CN109911234A - A kind of forced landing device for airfield runway - Google Patents
A kind of forced landing device for airfield runway Download PDFInfo
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- CN109911234A CN109911234A CN201910209666.0A CN201910209666A CN109911234A CN 109911234 A CN109911234 A CN 109911234A CN 201910209666 A CN201910209666 A CN 201910209666A CN 109911234 A CN109911234 A CN 109911234A
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- protection
- forced landing
- runway
- protection hole
- rescue
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Abstract
The invention discloses a kind of forced landing devices for airfield runway, including runway and the protective device for being set to runway side；Further include the deliverance apparatus for being located at protective device one end in the device for airfield runway forced landing, aircraft can be made to force-land by the effect of protective device, rescue personnel can be made quickly to reach rescue site by the effect of deliverance apparatus；Described runway one end is equipped with alarm, and runway one end is equipped with controller.The invention has the advantages that of simple structure and strong practicability.
Description
Technical field
The present invention relates to forced landing related fields, especially a kind of forced landing device for airfield runway.
Background technique
Nowadays aircraft trip has been used as a kind of main trip tool, and annual global commerce flight frequency is up to ten million
Secondary, flight safety reliability is very high, but when aircraft because the reasons such as mechanical, hydraulic or electrical equipment failure cause undercarriage without
In the case that method is opened or other reasons lead to the dangerous property of aircraft regular descent, at this moment there is aircraft accident, machine ruins people
The case where dying still not can avoid, and probability of the forced landing without injures and deaths is very low, in aviation history and in modern Aviation practice, usually go out
Now because undercarriage fail due to cause aircraft can not regular descent the problem of, be forced landing when, can aircraft landing moment aircraft
Bottom shell and ground hard contact, cause the accident of fatal crass to occur.In order to avoid the generation of such accident, China and foreign countries' aviation
The engineers and technicians in field have carried out a large amount of technological improvement, but these technological improvements are to be conceived to undercarriage and aircraft peace
Above full performance.Such as install additional electronic, it surges, in the mechanism of rise and fall manually etc. rack control device and other handling failures.In this way
Although doing the probability for reducing accident generation, problems can not be fundamentally solved.
Summary of the invention
The purpose of the present invention is to solve the above problems, devise a kind of forced landing device for airfield runway.
Realize above-mentioned purpose the technical scheme is that, including runway and the protection for being set to runway side
Device；Further include the deliverance apparatus for being located at protective device inner surface in the device for airfield runway forced landing, passes through protection
The effect of device can make aircraft force-land, and rescue personnel can be made quickly to reach rescue by the effect of deliverance apparatus existing
?；Described runway one end is equipped with alarm, and runway one end is equipped with controller.
The protective device includes the protection hole for being deployed in runway side, is equipped with buffering liquid, protection in protection hole
It cheats side surface and is equipped with recursive filter, protection hole lower surface is husky equipped with buffering, and protection hole inner surface is equipped with wear-resisting rubber pad, protection
It cheats side and is equipped with water trap, protection hole one end is equipped with speed sensor；The longitudinal section in the protection hole is inverted trapezoidal, the protection
Bottom is rice on the longitudinal section in hole, is gone to the bottom as rice；The depth in the protection hole is rice；The width in the protection hole is rice.
The deliverance apparatus is deployed in the rescue speedboat of protection hole one end, and the protection hole other end is equipped with tractor, tractor
Output end is equipped with connecting rope, and connecting rope one end is intertwined and connected with tractor, and the connecting rope other end is fixedly connected with rescue speedboat.
The rescue speedboat upper surface is equipped with first-aid kit.
Protection hole two sides are equipped with anticollision waste tire.
Protection hole one end is equipped with water plug.
Protection hole inner surface is equipped with horizontal detector.
The husky side surface of the buffering is equipped with smooth bar.
A kind of forced landing device for airfield runway made using technical solution of the present invention, passes through the work of protective device
With that aircraft can be made to force-land, to realize forced landing purpose.Rescue personnel can be made fast by the effect of deliverance apparatus
The arrival rescue site of speed, to improve rescue efficiency.
Detailed description of the invention
Fig. 1 is a kind of overlooking structure diagram of forced landing device for airfield runway of the present invention；
Fig. 2 is the schematic cross-sectional view in protection hole of the present invention；
In figure, 1, runway；2, alarm；3, controller；4, protection hole；5, buffering liquid；6, recursive filter；7,
Buffering is husky；8, wear-resisting rubber pad；9, water trap；10, speed sensor；11, speedboat is rescued；12, tractor；13, connecting rope；14,
First-aid kit；15, anticollision waste tire；16, water plug；17, horizontal detector；18, smooth bar.
Specific embodiment
The present invention is specifically described with reference to the accompanying drawing, as shown in Figs. 1-2.
In the present embodiment, aircraft can be made to force-land by the effect of protective device, to realize forced landing
Purpose.Rescue personnel can be made quickly to reach rescue site by the effect of deliverance apparatus, to improve rescue efficiency.
Aircraft when being force-landed can toward protection hole 4 in land, protection hole 4 shape be inverted trapezoidal, upper bottom and
Bottom is rectangle, and alarm 2 can issue ear-piercing alarm song when aircraft is force-landed, and prompts live irrelevant personnel
It leaves as early as possible, after aircraft pours protection hole, the buffering energetically of buffering liquid will be received, reduce the impact velocity of aircraft, due to
Protection 4 two sides of hole are equipped with buffering sand equipped with wear-resisting rubber pad 8,4 bottoms of protection hole, can form second to aircraft and buffer, finally
Aircraft is compeled to stop；Then controller 3 controls water trap 6 and carries out the liquid level that draining reduction is protected in hole, and it is excessive to reduce generation in cabin
The possibility of water completes forced landing work after liquid level is reduced to safety line, and rescue personnel starts to rescue.
After forced landing is good, rescue personnel can reach emergency place by taking rescue speedboat 11, multiply to stranded
Visitor's expansion rescue；After the completion of rescue, aboard by connecting rope system, then speedboating leaves rescue personnel, simultaneously
Controller 3 controls tractor 12 and works, and the power of tractor 12 is transmitted on forced landing aircraft by connecting rope 13, by aircraft
It is empty to pull out protection；After completing above-mentioned movement, staff is carried out whole by the buffering sand 7 of 18 pairs of part out-of-flatnesses of smooth bar
Reason, the structure that smooth bar is constituted using the fixed formation plate in stock one end.
In order to facilitate rescue, headlamp can also be arranged on the edge in protection hole in technical staff, to provide in protection hole
Illumination, facilitates rescue.Buffering liquid can select water.Buffering liquid 5 can be carried out centainly by the effect of recursive filter 6
Circulating filtration, reduce phytoplankton.
Above-mentioned technical proposal only embodies the optimal technical scheme of technical solution of the present invention, those skilled in the art
The principle of the present invention is embodied to some variations that some of them part may be made, belongs to the scope of protection of the present invention it
It is interior.
Claims (8)
1. a kind of forced landing device for airfield runway, including runway (1) and it is set to the protection of runway (1) side
Device；It is characterized in that, further including the deliverance apparatus for being located at protective device one end, aircraft can be made by the effect of protective device
It force-lands, rescue personnel can be made quickly to reach rescue site by the effect of deliverance apparatus；The runway (1) one
End is equipped with alarm (2), and runway (1) one end is equipped with controller (3).
2. a kind of forced landing device for airfield runway according to claim 1, which is characterized in that the protective device packet
The protection hole (4) for being deployed in runway (1) side is included, is equipped with buffering liquid (5) in protection hole (4), protection hole (4) side surface
Equipped with recursive filter (6), protection hole (4) lower surface, which is equipped with, to be buffered husky (7), and protection hole (4) inner surface is equipped with wear-resisting rubber pad
(8), protection hole (4) side is equipped with water trap (9), and protection hole (4) one end is equipped with speed sensor (10)；(4) are cheated in the protection
Longitudinal section be inverted trapezoidal, it is described protection hole (4) longitudinal section on bottom be 1500 meters, going to the bottom is 500 meters；(4) are cheated in the protection
Depth be 5 meters；The width of the protection hole (4) is 100 meters.
3. a kind of forced landing device for airfield runway according to claim 1, which is characterized in that the deliverance apparatus portion
It is deployed on the rescue speedboat (11) of protection hole (4) one end, protection hole (4) other end is equipped with tractor (12), tractor (12) output
End is equipped with connecting rope (13), and connecting rope (13) one end is intertwined and connected with tractor (12), and connecting rope (13) other end and rescue are fast
Ship (11) is fixedly connected.
4. a kind of forced landing device for airfield runway according to claim 3, which is characterized in that the rescue speedboat
(11) upper surface is equipped with first-aid kit (14).
5. a kind of forced landing device for airfield runway according to claim 2, which is characterized in that (4) are cheated in the protection
Two sides are equipped with anticollision waste tire (15).
6. a kind of forced landing device for airfield runway according to claim 2, which is characterized in that (4) are cheated in the protection
One end is equipped with water plug (16).
7. a kind of forced landing device for airfield runway according to claim 2, which is characterized in that (4) are cheated in the protection
Inner surface is equipped with horizontal detector (17).
8. a kind of forced landing device for airfield runway according to claim 2, which is characterized in that the buffering is husky (7)
Side surface is equipped with smooth bar (18).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910209666.0A CN109911234A (en) | 2019-03-19 | 2019-03-19 | A kind of forced landing device for airfield runway |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910209666.0A CN109911234A (en) | 2019-03-19 | 2019-03-19 | A kind of forced landing device for airfield runway |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109911234A true CN109911234A (en) | 2019-06-21 |
Family
ID=66965791
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910209666.0A Pending CN109911234A (en) | 2019-03-19 | 2019-03-19 | A kind of forced landing device for airfield runway |
Country Status (1)
| Country | Link |
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| CN (1) | CN109911234A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB591848A (en) * | 1939-03-14 | 1947-09-01 | George Alexis Rubisson | Method and device for forced takeof and forced landing of aeroplanes and airships |
| CN102151377A (en) * | 2011-05-27 | 2011-08-17 | 陈建辉 | Multifunctional rescue device suitable for complex environment |
| CN204701754U (en) * | 2015-06-11 | 2015-10-14 | 中国人民解放军第二军医大学东方肝胆外科医院 | Navigation-type falls extra large personnel's salvage ship |
| CN108560353A (en) * | 2018-04-25 | 2018-09-21 | 李金华 | A kind of airplane emergency forced landing runway and its method of construction |
| CN109334898A (en) * | 2018-09-30 | 2019-02-15 | 北京津泰海工科技有限公司 | A kind of drowning man's Quick rescue method and rescue system |
-
2019
- 2019-03-19 CN CN201910209666.0A patent/CN109911234A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB591848A (en) * | 1939-03-14 | 1947-09-01 | George Alexis Rubisson | Method and device for forced takeof and forced landing of aeroplanes and airships |
| CN102151377A (en) * | 2011-05-27 | 2011-08-17 | 陈建辉 | Multifunctional rescue device suitable for complex environment |
| CN204701754U (en) * | 2015-06-11 | 2015-10-14 | 中国人民解放军第二军医大学东方肝胆外科医院 | Navigation-type falls extra large personnel's salvage ship |
| CN108560353A (en) * | 2018-04-25 | 2018-09-21 | 李金华 | A kind of airplane emergency forced landing runway and its method of construction |
| CN109334898A (en) * | 2018-09-30 | 2019-02-15 | 北京津泰海工科技有限公司 | A kind of drowning man's Quick rescue method and rescue system |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20190621 |