CN105173099B - A kind of airborne equipment fast assembly and disassembly mechanism - Google Patents
A kind of airborne equipment fast assembly and disassembly mechanism Download PDFInfo
- Publication number
- CN105173099B CN105173099B CN201510585292.4A CN201510585292A CN105173099B CN 105173099 B CN105173099 B CN 105173099B CN 201510585292 A CN201510585292 A CN 201510585292A CN 105173099 B CN105173099 B CN 105173099B
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- China
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- airborne equipment
- stop pin
- chute
- sliding shoe
- disassembly mechanism
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Abstract
Include the advancing slip motion block (5) and rear sliding shoe (3) on airborne equipment base (7) the present invention relates to one kind, also include front connector (6) and rear connectors (4) on airplane floor, the preceding chute (10) slided for advancing slip motion block (5) is provided with front connector (6), the rear chute (9) slided for rear sliding shoe (3) is provided with rear connectors (4), also include the stop pin (2) on airborne equipment, stop pin (2) is connected with handle, airborne equipment base (7) is provided with limited block (12), handle passes through limited block (12), back-moving spring (8) is provided between limited block (12) and stop pin (2), front connector (6) and/or rear connectors (4) are provided with the location hole (11) coordinated with stop pin (2).Simple structure of the present invention, easy to operate, practicality.Solve the problems, such as the fast assembling-disassembling airborne equipment when the multiple-tasks such as airborne, air-drop, rescue and relief work are performed.
Description
Technical field
The present invention relates to fast assembly and disassembly mechanism, more specifically to a kind of airborne equipment fast assembly and disassembly mechanism.
Background technology
The various equipment installed on aircraft are needed to be reliably connected with aircaft configuration, and traditional airborne equipment mounting means is used
Bolt or the realization of General guide rail matching thread structure, are required for general utility tool or simple specific purpose tool during installation and removal,
Such as aircarrier aircraft seat is mounted and dismounted by the standard rail on engine room floor, seat chair leg is slipped into standard during installation and is led
Rail, then tightens the stud of seat chair leg bottom using special hook spanner.Existing installing mechanism operation is wasted time and energy, and is being held
During the multiple-tasks such as row is airborne, air-drop, rescue and relief work, this kind of mechanism can not meet the requirement of quick response.
The content of the invention
The technical problem to be solved in the present invention is, there is provided a kind of airborne equipment fast assembly and disassembly mechanism.
The technical solution adopted for the present invention to solve the technical problems is：A kind of airborne equipment fast assembly and disassembly mechanism is constructed,
Including advancing slip motion block and rear sliding shoe on airborne equipment base, also including the front connector on airplane floor
And rear connectors, the preceding chute slided for advancing slip motion block is provided with the front connector, slided after confession is provided with the rear connectors
The rear chute that motion block is slided, also including the stop pin on airborne equipment, the stop pin is connected with handle, airborne equipment
Base is provided with limited block, and the handle passes through the limited block, back-moving spring, institute are provided between the limited block and stop pin
State front connector and/or rear connectors are provided with the location hole coordinated with the stop pin；Current sliding shoe and rear sliding shoe exist
When preceding chute and rear chute are moved into place, in the stop pin insertion location hole.
In such scheme, the cross section of the advancing slip motion block and rear sliding shoe is I-shaped.
In such scheme, the cross section of the preceding chute and rear chute is I-shaped.
In such scheme, the location hole is connected with the preceding chute and/or rear chute, and the stop pin is advancing slip with described
Motion block and/or rear sliding shoe are disposed adjacent.
Implement airborne equipment fast assembly and disassembly mechanism of the invention, have the advantages that：
When airborne equipment is installed, advancing slip motion block and rear sliding shoe are respectively fallen in the preceding chute of front connector and rear connectors
In rear chute, certain distance is then slided backward, stop pin can under the action of the spring automatically fall into determining on rear connectors
In the hole of position, airborne equipment is locked on airplane floor, realizes Fast Installation.
During dismounting airborne equipment, release lever is cocked, stop pin is also pulled up upwards simultaneously, and now advancing slip motion block is with after
Sliding shoe can be slided in preceding chute and rear chute, after airborne equipment entirety forward slip certain distance, directly can be connected in the past
Taken out in block and rear contiguous block, realize fast quick-detach.
Simple structure of the present invention, easy to operate, practicality.Solve and performing the multiple-tasks such as airborne, air-drop, rescue and relief work
When fast assembling-disassembling airborne equipment problem.
Brief description of the drawings
Below in conjunction with drawings and Examples, the invention will be further described, in accompanying drawing：
Fig. 1 is the structural representation of airborne equipment fast assembly and disassembly mechanism of the present invention；
Fig. 2 is the sectional view of airborne equipment fast assembly and disassembly mechanism of the present invention；
Fig. 3 is the schematic diagram of rear sliding shoe and rear connectors.
Specific embodiment
In order to be more clearly understood to technical characteristic of the invention, purpose and effect, now compare accompanying drawing and describe in detail
Specific embodiment of the invention.
As shown in Figure 1-Figure 3, airborne equipment fast assembly and disassembly mechanism of the present invention includes release lever 1, stop pin 2, rear slip
Block 3, rear connectors 4, advancing slip motion block 5, front connector 6, airborne equipment base 7, back-moving spring 8.
Advancing slip motion block 5 and rear sliding shoe 3 are arranged on airborne equipment base 7, and front connector 6 and rear connectors 4 are arranged on
On airplane floor.It is provided with front connector 6 in the preceding chute 10 slided for advancing slip motion block 5, rear connectors 4 and is provided with for rear sliding shoe
The 3 rear chutes 9 for sliding.The cross section of advancing slip motion block 5 and rear sliding shoe 3 is I-shaped, preceding chute 10 and rear chute 9 it is transversal
Face is I-shaped, can prevent the play of vertical direction.
Stop pin 2 is connected with handle, and airborne equipment base 7 is provided with limited block 12, and handle passes through limited block 12.Limited block
Back-moving spring 8 is provided between 12 and stop pin 2, front connector 6 and/or rear connectors 4 are provided with the positioning coordinated with stop pin 2
Hole 11.Location hole 11 is connected with preceding chute 10 and/or rear chute 9, and stop pin 2 is adjacent with advancing slip motion block 5 and/or rear sliding shoe 3
Set., when preceding chute 10 and rear chute 9 are moved into place, stop pin 2 inserts location hole 11 for current sliding shoe 5 and rear sliding shoe 3
It is interior.
When airborne equipment is installed, before advancing slip motion block 5 and rear sliding shoe 3 are respectively fallen in into front connector 6 and rear connectors 4
In chute 10 and rear chute 9, certain distance is then slided backward, stop pin 2 is connected after being automatically fallen into the presence of spring 8
In location hole 11 on part 4, airborne equipment is locked on airplane floor, realizes Fast Installation.
During dismounting airborne equipment, release lever 1 is cocked, stop pin 2 is also pulled up upwards simultaneously, now advancing slip motion block 5
Can be slided in preceding chute 10 and rear chute 9 with rear sliding shoe 3, after airborne equipment entirety forward slip certain distance, can be direct
Taken out in the past contiguous block and rear contiguous block, realize fast quick-detach.
Simple structure of the present invention, easy to operate, practicality.Solve and performing the multiple-tasks such as airborne, air-drop, rescue and relief work
When fast assembling-disassembling airborne equipment problem.
Embodiments of the invention are described above in conjunction with accompanying drawing, but the invention is not limited in above-mentioned specific
Implementation method, above-mentioned specific embodiment is only schematical, rather than restricted, one of ordinary skill in the art
Under enlightenment of the invention, in the case of present inventive concept and scope of the claimed protection is not departed from, can also make a lot
Form, these are belonged within protection of the invention.
Claims (4)
1. a kind of airborne equipment fast assembly and disassembly mechanism, it is characterised in that including installed in airborne equipment base（7）On front slide
Block（5）With rear sliding shoe（3）, also including the front connector on airplane floor（6）And rear connectors（4）, it is described before connect
Fitting（6）Inside it is provided with for advancing slip motion block（5）The preceding chute for sliding（10）, the rear connectors（4）Inside it is provided with for rear sliding shoe（3）
The rear chute for sliding（9）, also including the stop pin on airborne equipment（2）, the stop pin（2）It is connected with handle, machine
Carry plant bottom case（7）It is provided with limited block（12）, the handle pass through the limited block（12）, the limited block（12）With locking
Pin（2）Between be provided with back-moving spring（8）, the front connector（6）And/or rear connectors（4）It is provided with and the stop pin（2）
The location hole of cooperation（11）；Current sliding shoe（5）With rear sliding shoe（3）In preceding chute（10）With rear chute（9）When moving into place,
The stop pin（2）Insertion location hole（11）It is interior.
2. airborne equipment fast assembly and disassembly mechanism according to claim 1, it is characterised in that the advancing slip motion block（5）With it is rear
Sliding shoe（3）Cross section be I-shaped.
3. airborne equipment fast assembly and disassembly mechanism according to claim 1, it is characterised in that the preceding chute（10）With rear cunning
Groove（9）Cross section be I-shaped.
4. airborne equipment fast assembly and disassembly mechanism according to claim 1, it is characterised in that the location hole（11）With it is described
Preceding chute（10）And/or rear chute（9）Connection, the stop pin（2）With the advancing slip motion block（5）And/or rear sliding shoe（3）Phase
Neighbour is set.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510585292.4A CN105173099B (en) | 2015-09-15 | 2015-09-15 | A kind of airborne equipment fast assembly and disassembly mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510585292.4A CN105173099B (en) | 2015-09-15 | 2015-09-15 | A kind of airborne equipment fast assembly and disassembly mechanism |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105173099A CN105173099A (en) | 2015-12-23 |
| CN105173099B true CN105173099B (en) | 2017-05-31 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510585292.4A Active CN105173099B (en) | 2015-09-15 | 2015-09-15 | A kind of airborne equipment fast assembly and disassembly mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105173099B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106697310A (en) * | 2016-12-12 | 2017-05-24 | 太原航空仪表有限公司 | Quick-disassembly structure for aviation displayer |
| CN108891618A (en) * | 2018-07-06 | 2018-11-27 | 西安爱生技术集团公司 | A kind of quick dispatch mechanism of unmanned plane antenna house |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2787500Y (en) * | 2004-12-09 | 2006-06-14 | 武汉云鹤汽车座椅有限公司 | Automobile seat track mechanism |
| DE102008030640A1 (en) * | 2008-07-01 | 2010-01-07 | GE Fanuc Intelligent Platforms Embedded Systems, Inc. (n.d.Ges.d. Staates Delaware) | Fastening device for a housing in a receiving device |
| CN202110475U (en) * | 2011-05-13 | 2012-01-11 | 雅固拉国际精密工业(苏州)有限公司 | Tool-free installing front support of slide rail for server |
| CN103692930B (en) * | 2013-12-27 | 2015-12-09 | 中欧汽车股份有限公司 | A kind of caravan seat slide |
| CN204916205U (en) * | 2015-09-15 | 2015-12-30 | 航宇救生装备有限公司 | Airborne equipment quick assembly disassembly mechanism |
-
2015
- 2015-09-15 CN CN201510585292.4A patent/CN105173099B/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN105173099A (en) | 2015-12-23 |
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