CN2413938Y

CN2413938Y - Flying car

Info

Publication number: CN2413938Y
Application number: CN 00222316
Authority: CN
Inventors: 熊伟; 李为忠; 蔡晓军; 申虎; 李年年; 郭菲; 黎泽金
Original assignee: Individual
Current assignee: Individual
Priority date: 2000-02-18
Filing date: 2000-02-18
Publication date: 2001-01-10
Anticipated expiration: 2010-02-18

Abstract

The utility model relates to a flying car. An output end of an engine 1 of the flying car is connected with a hydraulic pump 10 and a propeller 16 through a gear 9 and a power converting device 13 A. The hydraulic pump 10 is connected with a hydraulic motor 19 which is connected with a main staring wheel 7 through a transmission device 20. a tail wing 5 is provided with a collecting and folding device 23. In a steering device 2, a steering wheel 25 is connected with a shaft 26 which is connected with or disengaged from a gear 27 through a connecting mechanism 32 for achieving the connection or disengagement of the shaft 26 and a shaft 28. The shaft 26 is connected with or disengaged from a shaft 34 through a connecting mechanism 33. an operating mechanism for a rudder is connected with a wire rope 42 and a rudder 43 through rocker arms 41.

Description

Hovercar

The utility model is relevant with transportation means, but especially relevant with the hovercar of double as automobile and aircraft utilization.

Existing automobile can only use as land conveying tools, function singleness.

The purpose of this utility model provides a kind of land conveying tools that both can be used as, and can be used as the hovercar of flight tool again.

The utility model is achieved in that

The utility model is by driving engine 1, pilot instrument 2, and fuselage 3, main wing 4, empennage 5, vertical fin 6 and wheel are formed.The output of driving engine 1 is connected with propeller 16 with Hydraulic Pump 10 with moving transfer device 13A by gear 9.Hydraulic Pump 10 is connected with HM Hydraulic Motor 19, and the output of HM Hydraulic Motor 19 is taken turns 7 and is connected with having led by driving device (20).Empennage 5 has Folding device 23.In pilot instrument 2, mode control box 35 is connected with power switching device 13A, bindiny mechanism 32 and bindiny mechanism 33 respectively by cable 57.Gear 27 is connected or breaks away from axle 26 by bindiny mechanism 32, makes spools 26 to be connected with ground run steering shaft 28 by gear 27, gear 29.Make axle 26 and flight drive axle 34 by bindiny mechanism 33 and be connected or break away from, spools 34 with aileron control mechanism 36 with rise operating rock arm 60 and be connected.Having rudder control mechanism to pass through Rocker arm 41 is connected with yaw rudder 43 with cable wire 42.

The axle 8 of utility model driving engine 1 is connected with gear 9, gear 12 engagements on the axle 11 of gear 9 and Hydraulic Pump 10, the output shaft of electric hydaulic pressurized strut 13 is connected with gear 14, and gear 14 can mesh with gear 9 and gear 15 simultaneously, and gear 15 is fixed on the axle 17 of propeller 16.Led wheel 7 for left and right two, be installed on the main unit of landing gear 49, had two HM Hydraulic Motor 19 to take turns 7 and be connected with lead by wheel chain driving device 20 on the main wing 4, HM Hydraulic Motor 19 is passed through hydraulic pipe 21, hydraulic reservoir 22 is connected with Hydraulic Pump 10.The empennage that is contained in main wing 4 rotates pressurized strut 23 and is connected with empennage 5, and empennage 5 is hinged with main wing 4.Aileron 24 is arranged on the main wing 4, elevating rudder 62 arranged on the empennage 5.Pilot instrument 2 has bearing circle 25, its axle 26 is connected or breaks away from gear 27 by bindiny mechanism 32, gear 27 is connected with pitman arm 30 with ground run steering shaft 28; rocking arm 30 is connected with cable wire 31; have bindiny mechanism 32 to make axle 26 be connected or break away from gear 27, has bindiny mechanism 33 to make spools 26 to be connected or to break away from spools 34.

Mechanism

32,33 is connected with mode control box 35 by cable 57.Axle 34 is connected with aileron control mechanism 36, and steering unit 36 is connected with rocking arm 37, and rocking arm 37 is connected with pull bar 38, and spools 34 are connected with elevating rudder rocking arm 60, and rocking arm 60 is connected with cable wire 59, and cable wire 59 is connected with elevating rudder.Have yaw rudder to step on 40, be connected with cable wire 42 with Rocker arm 41, cable wire 42 is connected with yaw rudder 43.

The utility model is simple in structure, easy to manufacture, and is easy to use, both can be used as transportation means, can be used as flight tool again, can overcome traffic and hinder mobility strong.

Following is accompanying drawing of the present utility model:

Fig. 1 is an overall construction drawing of the present utility model

Fig. 2 is the birds-eye view of Fig. 1

Profile birds-eye view when Fig. 3 flies for the utility model

Fig. 4 is the utility model ground run profile and power system figure

Fig. 5 is the utility model state of flight power conversion constructional drawing

Fig. 6 is the utility model ground run state power conversion constructional drawing

Fig. 7 drives constructional drawing for the utility model

Following is embodiment of the present utility model:

Propeller fairing 44 is equipped with in head of the present utility model position, and double leaf propeller 16 is connected with axle 17, on the axle gear 15 is arranged, and can mesh with gear 14, and the axle of gear 14 is connected with the axle of electric hydaulic pressurized strut 13.Gear 14 can with gear 9 engagements of axle on 8 of piston engine 1.Gear 12 engagements on the axle 11 of gear 9 and Hydraulic Pump 10.

Head is equipped with a front-wheel 45.Front-wheel 45 has fairing 46, and damping cylinder 47, front-wheel are loaded on the nose-gear pillar 48.

Two masters are housed on the main wing 4 two ends main unit of landing gears 49 play wheel 7.The driving device 20 that wheel 7 is formed by gear and chain is connected with HM Hydraulic Motor 19, and damping cylinder 50 is arranged.

In the

seat rudder seat

51,52 is arranged, a rudder lid 53 and a front windshield 54 are arranged.

Main wing 4, empennage 5 is conventional structure, promptly is made of rib, girder and covering etc.Fuselage 3 adopts conventional structure, promptly adopts aluminum alloy system semihard shell-type fail safe structure, is made up of bulkhead, half frame, whole frame, long purlin, covering etc.

On the main wing 4 aileron is arranged, be connected with empennage by turning joint 56.The rotation pressurized strut 23 that is contained on the main wing 4 links to each other with empennage.Aileron 24 can be made wing flap again and use.Aileron by pull bar 38, rocking arm be 37, axle 34 handles, when making wing flap by cable control.Elevating rudder 62 arranged on the empennage 5, and it is by

cable wire

59,61, and manipulations such as rocking arm 60, axle 34 have yaw rudder 43 on the vertical fin 6, and it is handled by cable wire 42, Rocker arm 41 and foot-operated 40.

The bearing circle 25 of pilot instrument 2 of the present utility model has axle 26.Gear 29 and gear 27 engagements are arranged on the ground run steering shaft 28.Ground run handling maneuver cable wire 31 is connected with ground run steering hardware 39 by rocking arm 30.Aileron control pull bar 38 is connected with steering unit 36 by rocking arm 37.Elevator control cable wire 59 is connected with axle 34 by rocking arm 60.

Axle 26 can break away from or connection gear 27 by bindiny mechanism 32.Axle 26 can separate or adapter shaft 34 by shaft connection mechanism 33.Bindiny

mechanism

32,33 is connected with control capsule 35 by control cable 57, and master cock 58 is arranged on the box 35.

Following is the explanation of the utility model ground run state exchange:

In Fig. 6, switch in the mode control box 35 58 is connected, by cable 57, the electrical motor in the electric hydaulic pressurized strut 13 is rotated, drive the motion of hydraulic actuator axle, 14 whiles of gear and gear were opened in 9,15 minutes, the power of driving engine 1 then can be sent to propeller like this, and at this moment, the power of driving engine 1 is passed to Hydraulic Pump 10 by gear 9 and gear 12, and Hydraulic Pump 10 becomes the propulsion source of ground run, thereby realizes power conversion.

From Fig. 4, provide hydraulic pressure by hydraulic reservoir 22 and hydraulic tubing 21 to left and right two HM Hydraulic Motor 19 by Hydraulic Pump 10, HM Hydraulic Motor is rotated.

From Fig. 1, HM Hydraulic Motor 19 is formed driving device 20 by chain and gear, drives drive wheel 7 and rotates, and realizes the ground run of hovercar.

The maneuvering system conversion

From Fig. 7, switch 58 is connected, by cable 57, make mechanism's 32 lock shaft 26 and gear 27; By cable 57, make mechanism 33 separately axle 26 and axle 34, make axle 26 be connected with axle 28 like this by gear 27,29, realize the conversion of ground run maneuvering system.

From Fig. 7, when chaufeur direction of passage dish 25, axle 26, gear 27,29 during steering shaft 28 left-right rotation, shakes 30 by steering hardware 39 with turning to, and cable wire 31 is moved.Cable wire 31 is to be connected with the valve of the control oil mass of HM Hydraulic Motor 19 among Fig. 7, the motion of cable wire 31 among Fig. 7, and oil mass that will control motor 19 changes, thereby causes left and right HM Hydraulic Motor change in rotational speed, reaches the direction control of hovercar ground run.

The conversion of profile

In control capsule 35, connect switch 58, the electrical motor that uses empennage to rotate in the pressurized strut 23 by cable rotates, and makes the hydraulic actuator motion, and empennage 5 is rotated up to vertical with horizontal surface around hinge 56, and locking, thereby the conversion of realization hovercar ground run state.Conversion back profile is seen Fig. 4.

Following is the utility model state of flight conversion specification:

From Fig. 5, switch 58 in the mode control box 35 is oppositely connected, by control cable 57, make the motor backward rotation in the electric hydaulic pressurized strut 13, drive the counter motion of the moving tube of hydraulic pressure, make gear 14 while and gears 9,15 engagements, the power of piston engine 1 is passed to propeller 16 by gear 9,14,15 like this, makes propeller 16 high speed rotating, drive air, for hovercar provides power.

At this moment, engine power drives Hydraulic Pump 10 by gear 9,12, and Hydraulic Pump 10 provides hydraulic pressure only to supply the flight system equipment needed thereby, and does not supply with the HM Hydraulic Motor 19 that ground run uses, and this can realize by several valves.

The maneuvering system conversion

From Fig. 7, switch 58 is oppositely connected, and by cable 57, makes mechanism 32 separately axle 26 and gear 27, by cable 57, makes mechanism's 33 adapter shafts 26 and axle 34.Realize the conversion of flight control system like this.

Forward and backward when mobile when chaufeur by

axle

26,34, by rocking arm 60, make cable wire 59 motions, cable wire 59 links to each other with elevating rudder, and pitch attitude is controlled when realizing flight; When chaufeur turned left and right bearing circle, by

axle

26,34, aileron control mechanism 36 and rocking arm moved pull bar 38, and pull bar 38 links to each other with aileron 24 on the main wing 4, the roll control when realizing flight; Left and right when mobile when chaufeur by foot-operated 40, make cable wire 42 motions by Rocker arm 41, cable wire 42 links to each other with yaw rudder 43, and the direction when realizing flight is controlled.

The conversion of profile

Make empennage rotate pressurized strut 23 counter motions, make empennage pass through hinge 56 and rotate an angle and locking, thereby realize the profile conversion of hovercar state, the state of flight profile is seen Fig. 3.

Claims

1, a kind of hovercar, it is characterized in that by driving engine (1), pilot instrument (2), fuselage (3), main wing (4), empennage (5), vertical fin (6) and wheel are formed, the output of driving engine (1) is connected with propeller (16) with Hydraulic Pump (10) with power switching device (13A) by gear (9), Hydraulic Pump (10) is connected with HM Hydraulic Motor (19), the output of HM Hydraulic Motor (19) by driving device (20) with led wheel (7) and be connected, empennage (5) has Folding device (23), in pilot instrument (2), mode control box (35) by cable 57 respectively with power switching device (13 A), bindiny mechanism (32) is connected with bindiny mechanism (33), gear (27) is connected or breaks away from axle 26 by bindiny mechanism (32), by gear (27), gear (29) makes axle 26 be connected with ground run steering shaft 28, making axle 26 and flight drive axle (34) by bindiny mechanism (33) is connected or breaks away from, axle (34) and aileron control mechanism (36) with rise operating rock arm (60) and be connected, have rudder control mechanism to pass through rocking arm (41) and be connected with yaw rudder (43) with cable wire (42).

2; Hovercar according to claim 1; The axle (8) that it is characterized in that engine (1) is connected with gear (9); Gear (12) engagement on the axle (11) of gear (9) and hydraulic pump (10); The output shaft of electric hydaulic pressurized strut (13) is connected with gear (14); Gear (14) can mesh with gear (9) and gear (15) simultaneously; Gear (15) is fixed on the axle (17) of propeller (16); Led wheel (7) for left; Right two; Be installed on the main unit of landing gear (49); Have on the main wing (4) two hydraulic motors (19) by chain transmission device (20) with led wheel (7) and be connected; Hydraulic motor (19) is by hydraulic tube (21); Hydraulic oil container (22) is connected with hydraulic pump (10); The empennage that is contained in main wing (4) rotates pressurized strut (23) and is connected with empennage (5); Empennage (5) is hinged with main wing (4); Aileron (24) is arranged on the main wing (4); Elevator (62) is arranged on the empennage (5); Pilot instrument (2) has steering wheel (25); Its axle (26) is connected or breaks away from gear (27) by bindiny mechanism (32); Gear (27) is connected with pitman arm (30) with ground run steering spindle (28); Rocking arm (30) is connected with cable wire (31); Have bindiny mechanism (32) to make axle (26) be connected 27 with gear) connect or break away from; Have bindiny mechanism (33) to make axle (26) be connected 34 with axle) connect or break away from; Mechanism (32); (33) be connected with state control box (35) by cable (57); Axle (34) is connected with aileron control mechanism (36); Operating mechanism (36) is connected with rocking arm (37); Rocking arm (37) is connected with pull bar (38); Axle (34) is connected with elevator rocking arm (60); Rocking arm (60) is connected with cable wire (59); Cable wire (59) is connected with elevator; Have rudder foot-operated (40) to be connected 42 with rocking arm (41) with cable wire) be connected, cable wire (42) is connected with rudder (43).