CN201697539U - Adapter - Google Patents
Adapter Download PDFInfo
- Publication number
- CN201697539U CN201697539U CN2010201288634U CN201020128863U CN201697539U CN 201697539 U CN201697539 U CN 201697539U CN 2010201288634 U CN2010201288634 U CN 2010201288634U CN 201020128863 U CN201020128863 U CN 201020128863U CN 201697539 U CN201697539 U CN 201697539U
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- CN
- China
- Prior art keywords
- pin
- switch
- rubber body
- adapter
- shell
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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Abstract
The utility model discloses an adapter, which comprises a rubber body and a pin shell arranged in the rubber body, wherein the pin shell is provided with a pin cover, a pin is arranged in the middle of the pin cover, a spring is arranged between the pin and the pin shell, a switch is arranged in a bottom groove of the pin shell, and the switch is connected with a buzzer arranged on the rubber body via conducting wires. The switch is arranged in the bottom groove of the pin shell, when pin disengagement and blockage of the adapter appear, the pin can be pressed towards the bottom of the pin shell under the action of the pressure of the outer wall of a guided missile to make a film key switch closed so as to switch on a pin disengagement alarm circuit, and the buzzer sends out alarm sound which can be heard clearly outside a cylinder, so necessary measures are taken to eliminate hidden launching safety hazards.
Description
Technical field
The utility model belongs to machine components, is specifically related to a kind of empty adapter of axial annular that is positioned at guided missile and launching tube.
Background technology
Adapter is arranged in the axial annular space of guided missile and launching tube, thereby be suspended on the body surface by pin-and-hole on the pin insertion bullet, the out of stock phenomenon of pin must not take place in adapter in tube, otherwise will constitute major hidden danger to emission security, at present, whether out of stockly behind the adapter fitted tube only can watch dual mode to judge, lack necessary measuring means and warning device and judge that whether adapter is out of stock, makes MISSILE LAUNCHING have potential safety hazard from theory analysis and part.
The utility model content
The technical problems to be solved in the utility model is to determine whether adapter is out of stock, provides a kind of and can accurately judge whether out of stock adapter.
The technical solution of the utility model realizes in the following manner:
A kind of adapter comprises rubber body and the pin boss that is arranged on rubber body inside, and pin boss is provided with pin cap, be provided with pin in the middle of the pin cap, be provided with spring between pin and the pin boss, be provided with switch in the pin boss kerve, switch links to each other with buzzer on being arranged on rubber body by lead.
Above-mentioned switch is the film key switch.
Above-mentioned pin boss sulfuration is in rubber body.
The utility model is provided with switch in the pin boss kerve, when out of stock catching phenomenon takes place in adapter, pin will be pressed to the pin boss bottom under the pressure effect of guided missile outer wall, make the film key switch closure, thereby connect out of stock warning circuit, make buzzer send chimes of doom, and hear chimes of doom in that the tube external enwergy is clear, thereby take the necessary measures to eliminate emission security hidden danger.
Description of drawings
Accompanying drawing is a structural representation of the present utility model.
The specific embodiment
As shown in drawings, the utility model comprises rubber body 1 and is arranged on the pin boss 2 of rubber body 1 inside, pin boss 2 is provided with pin cap 6, be provided with pin 3 in the middle of the pin cap 6, be provided with spring 4 between pin 3 and the pin boss 2, be provided with switch 5 in pin boss 2 kerves, switch 5 links to each other with buzzer 8 on being arranged on rubber body 1 by lead 7.Described switch 5 is film key switches, and described pin boss 2 sulfurations are in rubber body 1.
In the utility model, switch 5 is fixed in the groove of pin boss 2 bottom surfaces, and pin boss 2 is fixed in the damping adapter rubber body 1 by sulfuration, and buzzer 8 is adhesively fixed in the groove of rubber body 1 sidewall.Link to each other by the lead 7 that runs through damping adapter rubber body 1 between film key switch 5 and the buzzer 8, when out of stock catching phenomenon takes place in adapter, pin 3 will be pressed to pin boss 2 bottoms under the pressure effect of guided missile outer wall, make film key switch 5 closures, thereby connect out of stock warning circuit, make buzzer 8 send chimes of doom, and hear chimes of doom in that the tube external enwergy is clear, thereby take the necessary measures to eliminate emission security hidden danger.
Claims (3)
1. adapter, comprise rubber body (1) and be arranged on the inner pin boss (2) of rubber body (1), pin boss (2) is provided with pin cap (6), be provided with pin (3) in the middle of the pin cap (6), be provided with spring (4) between pin (3) and the pin boss (2), it is characterized in that: be provided with switch (5) in pin boss (2) kerve, switch (5) links to each other with buzzer (8) on being arranged on rubber body (1) by lead (7).
2. adapter according to claim 1 is characterized in that: described switch (5) is the film key switch.
3. adapter according to claim 1 and 2 is characterized in that: described pin boss (2) vulcanizes in rubber body (1).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2010201288634U CN201697539U (en) | 2010-02-10 | 2010-02-10 | Adapter |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2010201288634U CN201697539U (en) | 2010-02-10 | 2010-02-10 | Adapter |
Publications (1)
Publication Number | Publication Date |
---|---|
CN201697539U true CN201697539U (en) | 2011-01-05 |
Family
ID=43398786
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2010201288634U Expired - Lifetime CN201697539U (en) | 2010-02-10 | 2010-02-10 | Adapter |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN201697539U (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105643947A (en) * | 2015-12-09 | 2016-06-08 | 上海复合材料科技有限公司 | Missile adapter co-curing molding technique |
CN105806151A (en) * | 2016-04-18 | 2016-07-27 | 中国运载火箭技术研究院 | Adjustable deviation type adapter structure |
CN110749233A (en) * | 2019-10-28 | 2020-02-04 | 上海机电工程研究所 | Honeycomb adapter and method of manufacture |
CN112729007A (en) * | 2020-12-03 | 2021-04-30 | 上海复合材料科技有限公司 | Missile adapter, forming process method thereof and missile launching device |
CN114111444A (en) * | 2021-10-26 | 2022-03-01 | 武汉高德红外股份有限公司 | Small-size adapter and guided missile emitter |
-
2010
- 2010-02-10 CN CN2010201288634U patent/CN201697539U/en not_active Expired - Lifetime
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105643947A (en) * | 2015-12-09 | 2016-06-08 | 上海复合材料科技有限公司 | Missile adapter co-curing molding technique |
CN105643947B (en) * | 2015-12-09 | 2017-12-15 | 上海复合材料科技有限公司 | A kind of guided missile adapter co-curing moulding process |
CN105806151A (en) * | 2016-04-18 | 2016-07-27 | 中国运载火箭技术研究院 | Adjustable deviation type adapter structure |
CN105806151B (en) * | 2016-04-18 | 2017-12-22 | 中国运载火箭技术研究院 | A kind of adjustable deviation type adapter structure |
CN110749233A (en) * | 2019-10-28 | 2020-02-04 | 上海机电工程研究所 | Honeycomb adapter and method of manufacture |
CN112729007A (en) * | 2020-12-03 | 2021-04-30 | 上海复合材料科技有限公司 | Missile adapter, forming process method thereof and missile launching device |
CN114111444A (en) * | 2021-10-26 | 2022-03-01 | 武汉高德红外股份有限公司 | Small-size adapter and guided missile emitter |
CN114111444B (en) * | 2021-10-26 | 2023-09-05 | 武汉高德红外股份有限公司 | Small-size adapter and guided missile launching device |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CX01 | Expiry of patent term | ||
CX01 | Expiry of patent term |
Granted publication date: 20110105 |