CN108910056A - A kind of aircraft with separable pressurized cabin - Google Patents
A kind of aircraft with separable pressurized cabin Download PDFInfo
- Publication number
- CN108910056A CN108910056A CN201810902072.3A CN201810902072A CN108910056A CN 108910056 A CN108910056 A CN 108910056A CN 201810902072 A CN201810902072 A CN 201810902072A CN 108910056 A CN108910056 A CN 108910056A
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- Prior art keywords
- cabin
- separable
- normal pressure
- sliding rail
- inseparable
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- 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.)
- Pending
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- 238000013016 damping Methods 0.000 claims description 7
- 230000011664 signaling Effects 0.000 claims description 5
- 239000011248 coating agent Substances 0.000 claims description 4
- 238000000576 coating method Methods 0.000 claims description 4
- 238000001816 cooling Methods 0.000 claims description 4
- 230000032258 transport Effects 0.000 abstract description 21
- 238000005520 cutting process Methods 0.000 abstract description 7
- 238000000034 method Methods 0.000 abstract description 5
- 230000008569 process Effects 0.000 abstract description 2
- 238000004378 air conditioning Methods 0.000 description 4
- 230000034994 death Effects 0.000 description 4
- 231100000517 death Toxicity 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 4
- 230000005484 gravity Effects 0.000 description 4
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 3
- 229910052760 oxygen Inorganic materials 0.000 description 3
- 239000001301 oxygen Substances 0.000 description 3
- 230000029058 respiratory gaseous exchange Effects 0.000 description 3
- 238000002679 ablation Methods 0.000 description 2
- 230000015556 catabolic process Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000006870 function Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000004064 recycling Methods 0.000 description 2
- 238000004904 shortening Methods 0.000 description 2
- 206010021143 Hypoxia Diseases 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000007954 hypoxia Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 230000008450 motivation Effects 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000004083 survival effect Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D25/00—Emergency apparatus or devices, not otherwise provided for
- B64D25/08—Ejecting or escaping means
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D17/00—Parachutes
- B64D17/80—Parachutes in association with aircraft, e.g. for braking thereof
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Body Structure For Vehicles (AREA)
Abstract
The present invention relates to a kind of aircrafts with separable pressurized cabin.Aircraft includes fuselage, wing, take-off and landing device, power device and control device, fuselage includes inseparable normal pressure cabin and separable pressurized cabin, automatic connection traction device draws the sliding rail sliding along cabin sliding rail and vehicle of separable pressurized cabin and passes in and out inseparable normal pressure cabin, and transport vehicle transports passenger in separable pressurized cabin and passes in and out urban district destination and departure place；Separable pressurized cabin includes cockpit and passenger compartment and normal pressure cargo hold, and Separable connecting device is equipped between cockpit and passenger compartment and normal pressure cargo hold；The flexible folding inflation wing and top that the two sides of the bottom of cockpit and passenger compartment are equipped with are equipped with parachute group；The parameter of the posture of the adjustable different parachute groups of pilot and the adjustment left and right flexible folding inflation wing, manipulates the process of landing during parachuting.The present invention effectively shortens non-cutting time for seizing the opportunity and the casualty rate for reducing airplane crash.
Description
Technical field
The present invention relates to civil aviation fields, and in particular to a kind of aircraft with separable pressurized cabin.
Background technique
Jet plane is efficiently mode of transportation in the existing vehicles, and there are also more economical oil for airliner of having a full house
Consumption, civil aviaton are the preferred traffic modes of middle and long distance travelling.Civil aviaton has the safety in statistical theory, is existing traffic work
Minimum casualty rate in tool is safest mode of transportation；But airplane crash, once occurring, civil aviaton is the highest traffic side of casualty rate
Formula, the especially death rate are highest in all modes of transportation.City the more is built the more big, and new airport the more is built the more remote, passes in and out from urban district
The time of outer suburbs airport consumption is increasingly longer, crowded safety check, more walking, and the non-cutting time seized the opportunity is increasingly longer.It seizes the opportunity
Non-cutting time refers to the time from origin to destination in addition to the flight time.The casualty rate of airplane crash is reduced, shortening multiplies
The non-cutting time of machine is that civil aviaton wishes the problem solved and the target constantly pursued in a hurry.
Airplane fault parachute assembly CN100480137C is under making aircraft that can delay aircraft in the event of a failure
Reduction of speed degree makes aircraft realize safe landing, reduce the advantages of injures and deaths and property loss, solves the wound for reducing airplane crash to a certain degree
Die rate.The probability of people survived has been significantly greatly increased in a kind of aircraft life-saving device CN102001447B.With can separate body and
It is slidably disposed therein the main cabin for being arranged into a column with multiple in the aircraft CN1148306C airplane skin of separate cabin, outside
Shell can be disconnected on predetermined fracture position with various methods, shell can by be mounted on can open position go forward mounting ring and rear peace
The controllable destructor filled in ring disconnects.A kind of subway system CN201710820734.8 shortening with terminal basic function
Non-cutting time is seized the opportunity, increases the competitiveness of civil aviation.
The above technology is not yet it is considered that need manipulation of the professional to parachute, time enough during parachuting
Select parachuting touchdown area；The high temperature chips float of destructor seriously threatens the safety of parachuting in the sky, reduces parachuting
Success rate；Additional jet-propulsion plant increases too many weight, reduces the economy of civil aviaton；Breakdown plane is greatly decreased in load
Afterwards, it is improved a possibility that automatic forced landing with success rate, the automatic Pilot technology recycling that unmanned plane can be used in breakdown plane is repaired.
Summary of the invention
The purpose of the present invention is：Shorten the non-cutting time seized the opportunity；Reduce airplane crash casualty rate, the especially death rate.
The technical solution adopted by the present invention is that：Passenger enters a kind of separable pressurization visitor from urban central zone departure place
Cabin without leaving main cabin, separates pressurized cabin according to weather and road conditions objective condition, selection visitor before reaching its destination
The means of conveyance in cabin, transport vehicle highway transportation, train railway transport, civil aviaton's air transport or steamer water transportation, convert traffic
It when mode and the vehicles, is dispatched as unit of separable pressurized cabin.Passenger reaches urban central zone purpose
Main cabin is just left behind ground.
A kind of aircraft with separable pressurized cabin includes fuselage, wing, take-off and landing device, power device and manipulation dress
It sets, fuselage includes inseparable normal pressure cabin, separable pressurized cabin, and signaling interface connects inseparable with power interface device
Normal pressure cabin and separable pressurized cabin.
Setting head hatch door, rear door, fixed locking damping device and cabin sliding rail, transport in inseparable normal pressure cabin
Vehicle includes sliding rail and headstock on automatic connection traction device, locking device, vehicle, and the automatic traction device that connects draws separable pressurization
Main cabin sliding rail sliding along cabin sliding rail and vehicle passes in and out inseparable normal pressure cabin, fixed locking damping device and locking device lock
Tightly separable pressurized cabin, transport vehicle transport passenger in separable pressurized cabin and pass in and out urban district destination and departure place.
Separable pressurized cabin includes cockpit and passenger compartment and normal pressure cargo hold, cockpit and passenger compartment and normal pressure cargo hold it
Between be equipped with Separable connecting device；The flexible folding inflation wing and top that the two sides of the bottom of cockpit and passenger compartment are equipped with are equipped with drop
Fall umbrella group；The outer surface of separable pressurized cabin is coated with evaporative cooling coating.
Aircraft with separable pressurized cabin is parked on horizontal airplane parking area, and the preceding height frame that rises and falls is high lower than rear undercarriage
Degree, thus the cabin lower than the cabin sliding rail at ventral, at ventral of cabin sliding rail at the head of inseparable normal pressure cabin
Sliding rail is lower than the cabin sliding rail at tail.Inseparable normal pressure cabin is slid into using gravity convenient for separable pressurized cabin.
A kind of apron floor that the aircraft with separable pressurized cabin can also use opens up the groove of similar track,
The ground groove of nose-gear is lower than the ground groove of rear undercarriage, when aircraft stops in a groove, inseparable normal pressure cabin
Cabin sliding rail at head lower than the cabin sliding rail at ventral, the cabin sliding rail at ventral is lower than the cabin sliding rail at tail.
Inseparable normal pressure cabin is slid into using gravity convenient for separable pressurized cabin.
After the present invention uses above-mentioned technology, shorten the non-cutting time seized the opportunity, a safety check in entire stroke, when not having walking
Between；If the waiting time that the time of scheduling is reasonable, not too many；It, can when the weather on arrival ground is not suitable for takeoff and landing
To be transformed to land transportation mode of transportation and the vehicles reached in the landing at the airport closed on.
Reduce airplane crash casualty rate, the especially death rate.The adjustable different parachute groups of pilot during parachuting
Posture, the parameter of the adjustable left and right flexible folding inflation wing, manipulates the process of landing during parachuting.It is separable to increase
Press main cabin that there is time enough to select parachuting touchdown area, pilot can accurately manipulate umbrella during parachuting, find choosing
It selects advantageous place and implements parachuting, extend the hang time, race against time for rescue, improve survival rate, separate pressurized cabin
The phase mutual friction of kinetic energy and gravitional force and atmosphere be converted into thermal energy, separate the hang time that pressurized cabin is detached from after aircraft
Longer, it is more abundant that its friction is converted into thermal energy, and kinetic energy and momentum are lower when landing, and impulse force is smaller, and casualty rate is lower.
Detailed description of the invention
Fig. 1 is the aircaft configuration schematic diagram with separable pressurized cabin；
Fig. 2 is separable pressurized cabin structural schematic diagram；
Fig. 3 is separable pressurized cabin sliding state schematic diagram；
Fig. 4 is transport vehicle travel position schematic diagram；
In figure：Inseparable normal pressure cabin 101, signaling interface and power interface device 102, cabin sliding rail 103, separable pressurization
Main cabin 104, cockpit 105, passenger compartment 106, the aircraft 107 with separable pressurized cabin, automatic connection traction device 108,
Sliding rail 109, locking device 110, headstock 111, transport vehicle 112 on vehicle；
Head hatch door 201, continuous-pressure breathing air-conditioning system 202, control system and its display screen 203, pilot 204, parachute group
205, flexible folding inflates the wing 206, inseparable normal pressure cabin rear door 207, normal pressure cargo hold 208, Separable connecting device
209, fixed locking damping device 210, evaporative cooling coating 211, automatic pilot and blind landing system 212；
Main support 301, sliding support 302, secondary bracket 303.
Specific embodiment
Embodiment 1：A specific embodiment of the invention is described in further detail below with reference to attached drawing.Such as Fig. 1
It is shown, a kind of aircraft 107 with separable pressurized cabin, including fuselage, wing, take-off and landing device, power device and control dress
It sets, fuselage includes inseparable normal pressure cabin 101, separable pressurized cabin 104, and separating pressurized cabin 104 includes cockpit
105 and passenger compartment 106.Cabin sliding rail 103 is set in inseparable normal pressure cabin 101, and automatic connection traction device 108 control can
It separates the sliding of sliding rail 109 along cabin sliding rail 103 and vehicle of pressurized cabin 104 and passes in and out inseparable normal pressure cabin 101, signaling interface
Inseparable normal pressure cabin 101 and separable pressurized cabin 104 are connected with power interface device 102.Transport vehicle 112 includes automatic
Traction device 108, locking device 110, sliding rail 109 and headstock 111 on vehicle are connected, the automatic traction device 108 that connects includes signal
Interface and power interface connection cockpit 105 and headstock 111, headstock 111 include power and control system, automatic connection traction dress
It sets 108 tractions and separates pressurized cabin 104, separate the sliding rail disengaging transport vehicle 112 and inseparable along vehicle of pressurized cabin 104
Normal pressure cabin 101, locking device 110 lock separable pressurized cabin 104, and transport vehicle 112 transports in separable pressurized cabin 104
Passenger passes in and out urban district destination and departure place.
Aircraft with separable pressurized cabin is parked on horizontal airplane parking area, and the preceding height frame that rises and falls is high lower than rear undercarriage
Degree, so that cabin sliding rail 103 at the head of inseparable normal pressure cabin 101 is lower than the cabin sliding rail 103 at ventral, at ventral
Cabin sliding rail 103 lower than the cabin sliding rail 103 at tail.Convenient for separable pressurized cabin 104 in connection traction device automatically
Gravity is utilized to slide into inseparable normal pressure cabin 101 under 108 control.
The groove similar to track can also be opened up in apron floor, be readily transported vehicle 112 and aircraft rapid abutting joint.It shuts down
The ground groove of nose-gear at the head of level ground ground is lower than the ground groove of the rear undercarriage at ventral, when aircraft is parked in groove
In, inseparable 101 head of normal pressure cabin is lower than ventral, and ventral is lower than tail, and separating pressurized cabin 104 can be by gravity
Effect, automatically connection traction device 108 control under, slide into inseparable normal pressure cabin 101.Notch end is provided with draining
Mouthful, in order to avoid ponding.The preferred road transport vehicle of transport vehicle 112.
As shown in Fig. 2, separable pressurized cabin 104 includes cockpit 105, passenger compartment 106 and normal pressure cargo hold 208, normally
State cockpit 105, passenger compartment 106 and normal pressure cargo hold 208 are the whole of a rigidity by the connection of Separable connecting device 209
Body.Signaling interface and power interface device 102 connect inseparable normal pressure cabin 101 and separable pressurized cabin 104, pilot
Aircraft flight is controlled using control system and its display screen 203；It is equipped with VR system in cockpit, pacifies on head, tail and wing
More panorama cameras are filled, pilot does not depend on any angle case that can visually observe without dead angle outside aircraft.Continuous-pressure breathing is empty
It is low in altitude low temperature that adjusting system 202 is that cockpit 105 and passenger compartment 106 provide pressurization, oxygen supply and air conditioning, especially aircraft
When forcing down oxygen environment flight or slide.
Separable 104 head of pressurized cabin is streamlined, approximate with inseparable 101 shape of normal pressure cabin, separates pressurization
Fixed locking damping device 210 is equipped between main cabin 104 and inseparable normal pressure cabin 101, preferably multiple independent air bags fill
Gas-solid is fixed, and the damage of single air bag does not influence fixed effect, and air bag has the function of bumper and absorbing shock.Separable pressurized cabin
104 are equipped at least three hatch doors, shorten the boarding time of passenger.Cockpit of 204 pilots in separable pressurized cabin 104
In 105, transport vehicle 112 is operated using control system and its display screen 203, transports passenger between urban district terminal and airport,
Passenger sets out and reaches in urban district terminal safety check boarding.
Embodiment 2：When awing encountering catastrophe failure pilot decision abandoning machine escape, it is first turned on inseparable
Secondly rear door 207 from normal pressure cabin 101 unclamps fixed locking damping device 210, finally opens head hatch door 201, powerful
Air-flow separable pressurized cabin 104 is blown out from inseparable normal pressure cabin 101, pilot guidance Separable connecting device
209 realization cockpits 105 and passenger compartment 106 are separated with normal pressure cargo hold 208, the voluntarily parachuting of normal pressure cargo hold 208, in order to find recycling
Satellite positioning device and satellite communication terminal is arranged in luggage in normal pressure cargo hold 208.At this point, separable pressurized cabin 104 is surplus
Lower cockpit 105 and passenger compartment 106, except the safe distance for avoiding engine wake flame ablation, pilot 204 opens separable
The flexible folding that 104 two sides of pressurized cabin are equipped with inflates the wing 206, then, opens the parachute group 205 that top is arranged in, can divide
Enter to slide from pressurized cabin 104 and continue controlled controHower with parachuting state, pilot, pilot 204 manipulates flexible folding
The inflation wing 206 and parachute group 205 slide the suitable parachuting landing site of selection and land.Evaporative cooling coating 211 can bear hair
Short time ablation of the motivation wake flame to separable pressurized cabin 104.Continuous-pressure breathing air-conditioning system 202 is cockpit 105 and passenger
The offer pressurization of cabin 106, oxygen supply and air conditioning, especially aircraft are when altitude low temperature hypobaric hypoxia environment slides.
If automatic pilot and 212 equipment of blind landing system are normal, aircraft can controlled flight, aircraft enters automatic Pilot
State is manipulated by ground flying person, finds possible place forced landing, recovery failure aircraft, and analyzing failure cause improves aircraft
Design and manufacture technique.
As shown in figure 3, pilot 204 manipulates telescoping mechanism, it is not drawn into figure, pushes sliding support 302 from tail to machine
The sliding of head direction, sliding support 302 push main support 301 to be unfolded, and drive the flexible folding inflation wing 206 to be unfolded, secondary bracket 303 is protected
The tail portion of the card flexible folding inflation wing 206 is sufficiently spread out, and is separated pressurized cabin 104 and is entered sliding mode；204 basis of pilot
The distributed data of main cabin person weight manipulates parachute group 205, and adjustment changes 205 parameter of parachute group, guarantees separable pressurization
104 level of approximation of main cabin slides, and avoids separable pressurized cabin 104 from sliding parameter out of control.
As shown in Figure 4, pressurized cabin 104 is separated including passenger compartment 106, normal pressure cargo hold 208 and connects dividing for they
From attachment device 209,106 the right and left of passenger compartment is equipped with flexible folding and inflates the wing 206, and top is equipped with parachute group 205.Vehicle
Upper sliding rail 109 and cabin sliding rail 103 are connected on more curved axis by multiple rubber wheels using bearing.Locking device 110 will
Separable pressurized cabin 104 and transport vehicle 112 are connected as a rigid body.The flexible folding inflation wing 206 is located at passenger compartment 106
Two sides bottom section plays the role of buffering pneumatic cushion first with ground face contact when failure is landed.
Embodiment 3：Transport vehicle 112, which can also be every train all, has the train of power and control system, more transports
It orbits after vehicle train marshalling list, there is punctuality.
The above is only presently preferred embodiments of the present invention, not does limitation in any form to the present invention, is appointed
What those skilled in the art, in the range of not departing from technical solution of the present invention, when the technology using the disclosure above
Content is modified or is modified to the equivalent embodiment of equivalent variations, but all without departing from technical solution of the present invention
Hold, simple modification, equivalent change and modification to the above embodiments, still falls within this hair according to the technical essence of the invention
In the range of bright technical solution.
Claims (2)
1. a kind of aircraft with separable pressurized cabin, including fuselage, wing, take-off and landing device, power device and control device,
It is characterized in that：Fuselage includes inseparable normal pressure cabin（101）With separable pressurized cabin（104）, signaling interface and power supply
Interface arrangement（102）Connect inseparable normal pressure cabin（101）With separable pressurized cabin（104）；
Inseparable normal pressure cabin（101）Interior setting head hatch door（201）, rear door（207）, fixed locking damping device
（210）With cabin sliding rail（103）, transport vehicle（112）Including connecting traction device automatically（108）, locking device（110）, Che Shang
Sliding rail（109）And headstock（111）, traction device is connected automatically（108）Draw separable pressurized cabin（104）Along cabin sliding rail
（103）With sliding rail on vehicle（109）Sliding passes in and out inseparable normal pressure cabin（101）, fixed locking damping device（210）And locking
Device（110）Lock separable pressurized cabin（104）, transport vehicle（112）Transport separable pressurized cabin（104）Interior passenger's disengaging
Urban district destination and departure place；
Separable pressurized cabin（104）Including cockpit（105）And passenger compartment（106）With normal pressure cargo hold（208）, cockpit
（105）And passenger compartment（106）With normal pressure cargo hold（208）Between be equipped with Separable connecting device（209）；Cockpit（105）With multiply
Main cabin（106）Two sides of the bottom be equipped with flexible folding inflation the wing（206）Parachute group is equipped with top（205）；It is separable to increase
Press main cabin（104）Outer surface be coated with evaporative cooling coating（211）.
2. a kind of aircraft with separable pressurized cabin described in accordance with the claim 1, it is characterised in that：With separable increasing
The aircraft in pressure main cabin is parked on horizontal airplane parking area, and the preceding height frame that rises and falls is lower than rear undercarriage height, thus inseparable normal pressure
Cabin（101）Head at cabin sliding rail（103）Lower than the cabin sliding rail at ventral（103）, cabin sliding rail at ventral
（103）Lower than the cabin sliding rail at tail（103）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810902072.3A CN108910056A (en) | 2018-08-09 | 2018-08-09 | A kind of aircraft with separable pressurized cabin |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810902072.3A CN108910056A (en) | 2018-08-09 | 2018-08-09 | A kind of aircraft with separable pressurized cabin |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108910056A true CN108910056A (en) | 2018-11-30 |
Family
ID=64393470
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810902072.3A Pending CN108910056A (en) | 2018-08-09 | 2018-08-09 | A kind of aircraft with separable pressurized cabin |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108910056A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109850136A (en) * | 2018-12-28 | 2019-06-07 | 唐强 | Aircraft flight is because of accident emergency gliding landing safety device |
| CN111284712A (en) * | 2020-03-03 | 2020-06-16 | 黄思源 | Method for saving lives of passengers after passenger plane accident |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1102163A (en) * | 1993-10-27 | 1995-05-03 | 陈治民 | Life-saving passenger cabin for civil airplane |
| CN2564472Y (en) * | 2002-08-26 | 2003-08-06 | 赵小荣 | Aircraft with separatable cabin and body |
| CN1663882A (en) * | 2005-03-31 | 2005-09-07 | 李震中 | Gliding type safety passenger plane |
| CN101148198A (en) * | 2007-10-31 | 2008-03-26 | 翁文辉 | Danger preventing airborne escaping method in civil airline passenger cabin ejected out the plane |
| CN101801784A (en) * | 2007-09-18 | 2010-08-11 | 邱垂文 | High passenger capacity airplane |
| CN105947223A (en) * | 2016-05-05 | 2016-09-21 | 莫国斌 | Split airplane |
| WO2018019075A1 (en) * | 2016-07-27 | 2018-02-01 | 冯政尧 | Aircraft having air crash lifesaving function |
-
2018
- 2018-08-09 CN CN201810902072.3A patent/CN108910056A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1102163A (en) * | 1993-10-27 | 1995-05-03 | 陈治民 | Life-saving passenger cabin for civil airplane |
| CN2564472Y (en) * | 2002-08-26 | 2003-08-06 | 赵小荣 | Aircraft with separatable cabin and body |
| CN1663882A (en) * | 2005-03-31 | 2005-09-07 | 李震中 | Gliding type safety passenger plane |
| CN101801784A (en) * | 2007-09-18 | 2010-08-11 | 邱垂文 | High passenger capacity airplane |
| CN101148198A (en) * | 2007-10-31 | 2008-03-26 | 翁文辉 | Danger preventing airborne escaping method in civil airline passenger cabin ejected out the plane |
| CN105947223A (en) * | 2016-05-05 | 2016-09-21 | 莫国斌 | Split airplane |
| WO2018019075A1 (en) * | 2016-07-27 | 2018-02-01 | 冯政尧 | Aircraft having air crash lifesaving function |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109850136A (en) * | 2018-12-28 | 2019-06-07 | 唐强 | Aircraft flight is because of accident emergency gliding landing safety device |
| CN111284712A (en) * | 2020-03-03 | 2020-06-16 | 黄思源 | Method for saving lives of passengers after passenger plane accident |
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Application publication date: 20181130 |
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