CN107086382B - A kind of image storing mechanism that the fast insert-pull for aero remote sensor is locked - Google Patents
A kind of image storing mechanism that the fast insert-pull for aero remote sensor is locked Download PDFInfo
- Publication number
- CN107086382B CN107086382B CN201710290181.XA CN201710290181A CN107086382B CN 107086382 B CN107086382 B CN 107086382B CN 201710290181 A CN201710290181 A CN 201710290181A CN 107086382 B CN107086382 B CN 107086382B
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- fixed
- fixed bin
- memory
- plug
- storage dish
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
- H01R13/62—Means for facilitating engagement or disengagement of coupling parts or for holding them in engagement
- H01R13/629—Additional means for facilitating engagement or disengagement of coupling parts, e.g. aligning or guiding means, levers, gas pressure electrical locking indicators, manufacturing tolerances
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R12/00—Structural associations of a plurality of mutually-insulated electrical connecting elements, specially adapted for printed circuits, e.g. printed circuit boards [PCB], flat or ribbon cables, or like generally planar structures, e.g. terminal strips, terminal blocks; Coupling devices specially adapted for printed circuits, flat or ribbon cables, or like generally planar structures; Terminals specially adapted for contact with, or insertion into, printed circuits, flat or ribbon cables, or like generally planar structures
- H01R12/70—Coupling devices
- H01R12/71—Coupling devices for rigid printing circuits or like structures
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
- H01R13/62—Means for facilitating engagement or disengagement of coupling parts or for holding them in engagement
- H01R13/627—Snap or like fastening
Landscapes
- Mounting Of Printed Circuit Boards And The Like (AREA)
Abstract
The present invention relates to a kind of image storing mechanism that the fast insert-pull for aero remote sensor is locked, which includes that memory inserts disk component, memory housing unit and memory plug component；The memory inserts the two upper lateral part fixing bearing sleeve connections that two guiding axis in disk component pass through bearing and supporting case respectively, and knob is fixed on the top of guiding axis；Storage dish plug is clamped in inside supporting case；Two upper lateral part of fixed bin is fixed with outline border in memory housing unit, and guide pin is fixed on the two sides of the bottom of fixed bin；Two guiding axis are respectively inserted into the outline border of fixed bin two sides；On the fixed assist side bracket of storage dish socket；Fixed bin is connected with route board mount and passes through guiding finger setting；Storage dish plug is connect with storage dish socket by socket.Structure of the invention is relatively easy, there is enough strength and stiffness, and there are also very high reset and alignment precisions.
Description
Technical field:
The invention belongs to aerial photography technical fields, are related to a kind of image storing mechanism for aero remote sensor.
Background technique:
When aero remote sensor is taken a picture in the sky, different air-flows, atmospheric pressure and different aspects can all make to navigate
Empty remote sensor generates greatly vibration and can connect between image storage apparatus and aero remote sensor fuselage when shaking excessive
Bad phenomenon is touched, the image obtained is lost so as to cause aero remote sensor, or even the image of acquisition can not be stored.Air remote sensing
Device, if obtaining the overlong time of image, will greatly reduce the effective of image information when completing to obtain the task of image
Property, in order to obtain effective target information, and the aerial mission of quick execution next time as soon as possible, need to aero remote sensor
Image storage apparatus realizes fast insert-pull.To guarantee quickly and effectively to obtain image information, it is necessary to which designing one kind can be realized tightly
Gu and the image storing mechanism of fast insert-pull.
The function that common image storing mechanism is not provided simultaneously with fast insert-pull and fastens, image information transmission is slow,
Under great vibration environment, it is easy to which the phenomenon that generating poor contact influences to obtain image information.According to the spy of aero remote sensor
Point invents a kind of image storing mechanism, realizes fastening and fast insert-pull by helicitic texture, and structure is relatively easy, high reliablity,
It can be good at the requirement for meeting image storage.
Summary of the invention:
The technical problem to be solved in the present invention is to provide one kind can be realized image storage apparatus fast insert-pull and fastening, and
And when storage dish is docked with wiring board, resiliency is good, can prevent that storage dish under great vibration environment from loosening for aviation
The image storing mechanism of the fast insert-pull locking of remote sensor,.
In order to solve the above-mentioned technical problem, the image that the fast insert-pull for aero remote sensor of the invention is locked stores machine
Structure, including memory insert disk component, memory housing unit and memory plug component；It includes handle that the memory, which inserts disk component,
Hand, supporting case, knob, guiding axis；Handle is fixed on supporting case；Two upper lateral parts of supporting case are fixed with bearing sleeve, and two
Guiding axis passes through bearing respectively and connect with two bearing sleeves, and knob is fixed on the top of guiding axis；Storage dish plug is logical
Support component is crossed to be clamped in inside supporting case；Memory housing unit includes fixed bin and the guiding for being fixed on its two sides of the bottom
Pin；Two upper lateral part of fixed bin is fixed with outline border, and guide pin is fixed on the two sides of the bottom of fixed bin；Two guiding axis are respectively inserted into
In the outline border of fixed bin two sides, one of guiding axis is threadedly coupled with corresponding outline border；Memory plug component includes storage
Disk socket, route board mount；On the fixed assist side bracket of storage dish socket；Fixed bin is connected by screw with route board mount
And pass through guiding finger setting；Storage dish plug is connect with storage dish socket by socket；The two sides of the route board mount have
There is through-hole；Two sides via bottoms are threadedly coupled hold-down column；Pressure spring is located at the upper surface of hold-down column in through-hole, and the top of pressure spring is sleeved on
Pre-tighten column lower position, pre-tighten column on have one at position limiting convex ring, the position limiting convex ring be located at through-hole upper inner shoulder and
Between pressure spring.
The front end panel and backboard that the supporting case is fixedly connected by both sides of the edge are constituted.
There is shoulder on the inside of the fixed bin front pressuring plate；Banking pin is fixed on the two sides of front end panel on backboard, and is located at back
In gap between plate and fixed bin front pressuring plate above shoulder.
The support component includes storage dish circuit board, the first heat conductive insulating pad and the second heat conductive insulating pad；Storage dish is inserted
Head be fixed on storage dish circuit board, storage dish circuit board by be located at its front and back the first heat conductive insulating pad and
Second heat conductive insulating pad is clamped in supporting case.
The fixed bin front pressuring plate and fixed bin backboard that the fixed bin is fixedly connected by both sides of the edge are constituted.
Fixed bin end cap is fixed at the top of the fixed bin.
Bulge loop is all had on described two guiding axis；Position below the bulge loop of one of guiding axis has external screw thread；It is convex
Ring is between bearing sleeve and outline border.
The storage dish socket is made of the memory plug plug of wiring board and welding in the circuit board；Wiring board is fixed
Before assist side bracket；Circuit board platen is clamped between route board mount and wiring board, and wiring board pressure pad, which is mounted on, to be deposited
In reservoir socket plug, and it is connect by screw with wiring board；Heat conductive insulating pad clamps assist side pressure pad and memory plug
Among plug.
In use, memory housing unit and memory plug component link together, it is distant to be installed to aviation by screw
On sensor, disk component is inserted by plug memory, realizes the transmission of image, has this multiple mechanism or multiple memories to insert disk group
When part, each memory is inserted can be interchanged between disk component, and versatility is good.
The present invention can be connected firmly using helicitic texture by frictional force fastener guarantee inter-module, utilize the guiding of guiding axis
Effect guarantees inter-module with correct position relative motion.When only one guiding axis is threadedly coupled with outline border, rotates this and lead
It can be achieved with the rotation of the guiding axis to the knob at the top of axis, realize fast insert-pull.It can be protected using the reset response of guide pin
Relative position is constant when demonstrate,proving inter-module dismounting, to guarantee the alignment precision of storage dish and wiring board；The two of assist side bracket
Installation hold-down column, pressure spring and preload column, can play buffer function, simultaneously when storage dish is docked with wiring board in the through-hole of side
The effect for also functioning to preload prevents storage dish under great vibration environment from loosening.Structure of the invention is relatively easy, has enough strong
Degree and rigidity, there are also very high reset and alignment precisions.
Detailed description of the invention:
Invention is further described in detail with reference to the accompanying drawings and detailed description.
Fig. 1 is the image storing mechanism that the fast insert-pull for aero remote sensor of the invention is locked, structural schematic diagram.
Fig. 2 is the sectional view along A-A of Fig. 1.
Fig. 3 is the image storing mechanism that the fast insert-pull for aero remote sensor of the invention is locked, structural front view.
Fig. 4 a is the C-C of Fig. 3 to cross-sectional view, and Fig. 4 b is L-L to cross-sectional view, and Fig. 4 c is the partial enlarged view of Fig. 4 b.
Fig. 5 is that memory inserts disk component diagram in the present invention.
Fig. 6 is the B-B direction cross-sectional view of Fig. 5.
Fig. 7 is memory housing unit schematic diagram in the present invention.
Fig. 8 is memory plug component diagram in the present invention.
Fig. 9 a is the sectional view along A-A of Fig. 8, and Fig. 9 b is the C-C of Fig. 9 a to cross-sectional view.
Figure 10 is the B-B direction cross-sectional view of Fig. 8.
Figure 11 a is the top view of memory plug component 3, and Figure 11 b is that the image for aero remote sensor of the invention is deposited
Store up mechanism structure bottom view.
Specific embodiment:
As shown in Figure 1, the image storing mechanism that the fast insert-pull for aero remote sensor of the invention is locked, comprising: deposit
Reservoir is inserted disk component 1, memory housing unit 2 and memory plug component 3 and is formed.
As shown in Figure 1,5, it includes handle 11, supporting case 12, knob 131, guiding axis 132 that the memory, which inserts disk component 1,；
Handle 11 is fixed on supporting case 12；Two upper lateral parts of supporting case 12 are fixed with bearing sleeve 121, and two guiding axis 132 are distinguished
It is connect by bearing 1211 with two bearing sleeves 121, knob 131 is fixed on the top of guiding axis 132 by screw.Such as
Shown in Fig. 2, front end panel 122 and backboard 123 are fixed together by the screw of both sides of the edge and constitute supporting case 12；Storage dish is inserted
First 140 are fixed on storage dish circuit board 141, and storage dish circuit board 141 is led by being located at the first of its front and back
Thermal insulation pad 142 and the second heat conductive insulating pad 143 are clamped in supporting case 12, and storage dish plug 140 is located at supporting case 12
Inside, below front end panel 122.Two of them guiding axis 132, using stainless steel material, quenching and tempering hardness is 28~32HRC；Four
A bearing 1211 uses P4 grades of angular contact ball bearings；Supporting case 12 uses superhard aluminum material, and does stabilization processes.
As shown in Fig. 2,3,4a, 6, the memory housing unit 2 includes: fixed bin and is fixed on leading for its two sides of the bottom
To pin 25；Fixed bin front pressuring plate 23 and fixed bin backboard 24 are fixed together by the screw of both sides of the edge constitutes fixed bin；Gu
Determining two upper lateral part of box has integrally fixed outline border 22, and fixed bin end cap 21 is fixed at the top of fixed bin；Guide pin 25 passes through spiral shell
Line connection type or interference fit type are fixed on the two sides of the bottom of fixed bin.Guide pin 25 does Passivation Treatment；Fixed bin end cap
21 use stainless steel material, and quenching and tempering hardness is 28~32HRC；Fixed bin front pressuring plate 23, outline border 22 and fixed bin end cap 21 use
Superhard aluminum material, wherein fixed bin front pressuring plate 23 and outline border 22 do stabilization processes.
As shown in Fig. 4 b, 4c, there is shoulder 231 on the inside of the fixed bin front pressuring plate 23；Banking pin 6 is fixed on backboard 123
The two sides of front end panel 122, and between backboard 123 and fixed bin front pressuring plate 23 in the gap of 231 top of shoulder.When will deposit
When the slotting disk component 1 of reservoir is installed to memory housing unit 2, banking pin 6 is in the gap of 23 top of shoulder, if memory
The installation direction for inserting disk component 1 is incorrect, is stuck in admittedly due to without shoulder, then will lead to banking pin 6 on the inside of fixed bin backboard 24
It on the upper surface for determining box backboard 24, can not continue into, therefore the Anti-misplug function that memory inserts disk component 1 may be implemented.Such as
Fruit does not have Anti-misplug function, then will lead to storage dish plug 140 cannot be inserted into memory plug plug 314, even results in storage
Disk plug 140 and memory plug plug 314 damage.
When storage dish plug 140 is inserted or pull out memory plug plug 314, due to needing 3.6kg between the two
Pressure or pulling force, cause to have some setbacks when plug, therefore design guiding axis 132 and be threadedly coupled with outline border 22, screw thread knot when plug
Pressure required for structure can provide or pulling force, therefore only need to rotate helicitic texture, it will be able to it realizes and easily quickly inserts
It pulls out.
Bulge loop 1321 is all had on described two guiding axis 132；1321 or less the position of bulge loop of one of guiding axis 132
With external screw thread.Bulge loop 1321 is between bearing sleeve 121 and outline border 22.
When the slotting disk component 1 of memory is mounted on memory housing unit 2, supporting case 12 is inserted in fixed bin, wherein
One guiding axis 132 is threadedly coupled with outline border 22, another guiding axis 132 is passed through by the through-hole on corresponding outline border 22.Rotation rotation
Button 131, driving guiding axis 132, which rotates, can be completed the assembly and disassembly that memory inserts disk component 1, and pass through the guiding of guiding axis 132
Effect, it is ensured that storage dish plug 140 is connected with wiring board 31 on memory plug component 3 with correct position.
As shown in Fig. 8,9a, 9b, 10,11a, 11b, the memory plug component includes circuit board platen 311, route
Plate pressure pad 312, heat conductive insulating pad 313, memory plug plug 314, wiring board 315, route board mount 32, hold-down column 321, pressure
Spring 322 pre-tightens the composition of column 323；Wherein memory plug plug 314 welds is constituted in assist side 315 with wiring board 315 together
Storage dish socket；Before the fixed assist side bracket 32 of screw that wiring board 315 passes through both sides of the edge；Circuit board platen 311
It is clamped between route board mount 32 and wiring board 315, plays the role of fixed (being welded to route to the electric wire on wiring board 315
The solder joint of electric wire on plate 315 here, therefore is clamped with circuit board platen 311)；Wiring board pressure pad 312 is mounted on storage
It in device socket plug 314, and is connect by screw with wiring board 315, plays the role of reinforcing to memory plug plug 314,
Prevent 314 stress of memory plug plug from falling off；Heat conductive insulating pad 313 clamps assist side pressure pad 312 and memory plug is inserted
Among first 314.The two sides of route board mount 32 have through-hole 324；Two side through hole, 324 bottom thread connects hold-down column 321；Pressure spring
322 are located at the upper surface of hold-down column 321 in through-hole 324, and the top of pressure spring 322 is sleeved on the lower position for pre-tightening column 323, pre-tighten column
There is position limiting convex ring 3231 at one, which is located at the shoulder 3241 and pressure spring of 324 upper inner of through-hole on 323
Between 322.
Memory housing unit 2 is mounted on memory plug component 3, is connected by guide pin 25 and screw, is guaranteed
The relative position of memory housing unit 2 and memory plug component 3 is constant.Storage dish plug 140 passes through with storage dish socket
Socket connection.
Route board mount (23) uses superhard aluminum material, does stabilization processes.
Claims (8)
1. a kind of image storing mechanism that the fast insert-pull for aero remote sensor is locked, it is characterised in that insert disk including memory
Component (1), memory housing unit (2) and memory plug component (3)；It includes handle that the memory, which inserts disk component (1),
(11), supporting case (12), knob (131), guiding axis (132)；Handle (11) is fixed on supporting case (12)；Supporting case (12)
Two upper lateral parts are fixed with bearing sleeve (121), and two guiding axis (132) pass through bearing (1211) and two bearing sleeves respectively
(121) it connects, knob (131) is fixed on the top of guiding axis (132)；Storage dish plug (140) is pressed from both sides by support component
It is tightly internal in supporting case (12)；Memory housing unit (2) includes fixed bin and the guide pin (25) for being fixed on its two sides of the bottom；
Fixed bin front pressuring plate (23) and fixed bin backboard (24) are fixed together by the screw of both sides of the edge and constitute fixed bin；Fixed bin
Two upper lateral parts are fixed with outline border (22), and guide pin (25) is fixed on the two sides of the bottom of fixed bin；Two guiding axis (132) are inserted respectively
Enter in the outline border (22) of fixed bin two sides, one of guiding axis (132) is threadedly coupled with corresponding outline border (22)；Memory
Jack assemblies include storage dish socket, route board mount (32)；On storage dish socket fixed assist side bracket (32)；Fixed bin
It is connected by screw with route board mount (32) and is positioned by guide pin (25)；Storage dish plug (140) and storage dish socket
It is connected by socket；The two sides of the route board mount (32) have through-hole (324)；Two side through hole (324) bottom thread connects
Connect hold-down column (321)；Pressure spring (322) is located at the upper surface of through-hole (324) interior hold-down column (321), and the top of pressure spring (322) is sleeved on
The lower position of column (323) is pre-tightened, pre-tightening has position limiting convex ring (3231) at one, position limiting convex ring (3231) position on column (323)
Between the shoulder (3241) and pressure spring (322) of through-hole (324) upper inner.
2. the image storing mechanism that the fast insert-pull according to claim 1 for aero remote sensor is locked, feature exist
The front end panel (122) and backboard (123) being fixedly connected by both sides of the edge in the supporting case (12) are constituted.
3. the image storing mechanism that the fast insert-pull according to claim 2 for aero remote sensor is locked, feature exist
There are shoulder (231) on the inside of the fixed bin front pressuring plate (23)；Banking pin (6) is fixed on backboard (123), and is located at front support
The two sides of plate (122)；And banking pin (6) is located at the sky between backboard (123) and fixed bin front pressuring plate (23) above shoulder (231)
In gap.
4. the image storing mechanism that the fast insert-pull according to claim 1 for aero remote sensor is locked, feature exist
In the support component include storage dish circuit board (141), the first heat conductive insulating pad (142) and the second heat conductive insulating pad (143)；
Storage dish plug (140) is fixed on storage dish circuit board (141), and storage dish circuit board (141) is by being located at its front
It is clamped in supporting case (12) with the first heat conductive insulating pad (142) at the back side and the second heat conductive insulating pad (143).
5. the image storing mechanism that the fast insert-pull according to claim 1 for aero remote sensor is locked, feature exist
The fixed bin front pressuring plate (23) and fixed bin backboard (24) being fixedly connected by both sides of the edge in the fixed bin are constituted.
6. the image storing mechanism that the fast insert-pull according to claim 1 for aero remote sensor is locked, feature exist
Fixed bin end cap (21) are fixed at the top of the fixed bin.
7. the image storing mechanism that the fast insert-pull according to claim 1 for aero remote sensor is locked, feature exist
In all having bulge loop (1321) on described two guiding axis (132)；The bulge loop (1321) of one of guiding axis (132) is with bottom
It sets with external screw thread；Bulge loop (1321) is located between bearing sleeve (121) and outline border (22).
8. the image storing mechanism that the fast insert-pull according to claim 1 for aero remote sensor is locked, feature exist
It is made of in the storage dish socket the memory plug plug (314) on wiring board (315) and welding assist side (315)；
Before wiring board (315) fixed assist side bracket (32)；Circuit board platen (311) is clamped in route board mount (32) and line
Between road plate (315), wiring board pressure pad (312) is mounted on memory plug plug (314), and passes through screw and wiring board
(315) it connects；It is intermediate that heat conductive insulating pad (313) clamps assist side pressure pad (312) and memory plug plug (314).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710290181.XA CN107086382B (en) | 2017-04-28 | 2017-04-28 | A kind of image storing mechanism that the fast insert-pull for aero remote sensor is locked |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710290181.XA CN107086382B (en) | 2017-04-28 | 2017-04-28 | A kind of image storing mechanism that the fast insert-pull for aero remote sensor is locked |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107086382A CN107086382A (en) | 2017-08-22 |
| CN107086382B true CN107086382B (en) | 2019-03-05 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710290181.XA Active CN107086382B (en) | 2017-04-28 | 2017-04-28 | A kind of image storing mechanism that the fast insert-pull for aero remote sensor is locked |
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| CN (1) | CN107086382B (en) |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2228458A (en) * | 1989-02-24 | 1990-08-29 | Eric David Whybray | Flight data recorder ejector |
| CN1063182A (en) * | 1991-01-07 | 1992-07-29 | 张宁 | Rotay type safety plug device and method |
| CN2760812Y (en) * | 2004-10-28 | 2006-02-22 | 贵州南方汇通世华微硬盘有限公司 | Locking and pop-up device for storage product switching card |
| CN201414272Y (en) * | 2009-06-09 | 2010-02-24 | 北京国科环宇空间技术有限公司 | Large-capacity data recorder and fast plug-pull structure thereof |
| CN102426844A (en) * | 2011-12-16 | 2012-04-25 | 陕西千山航空电子有限责任公司 | Quick access recorder ejection mechanism |
| FR2960517B1 (en) * | 2010-05-27 | 2012-10-19 | Pierre Bansard | DEVICE FOR EJECTING BLACK BOXES EQUIPPED WITH A FLOTATION DEVICE. |
| CN203870527U (en) * | 2014-04-22 | 2014-10-08 | 凌华科技股份有限公司 | Swappable hard disk device |
| CN104464773A (en) * | 2014-11-04 | 2015-03-25 | 中国航天科工集团第三研究院第八三五七研究所 | Plugging device applied to data recording equipment |
| CN105489234A (en) * | 2015-12-07 | 2016-04-13 | 中国航空工业集团公司洛阳电光设备研究所 | Built-in plug device for storage disk of airborne recording device |
-
2017
- 2017-04-28 CN CN201710290181.XA patent/CN107086382B/en active Active
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2228458A (en) * | 1989-02-24 | 1990-08-29 | Eric David Whybray | Flight data recorder ejector |
| CN1063182A (en) * | 1991-01-07 | 1992-07-29 | 张宁 | Rotay type safety plug device and method |
| CN2760812Y (en) * | 2004-10-28 | 2006-02-22 | 贵州南方汇通世华微硬盘有限公司 | Locking and pop-up device for storage product switching card |
| CN201414272Y (en) * | 2009-06-09 | 2010-02-24 | 北京国科环宇空间技术有限公司 | Large-capacity data recorder and fast plug-pull structure thereof |
| FR2960517B1 (en) * | 2010-05-27 | 2012-10-19 | Pierre Bansard | DEVICE FOR EJECTING BLACK BOXES EQUIPPED WITH A FLOTATION DEVICE. |
| CN102426844A (en) * | 2011-12-16 | 2012-04-25 | 陕西千山航空电子有限责任公司 | Quick access recorder ejection mechanism |
| CN203870527U (en) * | 2014-04-22 | 2014-10-08 | 凌华科技股份有限公司 | Swappable hard disk device |
| CN104464773A (en) * | 2014-11-04 | 2015-03-25 | 中国航天科工集团第三研究院第八三五七研究所 | Plugging device applied to data recording equipment |
| CN105489234A (en) * | 2015-12-07 | 2016-04-13 | 中国航空工业集团公司洛阳电光设备研究所 | Built-in plug device for storage disk of airborne recording device |
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| CN107086382A (en) | 2017-08-22 |
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