CN104816830A - Micro explosion type helicopter window glass jettisoning device - Google Patents
Micro explosion type helicopter window glass jettisoning device Download PDFInfo
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- CN104816830A CN104816830A CN201510212190.8A CN201510212190A CN104816830A CN 104816830 A CN104816830 A CN 104816830A CN 201510212190 A CN201510212190 A CN 201510212190A CN 104816830 A CN104816830 A CN 104816830A
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Abstract
The invention belongs to the helicopter emergency escape technology, and relates to a micro explosion type helicopter window glass jettisoning device. The micro explosion type helicopter window glass jettisoning device is characterized by being composed of a first manual exploder (1), a second manual exploder (2), a third manual exploder (3), a first two input and one output blasting fuse connector (5), a one input and two output blasting fuse connector (4), a second two input and one output blasting fuse connector (6), a first cutting fuse connector (7), a second cutting fuse connector (8), a first cutting fuse (18), a second cutting fuse (19), first left front jettisoning glass (9) and left rear jettisoning glass (10). The micro explosion type helicopter window glass jettisoning device simplifies structure, reduces the weight, improves work stability, avoids breakdown generated due to the fact that glass accidentally breaks away in an aerial flight, eliminates hidden safety dangers, and additionally shortens jettisoning operation time, and achieves a one key control and simultaneous jettisoning function.
Description
Technical field
The invention belongs to helicopter aircraft emergency escape technology, relate to the throwing of a kind of helicopter window-glass and put device.
Background technology
Window-glass throw put device as the important emergency facility of emergency escape channel in helicopter, when helicopter occur major failure time, occupant should open the window within the very first time glass throw put device escape.Current window-glass throwing is put device and is generally mechanical type throwing laying mechanism, mainly contains two kinds of forms: a kind of quick-release rope being push type principle and connecting, another kind is that sealing joint strip clamp structure is put in cross throwing.The quick-release rope shortcoming that push type principle connects is complex structure, Heavy Weight; It is job insecurity that sealing joint strip clamp structure shortcoming is put in cross throwing, and when often there is airflight, the fault that glass surprisingly departs from, exists potential safety hazard.Above-mentioned two kinds of helicopter windows throwing is put device and can only be realized single operation, and the operating time is long, can not realize a key control, throw the function of putting simultaneously.
Summary of the invention
The object of the invention is: propose the throwing of a kind of microexplosion formula helicopter window-glass and put device, so that simplified structure, expendable weight; The stability of raising work, when avoiding occurring airflight, the fault that glass surprisingly departs from, eliminates safe hidden trouble; In addition, shorten throwing and put the operating time, realize a key control, throw the function of putting simultaneously.
Technical scheme of the present invention is: a kind of microexplosion formula helicopter window-glass is thrown and put device, it is characterized in that: it enters one by the first manual firing device 1 to the 3rd manual firing device the 3, the 1 and goes out transfer cord joint 5, and enter two and go out transfer cord joint the 4, the 22 and enter one and go out the left front throwing of transfer cord joint 6, first flexible linear shaped charge joint 7, second flexible linear shaped charge joint 8, first flexible linear shaped charge 18, second flexible linear shaped charge 19, first and put glass 9 and left back throwing and put glass 10 and form; the mouth of the first manual firing device 1 is connected with one end of the first transfer cord 11, the other end and the one or two of the first transfer cord 11 enters a first input end outing transfer cord joint 5 and is connected, the mouth of the second manual firing device 2 is connected with one end of the second transfer cord 12, the other end and one of the second transfer cord 12 enters two input ends going out transfer cord joint 4 and is connected, one enters two the first mouths going out transfer cord joint 4 enters second input end outing transfer cord joint 5 by the 4th transfer cord 14 and the or two and is connected, one enters two the second mouths going out transfer cord joint 4 enters a first input end outing transfer cord joint 6 by the 5th transfer cord 15 and the two or two and is connected, the mouth of the 3rd manual firing device 3 is connected with one end of the 3rd transfer cord 13, the other end and the two or two of the 3rd transfer cord 13 enters second input end outing transfer cord joint 6 and is connected, one or two enters a mouth outing transfer cord joint 5 is connected by the input end of the 6th transfer cord 16 with the first flexible linear shaped charge joint 7, the mouth of the first flexible linear shaped charge joint 7 is connected with the first flexible linear shaped charge 18, first flexible linear shaped charge 18 puts the fixing of glass 9 border along left front throwing, two or two enters a mouth outing transfer cord joint 6 is connected by the input end of the 7th transfer cord 17 with the second flexible linear shaped charge joint 8, the mouth of the second flexible linear shaped charge joint 8 is connected with the second flexible linear shaped charge 19, second flexible linear shaped charge 19 puts the fixing of glass 10 border along left back throwing.
Advantage of the present invention is: propose the throwing of a kind of microexplosion formula helicopter window-glass and put device, simplify the structure, alleviate weight; Improve the stability of work, avoid when there is airflight, the fault that glass surprisingly departs from, eliminates potential safety hazard; In addition, shorten throwing and put the operating time, achieve a key control, throw the function of putting simultaneously.
Accompanying drawing explanation
Fig. 1 is principle schematic of the present invention.
Detailed description of the invention
Below the present invention is described in further details.See Fig. 1, a kind of microexplosion formula helicopter window-glass is thrown and is put device, it is characterized in that: it enters one by the first manual firing device 1 to the 3rd manual firing device the 3, the 1 and goes out transfer cord joint 5, and enter two and go out transfer cord joint the 4, the 22 and enter one and go out the left front throwing of transfer cord joint 6, first flexible linear shaped charge joint 7, second flexible linear shaped charge joint 8, first flexible linear shaped charge 18, second flexible linear shaped charge 19, first and put glass 9 and left back throwing and put glass 10 and form; the mouth of the first manual firing device 1 is connected with one end of the first transfer cord 11, the other end and the one or two of the first transfer cord 11 enters a first input end outing transfer cord joint 5 and is connected, the mouth of the second manual firing device 2 is connected with one end of the second transfer cord 12, the other end and one of the second transfer cord 12 enters two input ends going out transfer cord joint 4 and is connected, one enters two the first mouths going out transfer cord joint 4 enters second input end outing transfer cord joint 5 by the 4th transfer cord 14 and the or two and is connected, one enters two the second mouths going out transfer cord joint 4 enters a first input end outing transfer cord joint 6 by the 5th transfer cord 15 and the two or two and is connected, the mouth of the 3rd manual firing device 3 is connected with one end of the 3rd transfer cord 13, the other end and the two or two of the 3rd transfer cord 13 enters second input end outing transfer cord joint 6 and is connected, one or two enters a mouth outing transfer cord joint 5 is connected by the input end of the 6th transfer cord 16 with the first flexible linear shaped charge joint 7, the mouth of the first flexible linear shaped charge joint 7 is connected with the first flexible linear shaped charge 18, first flexible linear shaped charge 18 puts the fixing of glass 9 border along left front throwing, two or two enters a mouth outing transfer cord joint 6 is connected by the input end of the 7th transfer cord 17 with the second flexible linear shaped charge joint 8, the mouth of the second flexible linear shaped charge joint 8 is connected with the second flexible linear shaped charge 19, second flexible linear shaped charge 19 puts the fixing of glass 10 border along left back throwing.
Principle of work of the present invention is: when needs throwing put left front throwing put glass 9 time, by the first manual firing device 1, pass to the one or two by the first transfer cord 11 and enter the first input end that goes out transfer cord joint 5, enter a mouth outing transfer cord joint 5 by the one or two again and light the 6th transfer cord 16, be delivered to the first flexible linear shaped charge joint 7 and open quick-fried first flexible linear shaped charge 18, glass is put in left front throwing and blows.When needs throwing put left back throwing put glass 10 time, by the 3rd manual firing device 3, pass to the two or two by the 3rd transfer cord 13 and enter the first input end that goes out transfer cord joint 6, enter a mouth outing transfer cord joint 6 by the two or two again and light the 7th transfer cord 17, be delivered to the second flexible linear shaped charge joint 8 and open quick-fried second flexible linear shaped charge 19, glass is put in left back throwing and blows.When needs throw simultaneously put left front throwing put glass 9 and left back throwing put glass 10 time, by the second manual firing device 2, pass to one by the second transfer cord 12 and enter the input end that two go out transfer cord joint 4, enter two two mouths going out transfer cord joint 4 by one again and light the 6th transfer cord 16 and the 7th transfer cord 17 simultaneously, open quick-fried first flexible linear shaped charge 18 and the second flexible linear shaped charge 19 simultaneously, left front throwing is put glass and left back throwing and put glass and blow.
One embodiment of the present of invention, the adopt first manual firing device, two enters one and goes out that transfer cord joint, enters two to go out transfer cord joint, flexible linear shaped charge joint 7, second flexible linear shaped charge joint, flexible linear shaped charge are thrown and put glass and be finished parts.
Claims (1)
1. microexplosion formula helicopter window-glass is thrown and is put a device, it is characterized in that: it enters one by the first manual firing device (1) to the 3rd manual firing device (3), the or two and goes out transfer cord joint (5), and enter two and go out transfer cord joint (4), the two or two and enter that one goes out transfer cord joint (6), glass (9) is put in the first flexible linear shaped charge joint (7), the second flexible linear shaped charge joint (8), the first flexible linear shaped charge (18), the second flexible linear shaped charge (19), the first left front throwing and left back throwing is put glass (10) and formed; the mouth of the first manual firing device (1) is connected with one end of the first transfer cord (11), the other end and the one or two of the first transfer cord (11) enters a first input end outing transfer cord joint (5) and is connected, the mouth of the second manual firing device (2) is connected with one end of the second transfer cord (12), the other end and one of the second transfer cord (12) enters two input ends going out transfer cord joint (4) and is connected, one enters two the first mouths going out transfer cord joint (4) enters second input end outing transfer cord joint (5) by the 4th transfer cord (14) and the or two and is connected, one enters two the second mouths going out transfer cord joint (4) enters a first input end outing transfer cord joint (6) by the 5th transfer cord (15) and the two or two and is connected, the mouth of the 3rd manual firing device (3) is connected with one end of the 3rd transfer cord (13), the other end and the two or two of the 3rd transfer cord (13) enters second input end outing transfer cord joint (6) and is connected, one or two enters a mouth outing transfer cord joint (5) is connected with the input end of the first flexible linear shaped charge joint (7) by the 6th transfer cord (16), the mouth of the first flexible linear shaped charge joint (7) is connected with the first flexible linear shaped charge (18), first flexible linear shaped charge (18) puts the fixing of glass (9) border along left front throwing, two or two enters a mouth outing transfer cord joint (6) is connected with the input end of the second flexible linear shaped charge joint (8) by the 7th transfer cord (17), the mouth of the second flexible linear shaped charge joint (8) is connected with the second flexible linear shaped charge (19), second flexible linear shaped charge (19) puts the fixing of glass (10) border along left back throwing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510212190.8A CN104816830A (en) | 2015-04-29 | 2015-04-29 | Micro explosion type helicopter window glass jettisoning device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510212190.8A CN104816830A (en) | 2015-04-29 | 2015-04-29 | Micro explosion type helicopter window glass jettisoning device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104816830A true CN104816830A (en) | 2015-08-05 |
Family
ID=53727362
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510212190.8A Pending CN104816830A (en) | 2015-04-29 | 2015-04-29 | Micro explosion type helicopter window glass jettisoning device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104816830A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110979697A (en) * | 2019-12-23 | 2020-04-10 | 中国航空工业集团公司沈阳飞机设计研究所 | Porthole emergency blasting folding, turning and throwing device |
| CN112173128A (en) * | 2020-09-25 | 2021-01-05 | 中国直升机设计研究所 | Splint hinge is with throwing vaulting pole device of putting |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3248072A (en) * | 1964-04-01 | 1966-04-26 | Mcdonnell Aircraft Corp | Underwater explosive effects attenuator |
| US3670998A (en) * | 1970-07-10 | 1972-06-20 | Us Air Force | Severance of polycarbonate material canopy transparency |
| US3885761A (en) * | 1974-03-05 | 1975-05-27 | Jet Research Center | Aircraft emergency egress system |
| US6027073A (en) * | 1997-07-18 | 2000-02-22 | Eurocopter | Window release system |
-
2015
- 2015-04-29 CN CN201510212190.8A patent/CN104816830A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3248072A (en) * | 1964-04-01 | 1966-04-26 | Mcdonnell Aircraft Corp | Underwater explosive effects attenuator |
| US3670998A (en) * | 1970-07-10 | 1972-06-20 | Us Air Force | Severance of polycarbonate material canopy transparency |
| US3885761A (en) * | 1974-03-05 | 1975-05-27 | Jet Research Center | Aircraft emergency egress system |
| US6027073A (en) * | 1997-07-18 | 2000-02-22 | Eurocopter | Window release system |
Non-Patent Citations (1)
| Title |
|---|
| 李志强等: "微爆索线性切割航空有机玻璃的实验研究和有限元分析", 《爆炸与冲击》 * |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110979697A (en) * | 2019-12-23 | 2020-04-10 | 中国航空工业集团公司沈阳飞机设计研究所 | Porthole emergency blasting folding, turning and throwing device |
| CN110979697B (en) * | 2019-12-23 | 2023-01-17 | 中国航空工业集团公司沈阳飞机设计研究所 | Porthole emergency blasting folding, turning and throwing device |
| CN112173128A (en) * | 2020-09-25 | 2021-01-05 | 中国直升机设计研究所 | Splint hinge is with throwing vaulting pole device of putting |
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Application publication date: 20150805 |