CN206217526U - A kind of wheel is dwelt hovercar using the land, water and air three that rhombus is laid out - Google Patents

A kind of wheel is dwelt hovercar using the land, water and air three that rhombus is laid out Download PDF

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Publication number
CN206217526U
CN206217526U CN201620929412.8U CN201620929412U CN206217526U CN 206217526 U CN206217526 U CN 206217526U CN 201620929412 U CN201620929412 U CN 201620929412U CN 206217526 U CN206217526 U CN 206217526U
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wheel
hovercar
jack
land
vehicle body
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CN201620929412.8U
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Chinese (zh)
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王勇
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Sichuan Yidian Aviation Technology Co., Ltd
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Shanghai Plume Aviation Technology Co Ltd
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Abstract

A kind of wheel disclosed in the utility model is dwelt hovercar using the land, water and air three that rhombus is laid out, including:One type vehicle body, the type vehicle body has an aircraft control system, it is characterised in that also include:The front-wheel of one lower front that the type vehicle body is arranged on by front-wheel jack;The trailing wheel of one bottom rear that the type vehicle body is arranged on by trailing wheel jack;And one by left and right side wheel jack be arranged on the type vehicle body bottom in the middle of both sides left and right side wheel;Assume diamond in shape distribution between the front-wheel, trailing wheel and left and right side wheel, and the front-wheel jack, trailing wheel jack and left and right side wheel jack are connected with the aircraft control system respectively.Dwell four wheels of hovercar of land, water and air of the present utility model three are laid out using rhombus, and each wheel can individually folding and unfolding so that four wheels of hovercar can be switched in different operational modes, meet the service requirement of various states.

Description

A kind of wheel is dwelt hovercar using the land, water and air three that rhombus is laid out
Technical field
The utility model is related to land, water and air three to dwell hovercar technical field, more particularly to a kind of wheel is laid out using rhombus Land, water and air three dwell hovercar.
Background technology
The hovercar of dwelling of land, water and air three can run at high speed on land, also can takeoff and landing on the road of land, while Can also be in takeoff and landing on the water.Referring to Fig. 1, what is be given in figure is that existing land, water and air three are dwelt hovercar, including type Vehicle body 10 and be arranged on type vehicle body 10 lower front two front-wheels 20 and be arranged on the bottom rear of type vehicle body 10 Two trailing wheels 30.Existing land, water and air three are dwelt the wheel distribution form of hovercar and the wheel distribution form base of general-utility car This is similar, but this conventional wheel distribution form land, water and air three dwell hovercar there are problems that it is following some:
1st, speed of the hovercar in takeoff and landing, because the land, water and air three of this conventional wheel distribution form Dwelling hovercar can not be using big angles-of-attack in takeoff and landing, and this results in its security performance in takeoff and landing Reduce;
2nd, the land, water and air three of this conventional wheel distribution form landing speed of the hovercar on runway of dwelling is larger, thus The land, water and air three of this conventional wheel distribution form hovercar of dwelling needs runway more long in takeoff and landing.
Therefore, applicant carried out beneficial exploration and trial, have found result of the above problems, will be detailed below being situated between The technical scheme for continuing is produced under this background.
Utility model content
Technical problem to be solved in the utility model:There is provided in view of the shortcomings of the prior art a kind of security performance it is high, The shorter wheel of ground run distance is dwelt hovercar using the land, water and air three that rhombus is laid out during takeoff and landing.
Technical problem to be solved in the utility model can adopt the following technical scheme that to realize:
A kind of wheel is dwelt hovercar using the land, water and air three that rhombus is laid out, including:One type vehicle body, the type vehicle body With an aircraft control system, it is characterised in that also include:
The front-wheel of one lower front that the type vehicle body is arranged on by front-wheel jack;
The trailing wheel of one bottom rear that the type vehicle body is arranged on by trailing wheel jack;And
The one left and right side wheel that both sides in the middle of the bottom of the type vehicle body are arranged on by left and right side wheel jack;
Assume diamond in shape distribution between the front-wheel, trailing wheel and left and right side wheel, the front-wheel jack, trailing wheel radio and tape player Structure and left and right side wheel jack are connected with the aircraft control system respectively;
When hovercar is in land landing state, on the one hand the aircraft control system controls the front-wheel, left and right Side wheel puts down completely, on the other hand controls the trailing wheel to pack up completely;When hovercar is in water surface landing state or water surface cunning During row state, the aircraft control system controls the front-wheel, trailing wheel and left and right side wheel to pack up completely;When hovercar is in During land locomotion state, on the one hand the aircraft control system controls the front-wheel, trailing wheel to put down completely, on the other hand control institute Left and right side wheel is stated slightly to pack up and only play a part of Auxiliary support.
As a result of technical scheme as above, the beneficial effects of the utility model are:Land, water and air of the present utility model Three four wheels for dwelling hovercar are laid out using rhombus, and each wheel can individually folding and unfolding.Land is taken off when landing, and is put Lower front-wheel and left and right side wheel, pack up trailing wheel, and such front-wheel, left and right side wheel constitute the tricycle landing gear of standard so that fly Row automobile can use big angles-of-attack in land takeoff and landing, significantly reduce the landing speed of hovercar, contract Short ground run distance;When water surface landing or hydroplaning, front and rear wheel and left and right side wheel are packed up, and now hovercar turns into standard Seaplane, can high speed slide or landing on the water surface;When land is run at high speed, front and rear wheel is put down, and left and right side wheel is omited Micro- to pack up so that the wheel face of left and right side wheel is formed with ground and contacted, wherein front-wheel or trailing wheel control is turned to or driven, left and right side Wheel only plays a part of Auxiliary support.
Brief description of the drawings
In order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art, below will be to embodiment Or the accompanying drawing to be used needed for description of the prior art is briefly described, it should be apparent that, drawings in the following description are only It is some embodiments of the present utility model, for those of ordinary skill in the art, is not paying the premise of creative work Under, other accompanying drawings can also be obtained according to these accompanying drawings.
Fig. 1 is that existing land, water and air three are dwelt the structural representation of hovercar.
Fig. 2 is that land, water and air of the present utility model three are dwelt the structural representation of hovercar.
Specific embodiment
In order that technological means, creation characteristic, reached purpose and effect that the utility model is realized are easy to understand, under Face combines and is specifically illustrating, and the utility model is expanded on further.
Referring to Fig. 2, be given in figure to be a kind of wheel dwelt hovercar, including type using the land, water and air three that rhombus is laid out Vehicle body 100 and front-wheel 210, trailing wheel 220 and left and right side wheel 230,240.
There is an aircraft control system, aircraft control system can be to the configuration of hovercar, flight in type vehicle body 100 Attitude and kinematic parameter implement control.Front-wheel 210 is arranged on type vehicle body 100 by front-wheel jack (not shown) Lower front.Trailing wheel 220 is arranged on the bottom rear of type vehicle body 100 by trailing wheel jack (not shown).It is left and right Side wheel 230,240 is arranged on two in the middle of the bottom of type vehicle body 100 by left and right side wheel jack (not shown) respectively Side.
Assume diamond in shape distribution, i.e. front-wheel 210 and trailing wheel 220 between front-wheel 210, trailing wheel 220 and left and right side wheel 230,240 On the axis of hovercar, left and right side wheel 230,240 is located at the both sides of the axis of hovercar and both connections Line perpendicular to the axis of hovercar, the center of gravity A of hovercar be located at connecting line between front-wheel 210, trailing wheel 220 and a left side, The front of the intersection point of the connecting line between right-hand wheel 230,240.
Front-wheel jack, trailing wheel jack and left and right side wheel jack are connected with aircraft control system respectively, Front-wheel jack, trailing wheel jack and left and right side wheel jack be used for respectively to front-wheel 210, trailing wheel 220 and Left and right side wheel 230,240 puts down or packs up, and it is identical with existing undercarriage draw off gear, no longer goes to live in the household of one's in-laws on getting married one by one herein State.
When hovercar is in land landing state, aircraft control system is on the one hand by front-wheel jack, left and right Side wheel jack control front-wheel 210, the wheel of left and right side 230,240 put down completely, are on the other hand controlled by trailing wheel jack Trailing wheel 220 is packed up completely, and such front-wheel 210 and left and right side 230,240 constitute the tricycle landing gear of standard so that flight Automobile can use big angles-of-attack in land takeoff and landing, significantly reduce the landing speed of hovercar, shorten Ground run distance.
When hovercar is in water surface landing state or hydroplaning state, aircraft control system passes through front-wheel radio and tape player Structure, trailing wheel jack and left and right side wheel jack control front-wheel 210, trailing wheel 220 and left and right side wheel 230,240 are received completely Rise, now hovercar turns into the seaplane of standard, can high speed slide or landing on the water surface.
When hovercar be in land high-speed travel state when, aircraft control system on the one hand by front-wheel jack, Trailing wheel jack control front-wheel 210, trailing wheel 220 put down completely, on the other hand by left and right side wheel jack control it is left, Right-hand wheel 230,240 is slightly packed up so that the wheel face of left and right side wheel 230,240 and ground form and contacts, wherein front-wheel 210 or The control of trailing wheel 220 is turned to or driven, and left and right side wheel 230,240 only plays a part of Auxiliary support, left and right side wheel 230,240 Carry the weight of hovercar 5%~10%.
General principle of the present utility model and principal character and advantage of the present utility model has been shown and described above.One's own profession The technical staff of industry it should be appreciated that the utility model is not restricted to the described embodiments, described in above-described embodiment and specification Simply illustrate principle of the present utility model, on the premise of the utility model spirit and scope are not departed from, the utility model is also Various changes and modifications are had, these changes and improvements are both fallen within the range of claimed the utility model.The utility model Claimed scope is by appending claims and its equivalent thereof.

Claims (1)

1. a kind of wheel is dwelt hovercar using the land, water and air three that rhombus is laid out, including:One type vehicle body, the type vehicle body tool There is an aircraft control system, it is characterised in that also include:
The front-wheel of one lower front that the type vehicle body is arranged on by front-wheel jack;
The trailing wheel of one bottom rear that the type vehicle body is arranged on by trailing wheel jack;And
The one left and right side wheel that both sides in the middle of the bottom of the type vehicle body are arranged on by left and right side wheel jack;
Assume diamond in shape distribution between the front-wheel, trailing wheel and left and right side wheel, the front-wheel jack, trailing wheel jack with And left and right side wheel jack is connected with the aircraft control system respectively.
CN201620929412.8U 2016-08-23 2016-08-23 A kind of wheel is dwelt hovercar using the land, water and air three that rhombus is laid out Active CN206217526U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620929412.8U CN206217526U (en) 2016-08-23 2016-08-23 A kind of wheel is dwelt hovercar using the land, water and air three that rhombus is laid out

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620929412.8U CN206217526U (en) 2016-08-23 2016-08-23 A kind of wheel is dwelt hovercar using the land, water and air three that rhombus is laid out

Publications (1)

Publication Number Publication Date
CN206217526U true CN206217526U (en) 2017-06-06

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CN (1) CN206217526U (en)

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Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20180911

Address after: 214000 No. 75, Shuo Fang Yu An Road, new Wu District, Wuxi, Jiangsu

Patentee after: Mu Yu Aviation Technology (Jiangsu) Co., Ltd.

Address before: 201400 room 3, 6 building, 4299 Jin Du Road, Minhang District, Shanghai, D56

Patentee before: Shanghai plume Aviation Technology Co., Ltd.

TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20191204

Address after: Room 812, enterprise service center, No. 17, section 3, west section of Changjiang North Road, Lingang Economic Development Zone, Yibin City, Sichuan Province

Patentee after: Sichuan Yidian Aviation Technology Co., Ltd

Address before: 214000 No. 75, Shuo Fang Yu An Road, new Wu District, Wuxi, Jiangsu

Patentee before: Mu Yu Aviation Technology (Jiangsu) Co., Ltd.