CN1288843A - Pilot escaping technolgy for vertically and short-distance take-off and landing jet plane - Google Patents
Pilot escaping technolgy for vertically and short-distance take-off and landing jet plane Download PDFInfo
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- CN1288843A CN1288843A CN 99120812 CN99120812A CN1288843A CN 1288843 A CN1288843 A CN 1288843A CN 99120812 CN99120812 CN 99120812 CN 99120812 A CN99120812 A CN 99120812A CN 1288843 A CN1288843 A CN 1288843A
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Abstract
The present invention belongs to the field of aviation life technology. The invented technical problem required for solving mainly includes two points: 1. vertical/short take-off and landing jet aircraft, it is basis for implementing said invention; and 2. lift hanging cabin as life carrier. The main technique of said invention is characterized by that the vertical/STOL jet aircraft equipped with life hanging cabin can be used to rescure the pilot being in distress in the vertical langing mode. The application of said invention is to provide a new, more effective lift measure for pilot to make it combine with existent technique to form a more complete life system for pilot.
Description
The invention belongs to the aviation lifesaving field.
So-called pilot escaping technolgy for vertically and short-distance take-off and landing jet plane, the technology that the aviator that a kind of exactly vertical/short take-off and landing (STOL) jet supersonic plane (to call vertical take-off and landing aircraft (VTOL aircraft) in the following text) of utilizing equipment to attach life falls into the enemy to parachuting in parachutist, especially wartime succours.
As everyone knows, at present various countries adopt the helicopter lifesaving technology to succour for the aviator that the aviator of parachute jumping in danger, especially parachute jumping in wartime fall into the enemy, promptly send helicopter to go to aviator's place rescue of landing of falling in good time.As a kind of aerial lifesaving technology of maturation, the helicopter lifesaving is out of the ordinary in the on performance of all previous aviator's lifesaving, has stayed many proud lifesaving achievements.But some deficiency of helicopter lifesaving meanwhile, especially also can not be ignored in aviator's defective that lifesaving is shown wartime, such as: the viability of helicopter is not strong, and it is very easily under attack when executing the task to enter the enemy, has influenced single-piece lifesaving success ratio; The maneuverability of helicopter is limited in addition, be difficult to adapt to the needs of the modern war of comprehensive, great depth to aviator's lifesaving ... these problems show that the helicopter lifesaving technology is also imperfect, also need certain new technology to come it is replenished.
The objective of the invention is to: provide a kind of new, be mainly used in the aerial survival means that the aviator succour wartime, remedying the deficiency that has aerial lifesaving technology now, and constitute an aerial lifesaving system of more perfect aviator with prior art.Certainly present technique also can be used for some specific people and aviator's rescue at ordinary times.
The enforcement of the technology of the present invention is the vertical take-off and landing aircraft (VTOL aircraft) of hanging the cabin based on the equipment lifesaving.Why select vertical take-off and landing aircraft (VTOL aircraft), be because vertical take-off and landing aircraft (VTOL aircraft) can resemble vertical takeoff and landing the helicopter, have simultaneously the such high-altitude of conventional jet supersonic plane, high speed performance again, this makes vertical take-off and landing aircraft (VTOL aircraft) have more emergentness and disguise when carrying out the lifesaving task, has increased the success ratio of lifesaving; Why selecting to vertical take-off and landing aircraft (VTOL aircraft) equipment lifesaving extension cabin, be because present vertical take-off and landing aircraft (VTOL aircraft) lacks the available space that can hold the personnel that rescued, and lifesaving extension cabin can provide such space of sheltering oneself.So-called lifesaving hang the cabin be exactly personnel's level of a kind ofly having certain-length and volume, can holding a full-length couch, possess basic life-support equipment (as temperature and air pressure control, oxygen supply equipment, position fixed equipment etc.) and have certain aerodynamic configuration, can be by the plug-in box describe device that carries of aircraft.The radical function that the cabin is hung in lifesaving is provided a lifesaving carrier (space of promptly effectively sheltering oneself) to rescuing the aviator exactly, so that vertical take-off and landing aircraft (VTOL aircraft) can be rescued away it.Lifesaving is hung the cabin and generally is equipped on vertical take-off and landing aircraft (VTOL aircraft) with plug-in form, and plug-in mode both can be a under-fuselage mounting, also can be that wing hangs.The advantage that wing hangs is that left-right symmetric, aircraft can be equipped two lifesaving extension cabins simultaneously.The lifesaving that vertical take-off and landing aircraft (VTOL aircraft) is equipped when carrying out rescue mission is hung cabin quantity and generally is advisable with 1-2.The cabin is hung in lifesaving to be had when design and what time should be noted that: the hatch door design that the cabin is hung in (1) lifesaving will be convenient to be rescued personnel and enter fast, is beneficial to succour aircraft and as early as possible it is rescued away.(2) in order to be rescued aviator's safety, the cabin is hung in lifesaving can suitably increase protection plate armour and parachute.Equipped lifesaving extension cabin vertical take-off and landing aircraft (VTOL aircraft) and just possessed basic lifesaving ability, but also needed corresponding ancillary method in order to obtain good lifesaving effect in practice.Such as: when carrying out remote lifesaving task, to there be aerial fuel charger in time to refuel to vertical take-off and landing aircraft (VTOL aircraft); Being rescued the aviator then should have corresponding communication and fixing aid etc.Introduce the basis that the technology of the present invention is implemented, next introduced the basic operational mode of present technique again; Aviator's parachute jumping is landed the back earlier with self-position and situation report higher level and request rescue; Carry out and rush for the scene fast after the vertical landing aircraft of rescuing is received order, find just landing near it and opening the hatch door in lifesaving extension cabin behind the aviator; Aviator in danger then enters lifesaving extension cabin level fast and lies down, and fastens life simultaneously and closes the extension cabin door; Everything is ready, and back aviator in danger just sends signal, and vertical take-off and landing aircraft (VTOL aircraft) is just taken off and returned.Rescue action is finished successfully at this point.
Compare with existing helicopter lifesaving technology, the present invention has outstanding advantage.(1) since the vertical take-off and landing aircraft (VTOL aircraft) flying speed soon, highly big, have more emergentness and disguise, the success ratio of lifesaving thereby much higher when carrying out the lifesaving task; (2) the vertical take-off and landing aircraft (VTOL aircraft) maneuverability is very strong, more can adapt to for the modern war of comprehensive, the great depth demand to lifesaving.These advantages of present technique are that helicopter is incomparable, so its advantage is apparent.
In order to make each potential energy understanding more intuitively be arranged to the present invention, below be reference with the Figure of description just, the present invention is done further explanation.As shown in the figure, the form that vertical take-off and landing aircraft (VTOL aircraft) hangs with wing is being equipped lifesaving and is being hung the cabin, has lifesaving extension cabin and makes vertical take-off and landing aircraft (VTOL aircraft) possess basic lifesaving ability; The personnel that rescued place oneself in the midst of lifesaving with the posture that level is lain on the back to hang in the cabin, so that the rescue aircraft is rescued away it apace.
Realization of the present invention is relatively easy.Realize that key of the present invention is to be a kind of method, promptly in the mode of vertical landing aviator in danger is succoured with the vertical take-off and landing aircraft (VTOL aircraft) in equipment lifesaving extension cabin.From the technical standpoint, hang the cabin and just possessed basis of the invention process as long as have vertical take-off and landing aircraft (VTOL aircraft) and corresponding lifesaving.With regard to reality, vertical take-off and landing aircraft (VTOL aircraft) is ready-made equipment already, and the vertical take-off and landing aircraft (VTOL aircraft) that resembles AV-8, Ya Ke-38 and so on has been to be on active service for many years.Hang the cabin as for lifesaving, though do not have this special equipment at present, with lifesaving hang the cabin intimate, be used for the cargo-carring manned extension of personnel cabin and occurred, lifesaving is hung the cabin and has been improved as long as do some at this.Can know that from these situations technical foundation of the invention process substantially all is with the existing master of being equipped for, not have what great technical barrier, therefore realization of the present invention is easy to really.
Claims (1)
- Pilot escaping technolgy for vertically and short-distance take-off and landing jet plane is as a kind of invention, and present technique and existing helicopter lifesaving technology have common technical characterictic, promptly all is to utilize the aircraft of energy vertical takeoff and landing that aviator in danger is succoured.Technical characterictic of the present invention is: the vertical/short take-off and landing (STOL) jet supersonic plane in cabin is hung in the equipment lifesaving, in the mode of vertical landing aviator in danger is succoured.The present invention and existing technology exist more significantly difference on technical characterictic: prior art be the aviator that gets into danger to be succoured with the mode of helicopter landing, and be as the carrier that holds the personnel that rescued with the space of aircraft own; The present invention succours aviator in danger with the vertical take-off and landing aircraft (VTOL aircraft) in equipment lifesaving extension cabin, and is to hang the cabin as the lifesaving carrier that holds the personnel that rescued with subsidiary lifesaving.The cumulated volume invention can limit the scope of protection of present invention with prior art in the similarities and differences of technical characterictic, and the scope of protection of present invention is: every vertical take-off and landing aircraft (VTOL aircraft) with equipment lifesaving extension cabin is succoured the row that all belong to the claimed scope of the present invention in the mode of vertical landing to the aviator.For this usefulness vertical/lifesaving of short take-off and landing (STOL) jet supersonic plane equipment hangs the cabin and carries out the method for aviator's lifesaving and require to give corresponding protection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 99120812 CN1288843A (en) | 1999-09-21 | 1999-09-21 | Pilot escaping technolgy for vertically and short-distance take-off and landing jet plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 99120812 CN1288843A (en) | 1999-09-21 | 1999-09-21 | Pilot escaping technolgy for vertically and short-distance take-off and landing jet plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN1288843A true CN1288843A (en) | 2001-03-28 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 99120812 Pending CN1288843A (en) | 1999-09-21 | 1999-09-21 | Pilot escaping technolgy for vertically and short-distance take-off and landing jet plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN1288843A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104149984A (en) * | 2014-08-28 | 2014-11-19 | 沙太宝 | Helicopter rescue pod |
| DE102018116169A1 (en) | 2018-07-04 | 2020-01-09 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | aircraft |
| DE102018116160A1 (en) | 2018-07-04 | 2020-01-09 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | aircraft |
-
1999
- 1999-09-21 CN CN 99120812 patent/CN1288843A/en active Pending
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104149984A (en) * | 2014-08-28 | 2014-11-19 | 沙太宝 | Helicopter rescue pod |
| DE102018116169A1 (en) | 2018-07-04 | 2020-01-09 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | aircraft |
| DE102018116160A1 (en) | 2018-07-04 | 2020-01-09 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | aircraft |
| DE102018116169B4 (en) | 2018-07-04 | 2022-02-24 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | aircraft |
| DE102018116160B4 (en) | 2018-07-04 | 2022-07-07 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | aircraft |
| US11505087B2 (en) | 2018-07-04 | 2022-11-22 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | Aircraft |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |