CN101628532A - flying automobile - Google Patents

flying automobile Download PDF

Info

Publication number
CN101628532A
CN101628532A CN200810045544A CN200810045544A CN101628532A CN 101628532 A CN101628532 A CN 101628532A CN 200810045544 A CN200810045544 A CN 200810045544A CN 200810045544 A CN200810045544 A CN 200810045544A CN 101628532 A CN101628532 A CN 101628532A
Authority
CN
China
Prior art keywords
engine
aero
automobile
compartment
car
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.)
Pending
Application number
CN200810045544A
Other languages
Chinese (zh)
Inventor
陈昌志
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN200810045544A priority Critical patent/CN101628532A/en
Publication of CN101628532A publication Critical patent/CN101628532A/en
Pending legal-status Critical Current

Links

Images

Landscapes

  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

The invention discloses a flying automobile, which consists of an aviation jet engine or a propeller type aero-engine based on the structure of a common automobile. The flying automobile is provided with two sets of engines and operating mechanism systems which are mutually independent, and integrates the function of the common automobile and the function of a helicopter. As the picture, an aero-engine 1 and an engine U-shaped frame 2 can carry out parallel telescopic movement and reciprocating rotation of 360 degrees through a hydraulic operating device to change a working mode and a working state of the aero-engine 1. Two working conditions of the automobile and the helicopter can be converted at will according to requirements. The top of a carriage is provided with a special parachute which can be opened to ensure the flying safety at emergency. The flying automobile has the properties of safety, reliability, convenience, maneuverable working mode and wide application, is military and civil, and has good development and application prospects.

Description

Hovercar
Technical field:
The present invention and car opertion function, mode of operation are relevant.
Background technology:
Existing automobile all is to travel on the highway of land, it almost is difficult to move even one step leaving highway, my technical innovation is can only to travel on the highway of land and can aloft fly in order to allow automobile be not limited to, and enlarges car opertion scope, effect and working space.As meet war, disaster, when reasons such as highway and bridge are damaged, traffic accident make the land traffic interrupted, just hovercar can in minutes take off vertically in the original place task of finishing the work of entering before the flight in the place of being obstructed aloft.
Hovercar is used very extensive: as rescue and relief work, lifting heavy duty equipment, 110 police cars, 119 fire extinguishing tankers, 120 medical trucks, tourism passenger traffic, the goods and materials transportation, military armored motor cares etc. can both use, and this type of car is the military or civilian good development prospect that all has.
Summary of the invention:
The objective of the invention is in order to change the working condition of existing automobile, change the history that running car be unable to do without the land highway, automobile not only can be travelled on the highway of land, can aloft fly again, and be to take off vertically in the original place and the destination vertical landing, very safe ready is quick.Automobile increases the new function of flight, expands new usage space, make this easily the vehicle safer, serve for the human society all our undertakings easily.
The present invention is achieved in that
Hovercar than long 1 to 2 meter of common car body commonly used, is a new car that has automobile function and autogyro function fully only from seeing that in appearance with existing automobile almost be the same.The present invention is that example is carried out the explanation of structure and principle design with Nanjing IVECO, the all-cis vehicle of Ford: in the compartment, the rear installs two aircraft jet engines additional, about each one, shown among Fig. 31, when needs travel with the general-utility car operating mode, at this moment all just the same with the function and the operation of general automobile, aircraft jet engine is placed on and does not need work in the compartment fully.Structure as shown in Figure 6, the gravity of a whole set of aero-engine device passes on base 10 by 3,5 and four bearing support of quadruplet bearing, aero-engine 1, U type support 2 and bearing 3 be with axle 4 be unified into one can parallel telescopic moving integral body, driving engine 1, U type support 2 and bearing 3, axle 4 can be 360 degree through hydraulic actuated and back and forth rotate.Bearing 5 and support are fixed installations, and there is the sliding poor parallel telescopic moving usefulness that supplies support 3 bottoms with base 10, and the effect of 3 struts is to make driving engine more stable when work.
Flight control principle: when needs are operated in the flight operating mode, need perform several preceding preparations of flight operating mode.At first with the car door opening of both sides, compartment, as shown in Figure 3.Operating hydraulically operated as shown in Figure 6 transmission device is with the aircraft jet engine 1 parallel control position that moves to the outer driving engine of compartment car door, at the same time, interlock can also be followed the parallel control position that moves to support by parallel mobile bearing 3 simultaneously with the hydraulic gear both sides.3 struts 1 are installed fastening by shown in Figure 4, closed the both sides car door, open tailstock ground floor car door with hydraulic efficiency gear.
Carry out shown in Fig. 3,4,6 and after the above-mentioned pre-flight preparation, just can operating hydraulically operated steering unit be spent by driving engine right-hand revolution 90,3 make jet tail mouth downward as shown in Figure 5, the beginning engine on, open the throttle wide, after the lift that makes progress that driving engine produces makes automobile rise to the height of flight needs, operating hydraulically operated steering unit rotates about 90 degree with the driving engine anticlockwise direction, as shown in Figure 21, driving engine is parallel jet tail mouth backward, and the thrust that driving engine produces can make automobile flight advance.When not needing to be operated in the flight operating mode and will land ground, regulate throttle on the one hand and reduce flying height, two operating hydraulically operated devices are regulated the back door and are opened to the control flight orientation, three usefulness hydraulic control mechanisms are with driving engine right-hand revolution 90 degree slowly, make jet tail mouth downward, regulate throttle, make lift that driving engine produces gravity less than automobile, the automobile that makes the flight operating mode slowly safe falling in the destination.When arriving ground and need recover vehicle behavior, open both sides car door complete removal strut, close and turn to tail gate, operating hydraulically operated steering unit moves on in the compartment driving engine is parallel, closes both sides, compartment car door.
The control of hovercar flying height and adjusting: main mode is to regulate the aero-engine throttle to carry out, the 2nd, and slowly clockwise direction or anticlockwise direction rotation are regulated with driving engine with hydraulic control mechanism.
The control of heading and adjusting: as shown in figure 13, have the open and close direction of automobile-used hydraulic control mechanism adjusting tailstock ground floor two car doors in compartment to get final product.The car in no compartment can be installed small aero at the tailstock, regulates the direction of rotation aero-engine through hydraulic control mechanism.
For guaranteeing the hovercar safety in when flight, in the special ad hoc parachute storehouse that is equipped with, the top in compartment, two sliding doors are in closed condition at ordinary times, shown in Fig. 9,10, when automobile aloft flies,, open the door earlier just in case there was a mechanical failure, can touch the button or draw guard hoop when the emergency state, ejection is earlier opened a drogue-parachute and is taken the big parachute of multilayer again out of to protect flight safety.Be provided with two storied gate in the back, compartment, shown in Figure 12,13, ground floor door purposes is to open to be used to regulate heading when the flight operating mode, and second layer door is mainly used in safety precaution.
Description of drawings:
Fig. 1 is the vehicle behavior scheme drawing.
Fig. 2 is one of flight preparation and one of flight working condition chart, 1 jet engine among the figure, engine with two U type frame, 3 car bodies.
Fig. 3 be driving engine in the compartment set-up diagram and pre-flight set-up dirgram two, 1 driving engine among the figure, 2 mobile bearings and support, 3 car bodies.
Fig. 4 is three of a flight set-up dirgram, 1 strut among the figure, 2 bearings, 3,4 movable supporting frames, 5 car bodies, 6 car doors.
Fig. 5 is a flight set-up dirgram four, 1 strut among the figure, 2 driving engine U type framves, 3 driving engines, 4 car bodies.
Fig. 6 is that driving engine hydraulic pressure is handled parallel shifting principle figure, 1 driving engine among the figure, and 2 driving engine U type framves, 3 can parallel mobile bearing and support, 4 hydraulic efficiency gear transmission shafts, 5 fixed installation bearing and supports.The 6 rotatable hydraulic actuators of regulating, 7 hydraulic actuator pistons, 8 hydraulic actuator swing pinions, 9 hydraulic actuator ratch, 10 bases.
A, b are driving engine and U type frame assembly drowing among Fig. 7, and c, d are mobile bearing and support scheme drawing.
Fig. 8-a, b are that driving engine hydraulic pressure is handled translation and rotation schematic diagram, 1 hydraulic actuator axle among the figure, the bearing of 2 fixing installings, the 3 rotatable hydraulic efficiency gear of regulating, 4 hydraulic actuator pistons, 5 hydraulic actuator swing pinions, 6, the support of 7 fixing installings, 8 hydraulic actuator ratch, 9 hydraulic actuator axles, 10 driving device pistons, 11 hydraulic actuators.
Fig. 8-c is that the support of hydraulic actuator ratch is slided poor.
Fig. 9-the slip of a2 car body top parachute door, b strengthening rib, c strengthening rib and parachute suspension ring.
Figure 10 is that parachute is opened the work scheme drawing, 1 umbellule among the figure, 2 multilayer gamps.
Figure 11 is compartment two lavatory sliding door scheme drawings, 1 sliding door among the figure, and 2 slide is pickled with grains or in wine.
Figure 12-a is that the back, compartment is used for the heading adjustment doors, b curtain-type safety protective door c barrier formula safety protective door.
Figure 13 is that the back, compartment is used for heading adjustment doors adjusting scheme drawing, 1 direction adjustment doors among the figure, 2 hydraulic actuators.
Figure 14 is the strut scheme drawing, 1 lead screw among the figure, 2 struts, 3 movable joints.
Figure 15 is one of hydraulic actuator systematic schematic diagram, 1 hydraulic efficiency gear among the figure, 2 pistons, 3,4 hydraulic actuator racks, 5 hydraulic actuator pistons, 6 fluid transmission gears, 7 fluid control by-pass cockes, 8 fuel tanks, 9 oil pipes, 10 safety valves, 11 oil pumps.
Figure 16 is one of hydraulic actuator systematic schematic diagram, 1 driving engine among the figure, 2U type support, 3 mobile bearings and support, 4 hydraulic actuator axles, 5 fixed type bearings and support, 6 hydraulic actuators, 7 hydraulic actuator pistons, 8 fluid transmission gears, 9 hydraulic actuator racks, 10 fluid control by-pass cockes, 11 oil pipes.
The specific embodiment:
1, the design speed per hour is preferably 200 to 600 kilometers, is up to 800 kilometers.
2, the highest being defined as below the 5000m of flying height suggestion, general run of thins is 1000 to 2000 meters, never conflicts with airliner generation Flight Path, concrete conditionality condition must be by national blank pipe regulation.
3, aero-engine can install the postmedian at car body, looks the purposes of car and allocation has the Light-duty Vehicle in compartment can be installed in the car, and driving engine is selected for use jet-propelled for best; The heavy goods vehicles in no compartment can be installed on the car body as usefulness car engines such as lifting, fire-fightings, and driving engine can be selected for use jet-propelled or the rotary propeller type aero-engine, generally installs 2 to 3.
4, alleviate own wt as far as possible for fuel-economizing, adopt light metal material to make.
5, the power of driving engine needs according to vehicle, purposes, and deadweight and load carrying ability calculate and decide.
6, be arranged in the compartment as engine location, adopt giant tyre as far as possible.

Claims (5)

1, hovercar not only has the function of general-utility car but also have the function of autogyro.Can make general-utility car on ground and use, travel and interruptedly can take off vertically, can do autogyro in the original place and use and take off vertically, land, two kinds of operating modes optionally can indiscriminately ad. as one wishes be changed.He is at principal character: be equiped with driving engine and maneuvering system that automobile and aircraft work alone separately on the basis of existing automobile.
2, according to right 1, two and above aviation jet engine in being arranged, the car in compartment are housed, the vehicle in no compartment, aero-engine can be contained on the car body, and looking the vehicle purposes can many mounted engines platform number.Driving engine can be selected the aviation jet engine for use, available again rotary propeller type aero-engine.Principal character is: need be operated in flight during operating mode and do not need to be operated in when flying operating mode, move and be the reciprocating type rotation of 360 degree, the steering angle of control and regulation aero-engine and mode of operation and the mode of operation that the orientation can change its hovercar through the hydraulic actuated driving engine is can be parallel telescopic.
3, be equiped with two storied gate at the tailstock that the compartment is arranged, the ground floor door is used to control to adjust heading through hydraulic actuated, and second layer door is used for safety precaution.Regulate heading at the little aero-engine that a vehicle tailstock portion energy of installing in no compartment is regulated rotational angle by hydraulic actuated.
4, be provided with the parachute storehouse at the roof that the compartment is arranged, built-in special parachute.Principal character is: launch earlier during use and open top umbellule, take following multilayer main chute out of by umbellule again and guarantee flight safety.
5, be equiped with hydraulic actuated, control, control system device on the car.Whole manipulations of jet engine or rotary propeller type aero-engine, control, adjusting all thus device finish.
CN200810045544A 2008-07-14 2008-07-14 flying automobile Pending CN101628532A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN200810045544A CN101628532A (en) 2008-07-14 2008-07-14 flying automobile

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN200810045544A CN101628532A (en) 2008-07-14 2008-07-14 flying automobile

Publications (1)

Publication Number Publication Date
CN101628532A true CN101628532A (en) 2010-01-20

Family

ID=41573875

Family Applications (1)

Application Number Title Priority Date Filing Date
CN200810045544A Pending CN101628532A (en) 2008-07-14 2008-07-14 flying automobile

Country Status (1)

Country Link
CN (1) CN101628532A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102745069A (en) * 2012-08-08 2012-10-24 南昌航空大学 Power wind wheel type flying car
CN103223912A (en) * 2013-04-09 2013-07-31 浙江吉利汽车研究院有限公司杭州分公司 Vehicle drop protecting system and protecting method
CN104401280A (en) * 2014-10-25 2015-03-11 贺州学院 Liquid propellant rocket protection system for vehicle
CN105383243A (en) * 2015-11-26 2016-03-09 中国航空工业集团公司沈阳飞机设计研究所 Multifunctional driving system for flying car
CN105750129A (en) * 2016-04-29 2016-07-13 泉州市宏恩新能源汽车科技有限公司 Aerodynamic spray nozzle
CN105984516A (en) * 2015-02-05 2016-10-05 邱洪武 Microgravity vertical lifting initiative anti-collision system and anti-collision method thereof
CN106114097A (en) * 2016-06-29 2016-11-16 松会虎 One can vertical take-off and landing flying car
CN106970642A (en) * 2017-04-20 2017-07-21 佛山科学技术学院 A kind of multi-rotor unmanned aerial vehicle state monitoring apparatus
CN109649512A (en) * 2018-12-13 2019-04-19 华南理工大学 Vehicle-mounted active air power device and its application method
JP2021054363A (en) * 2019-10-02 2021-04-08 株式会社Subaru Slide door opening/closing structure and vehicle for both air and land
CN114407598A (en) * 2022-01-28 2022-04-29 广东汇天航空航天科技有限公司 Land-air coupling steering system and aerocar

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102745069A (en) * 2012-08-08 2012-10-24 南昌航空大学 Power wind wheel type flying car
CN103223912A (en) * 2013-04-09 2013-07-31 浙江吉利汽车研究院有限公司杭州分公司 Vehicle drop protecting system and protecting method
CN103223912B (en) * 2013-04-09 2016-01-27 浙江吉利汽车研究院有限公司杭州分公司 Vehicle fall protection system and guard method
CN104401280A (en) * 2014-10-25 2015-03-11 贺州学院 Liquid propellant rocket protection system for vehicle
CN105984516A (en) * 2015-02-05 2016-10-05 邱洪武 Microgravity vertical lifting initiative anti-collision system and anti-collision method thereof
CN105984516B (en) * 2015-02-05 2018-09-14 邱洪武 Microgravity VTOL active collision-avoidance system and its avoiding collision
CN105383243A (en) * 2015-11-26 2016-03-09 中国航空工业集团公司沈阳飞机设计研究所 Multifunctional driving system for flying car
CN105750129A (en) * 2016-04-29 2016-07-13 泉州市宏恩新能源汽车科技有限公司 Aerodynamic spray nozzle
CN106114097A (en) * 2016-06-29 2016-11-16 松会虎 One can vertical take-off and landing flying car
CN106970642A (en) * 2017-04-20 2017-07-21 佛山科学技术学院 A kind of multi-rotor unmanned aerial vehicle state monitoring apparatus
CN109649512A (en) * 2018-12-13 2019-04-19 华南理工大学 Vehicle-mounted active air power device and its application method
JP2021054363A (en) * 2019-10-02 2021-04-08 株式会社Subaru Slide door opening/closing structure and vehicle for both air and land
JP7411370B2 (en) 2019-10-02 2024-01-11 株式会社Subaru Sliding door opening/closing structure and amphibious vehicle
CN114407598A (en) * 2022-01-28 2022-04-29 广东汇天航空航天科技有限公司 Land-air coupling steering system and aerocar

Similar Documents

Publication Publication Date Title
CN101628532A (en) flying automobile
US11548637B2 (en) Electric vertical takeoff and landing aircraft
US20150102155A1 (en) Road-and-air transport vehicle
RU2547962C2 (en) Superhigh-speed aircraft and corresponding method of air movement
CN102015452B (en) Ground-bound device for take off, landing and taxiing of aircrafts
CN102180075A (en) Flying automobile
US11279473B2 (en) STOL aircraft
CN202345677U (en) Fast carrying structure used for transportation
CN101481015A (en) Small-sized foldable multi-wheel multi-column support type landing gear
DE102016011656A1 (en) Means of transport with a modular transport capsule for exchangeable connection with various drive units
CN1173157A (en) Space launch vehicles configured as gliders and towed to launch altitude by conventional aircraft
CN105711361A (en) New energy source triphibian flying car
EP2834152B1 (en) An aerospace plane system
CN201245243Y (en) Manned flying saucer
CN101450714A (en) Jet type helicopters
KR20090116573A (en) Vertical takeoff and landing flying vehicle
CN104875878A (en) Aircraft with a nacelle-housed main landing gear
DE102016120671A1 (en) Aircraft in Tailsitter configuration and its use
RU196251U1 (en) Unmanned Helicopter "SHADOW"
WO2005032939A1 (en) Toroidal flying object
RU2543471C2 (en) Multifunctional gyroplane
CN101879943A (en) Small-size retractable multi-wheel and multi-support undercarriage
DE112020003675T5 (en) Device for expedited transportation of passengers over intercontinental distances
CN1439573A (en) Jet airplanes
EA011979B1 (en) Flying vehicle

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C12 Rejection of a patent application after its publication
RJ01 Rejection of invention patent application after publication

Open date: 20100120