CN1342589A - Flying apparatus - Google Patents

Flying apparatus Download PDF

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Publication number
CN1342589A
CN1342589A CN 00126535 CN00126535A CN1342589A CN 1342589 A CN1342589 A CN 1342589A CN 00126535 CN00126535 CN 00126535 CN 00126535 A CN00126535 A CN 00126535A CN 1342589 A CN1342589 A CN 1342589A
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CN
China
Prior art keywords
vehicle body
vehicle
vehicle frame
fin
parachute
Prior art date
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Pending
Application number
CN 00126535
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Chinese (zh)
Inventor
赵翼华
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Individual
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Individual
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Publication date
Application filed by Individual filed Critical Individual
Priority to CN 00126535 priority Critical patent/CN1342589A/en
Publication of CN1342589A publication Critical patent/CN1342589A/en
Pending legal-status Critical Current

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Abstract

A flying vehicle is composed of vehicle body, vehicle frame, wings, propellers, power unit, hydrogen gas bag on vehicle top and parachute. The pot-shaped vehicle frame has vehicle body inlaid in it. The ring-shaped wings are around the vehicle frame layer by layer. The lifting propellers are installed to top layer of wings. The hydrogen gas bag and parachute are arranged on top of vehicle body. The power unit containing turbine engine, speed reducer and oil tank is attached to the bottom layer of wings. The advancing propellers are installed in the frout of wings. Its advantages are high safety, amphibious performance, vertical taking off and landing, and low cost.

Description

Driving
The present invention relates to a kind of aircraft that is used for communications and transportation.
Since earlier 1900s Lai Te brother creates first airplane, very big variation has taken place in aircraft between this a century, also become the main vehicle of people's trip gradually, the moving velocity that is higher than train and automobile and steamer because of its flying speed far away, shortened people's hourage greatly, brought convenience and quick to people.But at present with regard to China people's economic life level, still a few peoples of the airplane of the official business that travels away from home, majority still take landway traffic tool---automobile and train.In recent years, along with the raising of people's living standard, the increase of income, domestic automobile quantity constantly increases, and makes the city traffic of China be faced with huge pressure, and traffic congestion, traffic congestion happen occasionally, and city environment has also suffered serious automobile exhaust pollution.
The purpose of this invention just provides a kind of can taking off vertically, and is safe, improves the vehicle of land face congested traffic condition.
The main technical schemes of this invention is as follows:
Driving, it has vehicle body, vehicle frame, the wing, propeller and engine installation.Wherein the top of vehicle body is provided with hydrogen bag and parachute, and vehicle frame is a pot shape, and vehicle body is embedded in the vehicle frame.Be provided with ringwise fin on the surface of vehicle frame, fin is in layer around whole vehicle frame; The shock-reducing rubber that the lift propeller is housed on the superiors' fin and connects vehicle body fastens that (it is surrounded by shock-reducing rubber outside by screw rod and forms, on screw rod, have a pin-and-hole, can make vehicle frame and body contact by latch), the engine installation and the car pin that contain turbine engine, drop-gear box, fuel tank are housed on the orlop fin, the propeller of advancing also are housed at the front end of fin.
This invention has easy and simple to handle, and is safe, must not take the advantage in too much place.
Below in conjunction with accompanying drawing this invention is further described.
Fig. 1 is a FC-2 type driving schematic appearance; Fig. 2 is a FC-2 type vehicle body scheme drawing; Fig. 3 is a FC-2 type vehicle frame scheme drawing; Fig. 4 is FC-2 type emergency state figure; Fig. 5 is a retarder scheme drawing in this inventive embodiments; Fig. 6 is a FC-1 type driving schematic appearance; Fig. 7 is a FC-1 type vehicle body scheme drawing; Fig. 8 is a FC-1 vehicle frame scheme drawing; Fig. 9 is FC-1 type emergency state figure.
As shown in the figure, driving has vehicle body, vehicle frame, the wing, propeller and engine installation, and the top of vehicle body 2 is provided with hydrogen bag 1 and parachute 11, parachute 11 be positioned at hydrogen bag 1 the bottom both be connected the top of vehicle body 2 by removable pin.This removable pin is connected with handle in the driving compartment by steel rope.Vehicle body 2 offers car door 12 and vehicle window, and vehicle frame is a pot shape, and vehicle body 2 is embedded in the vehicle frame, is provided with ringwise fin 5 on the surface of vehicle frame, and fin 5 is in layer around whole vehicle frame; The shock-reducing rubber bolt 3 of 8 lifting propellers 4 and connection vehicle body 2 is housed on the superiors' fin, fuel tank, drop-gear box and turbine engine equal power device 8 and car pin 7 are housed on the orlop fin, vehicle frame also has a car door over against the position of the car door of vehicle body 2, front end at fin also is equipped with forward propeller 9, and three grades of dash plates when being used for water landing also are housed below fuel tank.Drop-gear box is the discus shape, and it links to each other with turbine engine by middle big gear wheel 14, forms 8 mouths 13, adds the direct port of turbine engine, and this drop-gear box has 9 output ports.
Open car door, have the stair function, can walk up, open the vehicle body door and advance then in the car cabin along it at the car door of the wing.At first, open the various instrument of main supply switch mode of operation (its electric energy is to be provided by storage battery) is provided, ignition engine then, by the close power-transfer clutch of lifting propeller 8 of hydraulic efficiency pressure system, clutch device is at the retarder output port, it is positioned at retarder output port place, at this moment, lifting propeller 8 enters mode of operation, then, souping up is when lift during greater than gravity, driving begins to go straight up to, if carry out low-latitude flying (its relative height can not above 1500 meters) then need not open forward propeller,, make it obtain forward power by regulating the angle of four lifting propellers on the wing, the similar helicopter of its this control system, but its flying speed can not surpass 100 kilometers/hour, and this speed limit is in order to guarantee when the driving engine et out of order, its descending speed can be too not fast, by parachute and the enough bondsmans' of the wing safety.When the needs high-speed flight, must go straight up to height more than 1500 meters, the power-transfer clutch of the forward propeller of closing then, when the flying speed instrument shows that its speed reaches predetermined speed, in the time of can producing with the cooresponding lift of gravity by the wing, good the angular adjustment of the wing, then the power-transfer clutch of lifting propeller is opened, at this moment, lifting propeller quits work.When arriving at the destination, at first will slow down, moderating process is as follows, opens lifting propeller, wait its running velocity just often, at this moment screw propeller in the time of before turning off adjusts the angle of four lifting propellers on the wing backward, the oblique rear of power that the lifting propeller above it produces, so, it can produce a power backward, and aircraft is slowed down, when advancing speed near zero the time, is the angular adjustment of four lifting propellers on the wing zero, at this moment, lifting propeller only produces lift, and driving just hovers in the air, when reducing horse-power-hour, lift just no longer reduces horsepower during less than gravity, allows its slow whereabouts.If running into driving engine et out of order or retarder aloft destroys, can be by being located at a urgent draw ring at the preceding top of operator's station, (it is connected with removable pin by steel cable,) pull out removable pin, the hydrogen bag at top passes through buoyancy, parachute is taken in the air, stretching stay cord, at this moment, because the resistance of parachute, the speed of driving can be slack-off, can descend with the speed below 30 kilometers/hour at last, in the decline process, the electricity of available storage battery, transfer to the forward propeller back with electrical motor in, can select the level point within the specific limits.Because the fuel tank below it is surrounded by non-conductive floating drum with it outward, when it lands on the water, can float whole aircraft come, because the bottom is provided with the dash plate of three circles, vibration reduces in the time of making entry, speed is slack-off gradually.And float over aerial hydrogen bag and parachute, and all can play the effect of sail, it is racked to the bank.If driving engine is on fire, can in water, land, if there is not the waters, then can whole vehicle frame and engine oil tank once all be fallen, and aircraft security is landed by parachute and hydrogen by another draw ring on operator's station.
Its bottom-to-top-height of FC--1 type driving (seeing figure) is 3.88 meters, and length and width are 5.2 meters, can sit four-player in the railway carriage, is the private savings type, it its be divided into: vehicle body, wing, car pin.
Vehicle body: it is to be made by aluminium alloy plate, and the observation place is used in the place ahead, has window, is made by high strength glass, and both sides also have window, and a side has door, is instrument and operator's station foremost.Height is 1.46 meters in the vehicle window, the people can only keep the posture of sitting inside, its loam cake is that a diameter is 3.6 meters a plectane, the high-strength plastic bin is housed on the plectane, the hydrogen bag just is contained in above the plastic processing frame, both connect with removable pin, are connected to parachute and stay cord around the hydrogen bag, and they are all ensconced between hydrogen bag and the parachute.
Wing: it has very big difference with the aircraft wing, and it is circular, and material is the thick aluminium alloy plate of 2mm, is made up of many annulus, and a uppermost annulus is an oblate ring of bilayer, and bilayer thickness is 0.05 meter, and eight lifting propellers are housed above.The wing a forward propeller is housed foremost.On bottom a slice rondelle fin, fuel tank and drop-gear box and turbine engine are housed, a side has door.It has the function of aircraft wing function and protection vehicle body.
The car pin: it is attached on the fin with bolt, and it has the landing buffer capacity.
Engine installation: one 200 kilowatts turbine engine, and a new type speed reducer and 9 two bladed propellers.
Technical data: 4.6 meters of wing diameters.
Weight data: maximum take-off weight 1200KG, unloaded weight 500KG, oily 300KG, load-carrying 300KG.
Performance data: flying speed 0---400 kilometer/hour.
Other device: relative height instrument, absolute altitude instrument, velocity indicator, hydraulic efficiency pressure system, automatic-balancing system, storage battery.
FC--2 type driving (seeing figure), it highly is 6.5 meters, length and width are 9.5 meters, can sit 22 people in the railway carriage, drive window can be sat two people, after freight house and sanitary accomodation are arranged.It is divided into is three parts: vehicle body, wing, car pin.
Vehicle body: it is to be made by aluminium alloy plate, and the position that the place ahead is used to observe has window, is made by high-strength glass, and both sides have window, and the back has door, and the height in the vehicle window is 1.95 meters, and the centre is the aisle, and both sides one row sits seat for 10 person-times.Its loam cake is that a diameter is 6.8 meters a plectane, and aluminium alloy frame is housed on the plate, is annular arrangement, and the hydrogen bag just is contained in above the frame, and both connect with removable pin, is connected to parachute and stay cord around the hydrogen bag, and they are all ensconced between hydrogen bag and the parachute.
Wing: it has very big difference with wing, and it is an annular arrangement, and material is the thick aluminium alloy plate of 4mm, is made up of many circular ring plates, and an annulus of going up most is an oblate ring of double-ply, and bilayer thickness is 0.1 meter, and eight lifting propellers are housed above.The wing a forward propeller is housed foremost, on nethermost a slice circular plate type wing, fuel tank and drop-gear box and turbine engine are housed, the back has door, it has function on the aircraft wing and two kinds of functions of protection vehicle body.
The car pin: be fixed on the wing and the dash plate, it has buffer capacity when landing.
Engine installation: two 700 kilowatts turbine engine (standby) and a new type speed reducer and 9 two bladed propellers.
Technical data: 9.5 meters of wing diameters.
Weight data: maximum take-off weight 4000KG, the heavy 1300KG of empty machine, oily 1000KG, load-carrying 1500KG;
Performance data: flying speed 0---400 kilometer/hour;
Other device: relative height instrument, absolute altitude instrument, velocity indicator, hydraulic efficiency pressure system, automatic-balancing system, storage battery.
If when running into engine breakdown aloft, can use alternative engine, if alternative engine can not use or retarder breaks down, the draw ring of a control parachute that so just can be by being located at the preceding top of operator's station, it connects together by steel cable and removable pin, pull out pin after, the hydrogen bag at top passes through buoyancy, the landing band is got on to open, at this moment, because the parachute resistance, the speed of driving is slack-off, when following when being land, available storage battery by propeller with electrical motor, select level point, jettisoning vehicle frame at the appropriate time in certain limit, expendable weight, make driving speed when landing less than 30 kilometers/hour.If the level point is very wide waters, so, just can not the jettisoning vehicle frame because on vehicle frame, have floating drum with and the bottom five entry dash plates are arranged, can float after whole driving is in falling into water, the vibration of entry is little.
1, hydrogen bag 2, vehicle body 3, shock-reducing rubber bolt 4, lifting propeller 5, wing 6, driving center of gravity place 7, car pin 8, driving power set 9, forward propeller 10, torsion rope 11, parachute 12, car door 13, clutch end 14, gear

Claims (3)

1. aircraft, it has vehicle body, vehicle frame, the wing, screw propeller and engine installation, it is characterized in that: the top of vehicle body [2] is provided with hydrogen bag [1] and parachute [11], and vehicle frame is a pot shape, and vehicle body [2] is embedded in the vehicle frame.Be provided with ringwise fin [5] on the surface of vehicle frame, fin [5] is in layer around whole vehicle frame; The shock-reducing rubber bolt [3] of lifting propeller [4] and connection vehicle body is housed on the superiors' fin, the engine installation [8] and the car pin [7] that contain turbine engine, drop-gear box, fuel tank are housed on the orlop fin, forward propeller [9] also are housed at the front end of fin [5].
2. a kind of aircraft as claimed in claim 1, it is characterized in that: vehicle body [2] is leak free pot shape body, the parachute at its top [11] is positioned at the bottom of hydrogen bag [1], both are fixed on the top of vehicle body [2] by removable pin, the handle that this removable pin connects in steel rope and the driving compartment is connected, and has car door [12] and vehicle window on the vehicle body [2].
3. a kind of aircraft as claimed in claim 1 is characterized in that: subtract the device case and be the discus shape, it links to each other with turbine engine by middle big gear wheel [14], forms eight mouths [13].
CN 00126535 2000-09-13 2000-09-13 Flying apparatus Pending CN1342589A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 00126535 CN1342589A (en) 2000-09-13 2000-09-13 Flying apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 00126535 CN1342589A (en) 2000-09-13 2000-09-13 Flying apparatus

Publications (1)

Publication Number Publication Date
CN1342589A true CN1342589A (en) 2002-04-03

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ID=4591856

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 00126535 Pending CN1342589A (en) 2000-09-13 2000-09-13 Flying apparatus

Country Status (1)

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CN (1) CN1342589A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103003148A (en) * 2010-06-08 2013-03-27 威尔海德救援公司 Life-saving vehicle
US10464668B2 (en) 2015-09-02 2019-11-05 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
US10875658B2 (en) 2015-09-02 2020-12-29 Jetoptera, Inc. Ejector and airfoil configurations
US11001378B2 (en) 2016-08-08 2021-05-11 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
US11148801B2 (en) 2017-06-27 2021-10-19 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103003148A (en) * 2010-06-08 2013-03-27 威尔海德救援公司 Life-saving vehicle
CN103003148B (en) * 2010-06-08 2015-06-17 威尔海德救援公司 Life-saving vehicle
US10464668B2 (en) 2015-09-02 2019-11-05 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
US10875658B2 (en) 2015-09-02 2020-12-29 Jetoptera, Inc. Ejector and airfoil configurations
US11001378B2 (en) 2016-08-08 2021-05-11 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
US11148801B2 (en) 2017-06-27 2021-10-19 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles

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