecting mirror (101) is synchronously fixedly installed on the display board (202); the bottom of the housing (201) is fixedly connected to the base (105); A support rod (104) is fixedly connected to the middle of the base (105), the top of the support rod (104) extends into the hinged closed-loop piezoelectric fast-reflecting mirror (101), a screw rod II (103) is installed on the top of the support rod (104), a disc spring (106) is sleeved in the middle of the screw rod II (103), the lower side of the disc spring (106) contacts the inner side of the middle of the hinged closed-loop piezoelectric fast-reflecting mirror (101), and four piezoelectric ceramic components (401) are evenly arranged along the circumferential direction on the upper surface of the middle of the base (105), and the four piezoelectric ceramic components (401) are evenly arranged in the outer shell (201) along the circumferential direction.
2. According to claim 1, the novel hinged closed-loop high-reliability piezoelectric fast-reflecting mirror is characterized by: A protective cover (301) is provided on the upper side of the display board (202), and a plurality of screw rods III (302) are evenly provided inside the protective cover (301) along the circumferential direction, and the bottoms of the plurality of screw rods III (302) are fixedly mounted on corresponding connecting seats (203), thereby fixing the protective cover (301) on the upper side of the display board (202).
3. The novel hinged closed-loop high-reliability piezoelectric fast-reflecting mirror according to claim 1 is characterized by: A plurality of glue injection holes (204) are evenly arranged in the middle of the shell (201) along the circumferential direction.
4. The novel hinged closed-loop high-reliability piezoelectric fast-reflecting mirror according to claim 3 is characterized by: A fitting ring (501) is fixedly connected to the middle part of the outer side of the housing (201), and a plurality of corresponding holes are evenly arranged on the fitting ring (501) along the circumferential direction, and are arranged one-to-one with the plurality of glue injection holes (204). A sliding ring (601) is slidably fitted on the outer side of the fitting ring (501), and a limiting rod (604) is fixedly connected to the left and right sides of the bottom of the sliding ring (601), respectively, and the two limiting rods (604) are slidably connected to the two sides of the fitting ring (501).
5. The novel hinged closed-loop high-reliability piezoelectric fast-reflecting mirror according to claim 4 is characterized by: A plurality of injection tubes (602) are evenly fixed and connected to the sliding ring (601) along the circumferential direction. The plurality of injection tubes (602) are arranged in one-to-one correspondence with the plurality of corresponding holes on the fitting ring (501). The bottoms of the plurality of injection tubes (602) are evenly fixed and connected to the upper side of the storage frame (603) along the circumferential direction. The storage frame (603) is slidably connected to an extrusion ring (701) inside.
6. The novel hinged closed-loop high-reliability piezoelectric fast-reflecting mirror according to claim 5 is characterized by: Each of the injection tubes (602) is a plastic telescopic tube.
7. The novel hinged closed-loop high-reliability piezoelectric fast-reflecting mirror according to claim 6 is characterized by: A cover (605) is installed on the upper right half of the storage frame (603).
8. The novel hinged closed-loop high-reliability piezoelectric fast-reflecting mirror according to claim 7 is characterized by: A push plate (702) is fixedly connected to the bottom of the extrusion ring (701).
Citation Information
Patent Citations
High-reliability piezoelectric deflection mirror for aerospace application
CN113219649A
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CN112346238A
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CN115079402A