CN1403342A - Flyer with relatively higher safety - Google Patents
Flyer with relatively higher safety Download PDFInfo
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- CN1403342A CN1403342A CN 02135004 CN02135004A CN1403342A CN 1403342 A CN1403342 A CN 1403342A CN 02135004 CN02135004 CN 02135004 CN 02135004 A CN02135004 A CN 02135004A CN 1403342 A CN1403342 A CN 1403342A
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Abstract
The present invention relates to aeronautical and astraonautic technology, and is one safe mechanism, which makes the flyer capable of landing safey in case the flyer can not fly normally. The technological scheme is that one parachute is provided for the flyer body. The technology of the present invention may be used widely in aeronautical and astronautic fields.
Description
Technical field:
The present invention relates to space flight, air material technical field, when refering in particular to a kind of driving engine and can't provide power to make the aircraft normal flight, can make the device of aircraft security landing at aircraft.
Background technology:
In space flight, aircraft industry, because the costliness of various equipment costs, and the destructive consequence that caused takes place in accident, requires various device all to have higher safety; But, because the reliability of each equipment can not reach 100%; Therefore, higher reliability can only reduce the probability that fault takes place theoretically; In the space flight of reality, aviation, particularly aspect civil aviaton, because the growth of equipment period of service, the increasing of et out of order probability, and reasons such as production, manufacturing, various accidents happen occasionally; For this reason, the professional person of each side has carried out continuous effort for this reason, has improved the safety of space flight, air material widely, still, still can't avoid the generation because of various faults such as driving engine, alighting gears fully; When aircraft because of engine breakdown run out of steam in the high-altitude support, alighting gear can't strut can't normal landing etc. accident when taking place, not only can cause damage to aircraft itself, and entail dangers to brings tremendous loss for people's lives and properties to passenger's life security, the property safety of institute's cargo; According to incompletely statistics,, still have every year many Aeronautics and Astronautics accidents to take place in scientific and technological highly developed today nowadays, the loss that it caused all the time in hundred million; Therefore, how thoroughly solving the safety issue of aircraft, is the problem that each Flight Vehicle Design person perplexs.
Summary of the invention:
The object of the present invention is to provide and a kind ofly can guarantee why no matter aircraft plant fault and can't normal flight the time, the device that can land safely.
The present invention is achieved through the following technical solutions: the top in the main body of aircraft is provided with the body parachute, when unpowered unsettled or other fault of aircraft takes place, to strut, aircraft is slowly landed or landing across the sea.
In addition, for guaranteeing the safety of aircraft, also can be provided with air cushion in the bottom of the main body of aircraft; Parachute and main body can be connected for 2 or multipoint system; The driving engine that one induction aircraft arranged the whether inductor of normal operation links to each other with the exploder that the body parachute is flicked; The driving engine that one induction aircraft arranged the whether inductor of normal operation links to each other with gas filled device with the air cushion fast aeration; Above-mentioned two inductors can be same inductor, control flicking with air-sprung of parachute simultaneously and inflate; The main body of aircraft is dish-shaped shape.
The present invention aircraft because of engine breakdown etc. former thereby can't normally land, when flying, the body parachute can be flicked immediately, and aircraft is landed lentamente; When aircraft contacts with ground or sea, at first contact with ground or sea, thereby the soft landing of realization aircraft is being guaranteed under the prerequisite of passenger safety, and need not the passenger suffered any impact, scaring by gas filed air cushion; Simultaneously, can also guarantee the safety of aircraft itself and institute's cargo, the generation of thoroughly stopping various space flight, aviation disaster.
Description of drawings:
The present invention is further described below in conjunction with accompanying drawing:
Accompanying drawing is a main body scheme drawing of the present invention.
The specific embodiment:
See accompanying drawing, the present invention is provided with a body parachute 2 in 2 at the top or the multipoint system of the main body 1 of dish-shaped shape aircraft, and is provided with air cushion 3 in the bottom; For ease of control, the driving engine that one induction aircraft arranged the whether inductor of normal operation and other fault links to each other with the exploder that body parachute 2 is flicked, and the driving engine that an induction aircraft also arranged the whether inductor of normal operation links to each other with gas filled device with air cushion 3 fast aeration; Above-mentioned inductor can also unite two into one, and controls flicking with air-sprung of body parachute 2 simultaneously by an inductor and inflates.
When the aircraft normal flight, 2 foldings of body parachute, air cushion 3 unaerateds; Can't normal flight because of reasons such as engine breakdowns or can't normally land the time, inductor passes the signal to exploder immediately, opens immediately by this exploder control body parachute 2 as aircraft; Meanwhile, gas filled device is also fast to air cushion 3 inflations; Under the effect of body parachute 2, aircraft reduces height lentamente; And under the effect of air cushion 3, can guarantee the ground of aircraft and landing or the sea is soft contacts, guarantee the safety of aircraft and interior manned, thing thereof.
Above-described aircraft is mainly used in the novel disc-shaped flying craft that the inventor invents, but all at present aircraft or in the future the course of new aircraft of institute's development and Design separate all and can move, and be not limited to cited.
And the application of this aircraft can be civilian, military aviation, space flight, and as toy use etc.
Claims (7)
1, the higher aircraft of a kind of safety is characterized in that: the top in the main body (1) of aircraft is provided with body parachute (2).
2, the higher aircraft of a kind of safety according to claim 1 is characterized in that: the bottom in the main body (1) of aircraft also can be provided with air cushion (3).
3, the higher aircraft of a kind of safety according to claim 1 is characterized in that: body parachute (2) and main body (1) can be connected for 2 or multipoint system.
4, according to claim 1 or the higher aircraft of 3 described a kind of safetys, it is characterized in that: the driving engine that an induction aircraft arranged the whether inductor of normal operation links to each other with the exploder that body parachute (2) is flicked.
5, the higher aircraft of a kind of safety according to claim 2 is characterized in that: the driving engine that an induction aircraft arranged the whether inductor of normal operation links to each other with gas filled device with air cushion (3) fast aeration.
6, according to claim 1,2, the higher aircraft of 3 or 5 described a kind of safetys, it is characterized in that: the main body of aircraft (1) is dish-shaped shape.
7, the higher aircraft of a kind of safety according to claim 4 is characterized in that: the main body of aircraft (1) is dish-shaped shape.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 02135004 CN1403342A (en) | 2002-10-23 | 2002-10-23 | Flyer with relatively higher safety |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 02135004 CN1403342A (en) | 2002-10-23 | 2002-10-23 | Flyer with relatively higher safety |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN1403342A true CN1403342A (en) | 2003-03-19 |
Family
ID=4747992
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 02135004 Pending CN1403342A (en) | 2002-10-23 | 2002-10-23 | Flyer with relatively higher safety |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN1403342A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103979110A (en) * | 2014-05-29 | 2014-08-13 | 襄阳宏伟航空器有限责任公司 | Ballistic parachute life-saving system |
| CN104260897A (en) * | 2014-09-23 | 2015-01-07 | 苏州天益航空科技有限公司 | Agricultural crop protection unmanned aerial vehicle fault forced landing device |
| CN109204835A (en) * | 2018-10-18 | 2019-01-15 | 五邑大学 | A kind of sounding rocket parachute opener of burn-out proof |
-
2002
- 2002-10-23 CN CN 02135004 patent/CN1403342A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103979110A (en) * | 2014-05-29 | 2014-08-13 | 襄阳宏伟航空器有限责任公司 | Ballistic parachute life-saving system |
| CN104260897A (en) * | 2014-09-23 | 2015-01-07 | 苏州天益航空科技有限公司 | Agricultural crop protection unmanned aerial vehicle fault forced landing device |
| CN109204835A (en) * | 2018-10-18 | 2019-01-15 | 五邑大学 | A kind of sounding rocket parachute opener of burn-out proof |
| CN109204835B (en) * | 2018-10-18 | 2023-09-08 | 五邑大学 | Anti-ablation sounding rocket parachute opening device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C12 | Rejection of a patent application after its publication | ||
| RJ01 | Rejection of invention patent application after publication |