CN103112590A - Airplane capable of landing safely - Google Patents
Airplane capable of landing safely Download PDFInfo
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- CN103112590A CN103112590A CN2011103624253A CN201110362425A CN103112590A CN 103112590 A CN103112590 A CN 103112590A CN 2011103624253 A CN2011103624253 A CN 2011103624253A CN 201110362425 A CN201110362425 A CN 201110362425A CN 103112590 A CN103112590 A CN 103112590A
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Abstract
The invention provides an airplane capable of landing safely, belongs to the field of airplane technology and mainly solves the problems that an existing airplane can not safely land due to faults or in the hijacked process. The airplane capable of landing safely is mainly characterized in that an airplane electric undercarriage is arranged beside an airplane mechanical undercarriage. A whole journey monitor unit is arranged in an airplane passenger cabin. Whole journey monitor unit display screens are arranged in an airplane flight compartment and the airplane passenger cabin. Instrument panel airplane remote control buttons are arranged on an instrument panel. Pedal-type airplane remote control buttons are arranged below the instrument panel. A plurality of layers of parachutes and parachute catapults are arranged on the airplane flight compartment, the airplane passenger cabin, an airplane tail, an airplane left wing and an airplane right wing. An electric propeller thruster is arranged on the outer upper portion of the airplane passenger cabin. On the condition that the airplane can not normally land and falls down rapidly, the airplane capable of landing safely has the advantage that pilots, security staff and service staff all can operate and enable the airplane to safety land and the airplane capable of landing safely is mainly the airplane which is provided with various safety landing support facilities.
Description
Technical field
The invention belongs to the aircraft technology field.Be specifically related to a kind of type aircraft that possesses multiple safe falling support facility.
Background technology
Come from serious hope and the dream in fly blue sky, the mankind can be carried the mankind and fly skyward carrier studying always over the past thousands of years, development along with human sciences's technology, in 20 beginnings of the century, the Lai Te brother of the U.S. has invented aircraft, on December 17th, 1903, U.S. Lai Te brother is driving an Aircraft Flight Test success of aviator, human dream of aloft hovering as flying bird is made one's wish fulfilled finally, since then, has pulled open the prelude of human science and technology of aviation great development.Along with human society in military affairs, commercial affairs, tourism, logistics, geography, photography and all trades and professions development and efficient demand, aeronautical technology has also obtained increasing application in the human lives.
Because aircraft is in high-altitude flight, in case because the overheated a variety of causes such as on fire of mechanical breakdown, rough weather impact, lightning thunderbolt, flying bird collision, machinery, oil circuit causes aircraft to stop can not normal flight the time, usually can cause fatal crass's tragedy aloft.The generation of each air crash, not only allow the victim family members overwhelmed with sorrow, brought huge loss to country, brought ill effect also for the reputation of aircraft industry.
So, how to make the safe falling aircraft of hommization? I think: that people-oriented, take people's life as supreme interest, with sight lengthen see far away, aircraft industry reply passenger's safe altitude is responsible for, aircraft manufacturing producer should adopt safer new material and from the angle of safety go to research and develop more advanced technology, more feasible method manufacturing can be tackled the safe falling aircraft of various burst dangerous situations, no matter be government or businessman's early investment than the later stage more positive reparations human-oriented, like the people many.
Nowadays, the birth of aircraft, existing more than 100 year, aircraft manufacturing producer spreads all over the world especially, much heavier aircraft manufacturing producer also constantly drops into huge manpower and financial resources for how making the safe falling aircraft always, still: airplane crash also continue, each tragedy also shows continuing.
Summary of the invention
Purpose of the present invention provides a kind of after aircraft involuntary stoppage occurs aloft for above-mentioned weak point exactly, aircraft can not normally land and aircraft in the situation of falling rapidly, aviator on the aircraft, security officers and attendant all can press button or the remote controller buttons of the operating aircraft that arranges on the aircraft, a kind of safe falling aircraft that lands a plane safely.
Technical solution of the present invention is: a kind of safe falling aircraft, comprise aircraft cockpit, aircraft passenger compartment, aircraft tail, aircraft port wing, aircraft starboard wing and aircraft machinery alighting gear, be provided with control system and gauge panel in the aircraft cockpit, it is characterized in that: at the other aircraft electric lifting device frame that is provided with side by side of described aircraft machinery alighting gear; In aircraft passenger compartment, be provided with the complete monitoring device; In aircraft cockpit, aircraft passenger compartment, be provided with complete monitoring device read-out; Gauge panel at aircraft cockpit is provided with gauge panel aircraft remote controller buttons, is provided with foot-operated aircraft remote controller buttons at under-dash; Be provided with multilayer parachute and parachute ejector at aircraft cockpit, aircraft passenger compartment, aircraft tail, aircraft port wing and aircraft starboard wing outside face; Be provided with the electric propeller propelling unit at the aircraft passenger compartment outside face.
Aircraft cockpit described in the technical solution of the present invention, the outer bottom of aircraft passenger compartment and the right and left are provided with safety air bag.
Aircraft cockpit gauge panel aircraft remote controller buttons described in the technical solution of the present invention is two, divides the place ahead that is located at driver and copilot; Foot-operated aircraft remote controller buttons is two, divides the front lower place that is located at driver and copilot.
Electric propeller propelling unit described in the technical solution of the present invention is 2, and is provided with the rotating mechanism of rotatable 60 degree directions.
Also comprise control aircraft electric lifting device frame, parachute ejector, electric propeller propelling unit in the technical solution of the present invention, and portable miniature remote controlled device.
The present invention is because at the existing aircraft cockpit that comprises, aircraft passenger compartment, the aircraft tail, the aircraft port wing, on the aircraft basis of aircraft starboard wing and aircraft machinery alighting gear, at the other aircraft electric lifting device frame that is provided with side by side of aircraft machinery alighting gear, in aircraft passenger compartment, be provided with the complete monitoring device, at aircraft cockpit, be provided with complete monitoring device read-out in the aircraft passenger compartment, gauge panel at aircraft cockpit is provided with gauge panel aircraft remote controller buttons, be provided with foot-operated aircraft remote controller buttons at under-dash, at aircraft cockpit, aircraft passenger compartment, the aircraft tail, aircraft port wing and aircraft starboard wing outside face are provided with multilayer parachute and parachute ejector, be provided with the electric propeller propelling unit at the aircraft passenger compartment outside face, thereby when aircraft landing, as not opening because of mechanical breakdown aircraft machinery alighting gear, can press aircraft electric lifting device frame button and the electric lifting device frame be opened aircraft safety is landed; In case chance failure appears in aircraft, aircraft is aloft stopped, at this moment the aviator can be with the foot-operated aircraft button of driver and copilot front lower place in the aircraft remote controller buttons on the driver and copilot gauge panel in the aircraft cockpit or the aircraft cockpit, Security Personnel in the aircraft passenger compartment or attendant can with the miniature remote controlled device of carrying, eject the multilayer parachute and launch holding in the palm slowly safe falling of aircraft with the starting of parachute ejector; When aircraft in the process of landing, if just in time be in densely populated urban area during aircraft landing or high-lager building when overhead, also can cause disaster, at this moment can start the electric propeller propelling units of rotatable 60 degree directions, promote aircraft and waft from the danger zone; When aircraft in when landing, if aircraft drops on the water surface of great river, sea and each region, but also airbag opening at this moment, even aircraft landing is on the water surface, aircraft also can float on the surface, and the electric propeller propelling units that start simultaneously rotatable 60 degree directions promote aircrafts and pull in to shore or wait for rescue safe escape.In addition, occur if break down in the driving compartment or by contingencies such as terrified offender hijack, at this moment Security Personnel or the attendant in the aircraft passenger compartment can press the miniature remote controlled device of carrying, the above security procedure of starting lands a plane safely, and guarantees that the people's lives and property do not suffer a loss.The present invention has overcome the deficiencies in the prior art, have after aircraft involuntary stoppage occurs aloft, aircraft can not normally land and aircraft in the situation of falling rapidly, aviator on the aircraft, security officers and attendant all can press button or the remote controller buttons of the operating aircraft that arranges on the aircraft, the characteristics that land a plane safely.The present invention is mainly used in possessing the aircraft of multiple safe falling support facility.
Description of drawings
Fig. 1 is structural representation of the present invention.
Fig. 2 aircraft is opened associated safety program display figure after vacating existing accident.
The built-in figure of Fig. 3 aircraft passenger compartment.
The built-in figure of Fig. 4 aircraft cockpit.
Fig. 5 aircraft occurs unexpected parachute aloft and ejects rear scheme drawing.
The specific embodiment
Extremely shown in Figure 5 such as Fig. 1.A kind of safe falling aircraft of the present invention, comprise aircraft cockpit 1, aircraft passenger compartment 2, aircraft tail 3, aircraft port wing 4, aircraft starboard wing 5 and aircraft machinery alighting gear 6, be provided with control system and gauge panel in the aircraft cockpit 1, corresponding identical with in the existing aircraft.Different is at the aircraft machinery alighting gear 6 other aircraft electric lifting device framves 7 that are provided with side by side, gauge panel at aircraft cockpit 1 is provided with gauge panel aircraft remote controller buttons 11, be provided with foot-operated aircraft remote controller buttons 12 at under-dash, also be provided with and control aircraft electric lifting device frame 7, parachute ejector 13, electric propeller propelling unit 15, and portable miniature remote controlled device 10, aircraft remote controller buttons 11, foot-operated aircraft remote controller buttons 12 and miniature remote controlled device 10 equal controllable starting aircraft electric lifting device framves 7 are opened.Gauge panel aircraft remote controller buttons 11 is two, divides the place ahead that is located at driver and copilot; Foot-operated aircraft remote controller buttons 12 is two, divides the front lower place that is located at driver and copilot.Be provided with multilayer parachute 14 and parachute ejector 13 at aircraft cockpit 1, aircraft passenger compartment 2, aircraft tail 3, aircraft port wing 4 and aircraft starboard wing 5 outside faces, multilayer parachute 14 is connected and composed successively by a plurality of parachutes, parachute ejector 13 is used for multilayer parachute 14 is ejected, and each parachute is opened.Be provided with electric propeller propelling unit 15 at aircraft passenger compartment 2 outside faces, electric propeller propelling unit 15 is 2, and be provided with the rotating mechanism of rotatable 60 degree directions, be used for aircraft and drop to densely populated urban area or high-lager building when overhead opening multilayer parachute 14, promote aircraft and waft from the danger zone; Or aircraft is when dropping on the water surface of great river, sea and each region, promotes aircraft and pulls in to shore or wait for rescue safe escape.In aircraft passenger compartment 2, be provided with complete monitoring device 8, in aircraft cockpit 1, aircraft passenger compartment 2, be provided with the complete monitoring device read-out 9 that shows complete monitoring device 8 monitoring contents, can make aviator, the interior Security Personnel of aircraft passenger compartment or attendant in time find aircraft by accidents such as terrified offender's abduction, and land a plane safely by aircraft remote controller buttons 11, foot-operated aircraft remote controller buttons 12 and miniature remote controlled device 10.Be provided with safety air bag 16 at aircraft cockpit 1, aircraft passenger compartment 2 outer bottoms and the right and left, when aircraft in when landing, if aircraft drops on the water surface of great river, sea and each region, at this moment also can pass through aircraft remote controller buttons 11, foot-operated aircraft remote controller buttons 12 and miniature remote controlled device 10 airbag openings 16, even aircraft landing is on the water surface, aircraft also can float on the surface, and the electric propeller propelling units 15 that start simultaneously rotatable 60 degree directions promote aircrafts and pull in to shore or wait for rescue safe escape.
Claims (5)
1. safe falling aircraft, comprise aircraft cockpit (1), aircraft passenger compartment (2), aircraft tail (3), aircraft port wing (4), aircraft starboard wing (5) and aircraft machinery alighting gear (6), aircraft cockpit is provided with control system and gauge panel in (1), it is characterized in that: at the other aircraft electric lifting device frame (7) that is provided with side by side of described aircraft machinery alighting gear (6); In aircraft passenger compartment (2), be provided with complete monitoring device (8); In aircraft cockpit (1), aircraft passenger compartment (2), be provided with complete monitoring device read-out (9); Gauge panel at aircraft cockpit (1) is provided with gauge panel aircraft remote controller buttons (11), is provided with foot-operated aircraft remote controller buttons (12) at under-dash; Be provided with multilayer parachute (14) and parachute ejector (13) at aircraft cockpit (1), aircraft passenger compartment (2), aircraft tail (3), aircraft port wing (4) and aircraft starboard wing (5) outside face; Be provided with electric propeller propelling unit (15) at aircraft passenger compartment (2) outside face.
2. a kind of safe falling aircraft according to claim 1, it is characterized in that: described aircraft cockpit (1), the outer bottom of aircraft passenger compartment (2) and the right and left are provided with safety air bag (16).
3. a kind of safe falling aircraft according to claim 1 and 2, it is characterized in that: described aircraft cockpit gauge panel aircraft remote controller buttons (11) is two, minute is located at the place ahead of driver and copilot; Foot-operated aircraft remote controller buttons (12) is two, divides the front lower place that is located at driver and copilot.
4. a kind of safe falling aircraft according to claim 1 and 2, it is characterized in that: described electric propeller propelling unit (15) is 2, and is provided with the rotating mechanisms of rotatable 60 degree directions.
5. a kind of safe falling aircraft according to claim 1 and 2 is characterized in that: also comprise control aircraft electric lifting device frame (7), parachute ejector (13), electric propeller propelling unit (15), and portable miniature remote controlled device (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201110362425.3A CN103112590B (en) | 2011-11-16 | 2011-11-16 | A kind of safe falling aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201110362425.3A CN103112590B (en) | 2011-11-16 | 2011-11-16 | A kind of safe falling aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103112590A true CN103112590A (en) | 2013-05-22 |
| CN103112590B CN103112590B (en) | 2015-09-23 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201110362425.3A Expired - Fee Related CN103112590B (en) | 2011-11-16 | 2011-11-16 | A kind of safe falling aircraft |
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| Country | Link |
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| CN (1) | CN103112590B (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104029813A (en) * | 2014-06-04 | 2014-09-10 | 深圳市万博鑫科技有限公司 | Aeronautic amphibious transport plane |
| CN104670502A (en) * | 2015-02-09 | 2015-06-03 | 武汉天降科技有限公司 | Helicopter in-flight shutdown safe-combination soft landing equipment and soft landing method |
| CN109683625A (en) * | 2018-08-29 | 2019-04-26 | 深圳市旭发智能科技有限公司 | A kind of method of unmanned plane layering landing |
| CN111284712A (en) * | 2020-03-03 | 2020-06-16 | 黄思源 | Method for saving lives of passengers after passenger plane accident |
| CN115027679A (en) * | 2022-06-23 | 2022-09-09 | 宋学恭 | Safe landing aircraft |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1036372A (en) * | 1988-11-26 | 1989-10-18 | 刘钢岩 | Lifesaving control system of civil aircraft |
| US20030094541A1 (en) * | 2001-11-16 | 2003-05-22 | Zeineh Rashid A. | Security & anti suicide-hijacking system for airplanes |
| US20030163232A1 (en) * | 2002-02-07 | 2003-08-28 | Moretto Jose Paul | Airliner irreversible-control anti-hijack system |
| CN101391654A (en) * | 2007-09-21 | 2009-03-25 | 厦门中虎网络科技有限公司 | Safety lifesaving airplane |
| US20110163200A1 (en) * | 2006-10-20 | 2011-07-07 | Lta Corporation | Lenticular airship |
| CN202345919U (en) * | 2011-11-16 | 2012-07-25 | 宋学恭 | Safely landing airplane |
-
2011
- 2011-11-16 CN CN201110362425.3A patent/CN103112590B/en not_active Expired - Fee Related
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1036372A (en) * | 1988-11-26 | 1989-10-18 | 刘钢岩 | Lifesaving control system of civil aircraft |
| US20030094541A1 (en) * | 2001-11-16 | 2003-05-22 | Zeineh Rashid A. | Security & anti suicide-hijacking system for airplanes |
| US20030163232A1 (en) * | 2002-02-07 | 2003-08-28 | Moretto Jose Paul | Airliner irreversible-control anti-hijack system |
| US20110163200A1 (en) * | 2006-10-20 | 2011-07-07 | Lta Corporation | Lenticular airship |
| CN101391654A (en) * | 2007-09-21 | 2009-03-25 | 厦门中虎网络科技有限公司 | Safety lifesaving airplane |
| CN202345919U (en) * | 2011-11-16 | 2012-07-25 | 宋学恭 | Safely landing airplane |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104029813A (en) * | 2014-06-04 | 2014-09-10 | 深圳市万博鑫科技有限公司 | Aeronautic amphibious transport plane |
| CN104670502A (en) * | 2015-02-09 | 2015-06-03 | 武汉天降科技有限公司 | Helicopter in-flight shutdown safe-combination soft landing equipment and soft landing method |
| CN109683625A (en) * | 2018-08-29 | 2019-04-26 | 深圳市旭发智能科技有限公司 | A kind of method of unmanned plane layering landing |
| CN111284712A (en) * | 2020-03-03 | 2020-06-16 | 黄思源 | Method for saving lives of passengers after passenger plane accident |
| CN115027679A (en) * | 2022-06-23 | 2022-09-09 | 宋学恭 | Safe landing aircraft |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103112590B (en) | 2015-09-23 |
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150923 Termination date: 20171116 |
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| CF01 | Termination of patent right due to non-payment of annual fee |