CN103112590B - A kind of safe falling aircraft - Google Patents
A kind of safe falling aircraft Download PDFInfo
- Publication number
- CN103112590B CN103112590B CN201110362425.3A CN201110362425A CN103112590B CN 103112590 B CN103112590 B CN 103112590B CN 201110362425 A CN201110362425 A CN 201110362425A CN 103112590 B CN103112590 B CN 103112590B
- Authority
- CN
- China
- Prior art keywords
- aircraft
- passenger compartment
- cockpit
- remote controller
- controller buttons
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Abstract
Name of the present invention is called a kind of safe falling aircraft.Belong to aircraft technology field.It mainly solve existing aircraft because of fault or be held as a hostage time can not the problem of safe falling.Its principal character is: be provided with aircraft electric lifting device frame on aircraft machinery alighting gear side; Complete monitoring device is provided with in aircraft passenger compartment; Complete monitoring device read-out is provided with in aircraft cockpit, aircraft passenger compartment; Gauge panel is provided with gauge panel aircraft remote controller buttons, is provided with foot-operated aircraft remote controller buttons at under-dash; Aircraft cockpit, aircraft passenger compartment, aircraft tail, aircraft port wing and aircraft starboard wing are provided with multilayer parachute and parachute ejector; Electric propeller propelling unit is provided with on the outer top of aircraft passenger compartment.The present invention have aircraft can not regular descent and aircraft when falling rapidly, aviator, security officers and attendant all can handle the feature landed a plane safely, and are mainly used in the aircraft possessing multiple safe falling support facility.
Description
Technical field
The invention belongs to aircraft technology field.Be specifically related to a kind of type aircraft possessing multiple safe falling support facility.
Background technology
Come from serious hope and the dream in fly blue sky, the mankind can carry the mankind and fly skyward carrier studying always over the past thousands of years, along with the development of 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 drives aviator's Aircraft Flight Test success, the dream that the mankind are aloft hovered as flying bird is made one's wish fulfilled finally, since then, has pulled open the prelude of mankind's science and technology of aviation great development.Along with human society is in military affairs, commercial affairs, tourism, logistics, geography, photography and all trades and professions development and efficient demand, aeronautical technology also obtains increasing application in human lives.
Because aircraft is in high-altitude flight, once because the overheated a variety of causes such as on fire of mechanical breakdown, rough weather impact, lightning strokes, flying bird collision, mechanical, oil circuit cause aircraft to stop aloft can not normal flight, usually can cause the tragedy of fatal crass.The generation of each air crash, not only allow victim family members overwhelmed with sorrow, bring huge loss to country, bring ill effect also to the reputation of aircraft industry.
So, how to make the safe falling aircraft of hommization? I thinks: people-oriented, with the life of people for supreme interest, sight being lengthened, it is far away to see, the safe altitude of aircraft industry reply passenger is responsible for, aircraft manufacturing producer should adopt safer new material and remove the safe falling aircraft of researching and developing more advanced technology, more feasible method manufacture can tackle various burst dangerous situation from the angle of safety, be no matter government or businessman's early investment than later stage more positive reparation 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, heavy many aircraft manufacturing producers also constantly drop into huge manpower and financial resources for how manufacturing safe falling aircraft always, but: airplane crash also is also continuing to show at continuation, each tragedy.
Summary of the invention
Object of the present invention is exactly provide a kind of after aircraft occurs involuntary stoppage aloft for above-mentioned weak point, aircraft can not regular descent and aircraft when falling rapidly, aviator on aircraft, security officers and attendant all can press button or the remote controller buttons of the operating aircraft that aircraft is arranged, a kind of safe falling aircraft landed 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 aircraft cockpit, it is characterized in that: be provided with aircraft electric lifting device frame side by side on described aircraft machinery alighting gear side; Complete monitoring device is provided with in aircraft passenger compartment; Complete monitoring device read-out is provided with in aircraft cockpit, aircraft passenger compartment; The gauge panel of aircraft cockpit is provided with gauge panel aircraft remote controller buttons, is provided with foot-operated aircraft remote controller buttons at under-dash; Aircraft cockpit, aircraft passenger compartment, aircraft tail, aircraft port wing and aircraft starboard wing outside face are provided with multilayer parachute and parachute ejector; Aircraft passenger compartment outside face is provided with electric propeller propelling unit.
The outer bottom of aircraft cockpit described in technical solution of the present invention, aircraft passenger compartment and the right and left are provided with safety air bag.
Aircraft cockpit gauge panel aircraft remote controller buttons described in technical solution of the present invention is two, divides the front being located at driver and copilot; Foot-operated aircraft remote controller buttons is two, divides the front lower place being located at driver and copilot.
Electric propeller propelling unit described in technical solution of the present invention is 2, and is provided with the rotating mechanism in rotatable 60 degree of directions.
Also comprise in technical solution of the present invention and control aircraft electric lifting device frame, parachute ejector, electric propeller propelling unit, and portable miniature remote controlled device.
The present invention is owing to comprising aircraft cockpit existing, aircraft passenger compartment, aircraft tail, aircraft port wing, on the aircraft basis of aircraft starboard wing and aircraft machinery alighting gear, aircraft electric lifting device frame is provided with side by side on aircraft machinery alighting gear side, complete monitoring device is provided with in aircraft passenger compartment, at aircraft cockpit, complete monitoring device read-out is provided with in aircraft passenger compartment, the gauge panel of aircraft cockpit is provided with gauge panel aircraft remote controller buttons, foot-operated aircraft remote controller buttons is provided with at under-dash, at aircraft cockpit, aircraft passenger compartment, aircraft tail, aircraft port wing and aircraft starboard wing outside face are provided with multilayer parachute and parachute ejector, aircraft passenger compartment outside face is provided with electric propeller propelling unit, thus when aircraft landing, as do not opened because of mechanical breakdown aircraft machinery alighting gear, aircraft electric lifting device frame button can be pressed electric lifting device frame is opened aircraft safety is landed, once there is chance failure in aircraft, aircraft is aloft stopped, at this moment aviator can with the foot-operated aircraft button of driver and copilot front lower place in the aircraft remote controller buttons on driver and copilot gauge panel in aircraft cockpit or aircraft cockpit, multilayer parachute with the miniature remote controlled device carried with, can eject and launches to hold in the palm aircraft slowly safe falling by the Security Personnel in aircraft passenger compartment or attendant by the starting of parachute ejector, when aircraft is in the process of landing, if be just in time when densely populated urban area or high-lager building overhead during aircraft landing, also can causes disaster, at this moment can start the electric propeller propelling unit in rotatable 60 degree of directions, promote aircraft and waft from danger zone, when aircraft is when landing, if aircraft drops on the water surface of great river, sea and each region, at this moment also can airbag opening, even if aircraft landing is on the water surface, aircraft also can float on the surface, and the electric propeller propelling unit simultaneously starting rotatable 60 degree of directions promotes aircraft and pulls in shore or wait for rescue safe escape.In addition, if broken down in driving compartment or occurred by contingencies such as terrified offender hijack, at this moment the Security Personnel in aircraft passenger compartment or attendant can press the miniature remote controlled device carried with, start above security procedure to land a plane safely, guarantee that the people's lives and property is not suffered a loss.Instant invention overcomes the deficiencies in the prior art, have aloft after aircraft occurs involuntary stoppage, aircraft can not regular descent and aircraft when falling rapidly, aviator on aircraft, security officers and attendant all can press button or the remote controller buttons of the operating aircraft that aircraft is arranged, the feature landed a plane safely.The present invention is mainly used in the aircraft possessing multiple safe falling support facility.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention.
Associated safety program display figure opened by Fig. 2 aircraft 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 that unexpected parachute ejects rear schematic diagram aloft.
Detailed description of the invention
As shown in Figures 1 to 5.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, control system and gauge panel is provided with, corresponding identical with existing aircraft in aircraft cockpit 1.Aircraft electric lifting device frame 7 is provided with side by side unlike on aircraft machinery alighting gear 6 side, the gauge panel of aircraft cockpit 1 is provided with gauge panel aircraft remote controller buttons 11, foot-operated aircraft remote controller buttons 12 is provided with at under-dash, also be provided with and can 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 all controllable starting aircraft electric lifting device frame 7 are opened.Gauge panel aircraft remote controller buttons 11 is two, divides the front being located at driver and copilot; Foot-operated aircraft remote controller buttons 12 is two, divides the front lower place being located at driver and copilot.Aircraft cockpit 1, aircraft passenger compartment 2, aircraft tail 3, aircraft port wing 4 and aircraft starboard wing 5 outside face are provided with multilayer parachute 14 and parachute ejector 13, multilayer parachute 14 is connected and composed successively by multiple parachute, each parachute for being ejected by multilayer parachute 14, and is opened by parachute ejector 13.Aircraft passenger compartment 2 outside face is provided with electric propeller propelling unit 15, electric propeller propelling unit 15 is 2, and be provided with the rotating mechanism in rotatable 60 degree of directions, for aircraft when opening multilayer parachute 14 and dropping to densely populated urban area or high-lager building overhead, promote aircraft and waft from danger zone; Or aircraft is when dropping on the water surface of great river, sea and each region, promotes aircraft and pull in shore or wait for rescue safe escape.Complete monitoring device 8 is provided with in aircraft passenger compartment 2, the complete monitoring device read-out 9 of display complete monitoring device 8 monitoring content is provided with in aircraft cockpit 1, aircraft passenger compartment 2, Security Personnel or attendant's Timeliness coverage aircraft can be made in aviator, aircraft passenger compartment by accidents such as terrified offender kidnap, and is landed a plane safely by aircraft remote controller buttons 11, foot-operated aircraft remote controller buttons 12 and miniature remote controlled device 10.Safety air bag 16 is provided with at aircraft cockpit 1, the outer bottom of aircraft passenger compartment 2 and the right and left, when aircraft is when landing, if aircraft drops on the water surface of great river, sea and each region, at this moment also by aircraft remote controller buttons 11, foot-operated aircraft remote controller buttons 12 and miniature remote controlled device 10 airbag opening 16, even if aircraft landing is on the water surface, aircraft also can float on the surface, and the electric propeller propelling unit 15 simultaneously starting rotatable 60 degree of directions promotes aircraft and pulls in shore or wait for rescue safe escape.
Claims (3)
1. a 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: be provided with aircraft electric lifting device frame (7) side by side on described aircraft machinery alighting gear (6) side; Complete monitoring device (8) is provided with in aircraft passenger compartment (2); Complete monitoring device read-out (9) is equipped with in aircraft cockpit (1) and aircraft passenger compartment (2); The gauge panel of 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; Aircraft cockpit (1), aircraft passenger compartment (2), aircraft tail (3), aircraft port wing (4) and aircraft starboard wing (5) outside face are provided with multilayer parachute (14) and parachute ejector (13); Aircraft passenger compartment (2) outside face is provided with electric propeller propelling unit (15); Described electric propeller propelling unit (15) is 2, and is provided with the rotating mechanism of rotatable 60 degree; Also comprise and control aircraft electric lifting device frame (7), parachute ejector (13) and electric propeller propelling unit (15), and portable miniature remote controlled device (10).
2. a kind of safe falling aircraft according to claim 1, is characterized in that: both outer bottoms of described aircraft cockpit (1) and aircraft passenger compartment (2) and the right and left are equipped with safety air bag (16).
3. a kind of safe falling aircraft according to claim 1 and 2, is characterized in that: described aircraft cockpit gauge panel aircraft remote controller buttons (11) is two, divides the front being located at driver and copilot; Foot-operated aircraft remote controller buttons (12) is two, divides the front lower place being located at driver and copilot.
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 CN103112590A (en) | 2013-05-22 |
| CN103112590B true CN103112590B (en) | 2015-09-23 |
Family
ID=48410992
Family Applications (1)
| 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 |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103112590B (en) |
Families Citing this family (4)
| 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 |
Citations (3)
| 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 |
| 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 |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20030094541A1 (en) * | 2001-11-16 | 2003-05-22 | Zeineh Rashid A. | Security & anti suicide-hijacking system for airplanes |
| US6845302B2 (en) * | 2002-02-07 | 2005-01-18 | Jose Paul Moretto | Airliner irreversible-control anti-hijack system |
| EP2076429B1 (en) * | 2006-10-20 | 2013-05-15 | LTA Corporation | Lenticular airship |
-
2011
- 2011-11-16 CN CN201110362425.3A patent/CN103112590B/en not_active Expired - Fee Related
Patent Citations (3)
| 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 |
| 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 |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103112590A (en) | 2013-05-22 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105644800B (en) | One kind is taken off warning system | |
| CN103112590B (en) | A kind of safe falling aircraft | |
| CN202400290U (en) | Plane distress separate cabin escape device | |
| WO2009039787A1 (en) | Safety rescue aircraft | |
| CN205098484U (en) | Aircraft launches system of fleing | |
| US10005559B2 (en) | Crash-resistant aircraft and crash-resistant control method | |
| CN107117316A (en) | A kind of detachable unmanned plane assisting in flying device | |
| CN1962362A (en) | Light airplane safe life-saving system | |
| DE112012001360B4 (en) | New kind of future airships | |
| CN101234671A (en) | Airplane with falling protecting device | |
| CN202345919U (en) | Safely landing airplane | |
| CN206068176U (en) | A kind of nacelle arrangement of fixed-wing aerial survey unmanned plane | |
| CN201432796Y (en) | Aircraft with safety protection device | |
| CN101927829A (en) | Passenger cabin-separable aircraft | |
| CN204399481U (en) | A kind of Aircraft Air stops safe soft landing equipment | |
| Khurana | Aviation management: global perspectives | |
| CN201169386Y (en) | Airplane with falling protection device | |
| CN203727641U (en) | Reconnaissance drone | |
| CN205010497U (en) | Novel prevent weighing down aircraft | |
| CN104890850A (en) | Dual-power dual-insurance solar airship | |
| CN205554619U (en) | Innovative multi -functional space shuttle | |
| CN213473505U (en) | Dual-engine layout self-gyroplane system | |
| Li et al. | On the peculiarities of shaping the appearance of aircraft equipped with a collective rescue system for passengers and crew | |
| CN113599738B (en) | Aviation fire extinguishing task control system and control method | |
| Gheorghiu et al. | Survivability rate among pilots in case of ejection |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150923 Termination date: 20171116 |