CN105905290A - Movable flight vehicle - Google Patents
Movable flight vehicle Download PDFInfo
- Publication number
- CN105905290A CN105905290A CN201610369106.8A CN201610369106A CN105905290A CN 105905290 A CN105905290 A CN 105905290A CN 201610369106 A CN201610369106 A CN 201610369106A CN 105905290 A CN105905290 A CN 105905290A
- Authority
- CN
- China
- Prior art keywords
- aircraft
- wheel
- mobile
- steering wheel
- arranges
- 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
Links
- 241000380131 Ammophila arenaria Species 0.000 claims description 18
- 241000276425 Xiphophorus maculatus Species 0.000 claims description 3
- 238000004891 communication Methods 0.000 claims description 2
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60B—VEHICLE WHEELS; CASTORS; AXLES FOR WHEELS OR CASTORS; INCREASING WHEEL ADHESION
- B60B33/00—Castors in general; Anti-clogging castors
- B60B33/0002—Castors in general; Anti-clogging castors assembling to the object, e.g. furniture
-
- 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
- B64D47/00—Equipment not otherwise provided for
-
- 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
- B64D2205/00—Aircraft with means for ground manoeuvring, such as taxiing, using an auxiliary thrust system, e.g. jet-engines, propellers or compressed air
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
Abstract
The invention discloses a movable flight vehicle. The movable flight vehicle comprises a flight vehicle body and a movable device. The flight vehicle body is a multi-rotary-wing unmanned plane. The movable device comprises universal wheel device bodies and steering engine device bodies. According to the movable flight vehicle provided by the invention, based on a control platform of the unmanned plane and through remote control, steering engines drive wheels to move the unmanned plane on the ground to a designated position, then the unmanned plane takes off, and cargo replenishment, disaster response, medical aid and other steering ranges needing the unmanned plane to move on the ground are completed.
Description
Technical field
The present invention relates to a kind of mobile aircraft, belong to aircraft unmanned plane field.
Background technology
In the last few years, unmanned plane with the features such as its low-loss, high maneuverability, safety military, civilian and
Scientific research aspect has important effect, unmanned plane the disaster relief, take photo by plane, agricultural, each neck such as investigation
Territory has obtained studying widely and applying.Many rotor wing unmanned aerial vehicles are that a kind of have can the nothing of VTOL ability
People's aircraft, has the advantages such as excellent, mobile flexibly, the compact conformation of hovering ability.
Summary of the invention
Present invention aims to the drawbacks described above of prior art, propose the mobile aircraft of one, open up
The operable scope of exhibition unmanned plane, report control platform based on unmanned plane, by remote control, make steering wheel drive
Unmanned plane is moved to specify position to take off by motor car wheel on the ground the most again, completes goods supply, disaster sound
Should, medical aid, etc. need unmanned plane in the steering range of ground moving.
For achieving the above object, the present invention provides following technical scheme:
A kind of mobile aircraft, including: aircraft and mobile device.
Wherein, aircraft is many rotary wind types unmanned plane, including criss-cross body, on four tops of body
Point is each arranges a rotor, and the downward vertical at each rotor arranges a mobile device.
And wherein, mobile device includes universal wheel unit and helm gear.
The lower end of two rotors arranges and each arranges a universal wheel unit, at two other rotor wherein
Lower end respectively arranges a helm gear.
Two universal wheel units are arranged on side, and two helm gears are arranged on opposite side.
Helm gear includes steering wheel, main body, connector, wheel, securing member and wheel shaft.
Main body is vertical platy structure, is connecting plate at its top, flies for being arranged on by helm gear
On the body of row device.
Install steering wheel in the bottom of main body, wherein steering wheel is arranged on body by securing member.
Crossing out wheel shaft, the rotation of servo driving wheel shaft from steering wheel, wheel shaft end arranges wheel, car
Wheel is followed wheel shaft and is turned.
Body central authorities at aircraft also include attachment structure, can be used for being connected with operation device, make
Industry.
Accompanying drawing explanation
Fig. 1 is the structural representation of the mobile aircraft of the present invention.
Fig. 2 is the structural representation of the helm gear of the mobile aircraft of the present invention.
(note: the shown structure in accompanying drawing, simply to illustrate that the signal of feature of present invention, is not intended to
According to structure shown in accompanying drawing.)
Detailed description of the invention
As it is shown in figure 1, according to mobile aircraft of the present invention, including: aircraft and mobile device.
Wherein, aircraft is many rotary wind types unmanned plane, including criss-cross body 2, on four tops of body
Point is each arranges a rotor 3, and the downward vertical at rotor 3 arranges a mobile device.
Body 2 central authorities at aircraft also include attachment structure 1, can be used for being connected with devices such as mechanical hands,
Carry out operation.
And wherein, mobile device includes universal wheel unit 4 and helm gear 5.As it is shown in figure 1,
The lower end of two of which rotor 3 arranges and each arranges a universal wheel unit 4, at two other rotor 3
Lower end respectively arranges a helm gear 5.
Preferably, two universal wheel units 4 are arranged on side, and two helm gears 5 are arranged on opposite side.
Thus one, when the aircraft on the ground, driving and universal wheel by helm gear 5 fill
Put 4 servo-actuated, aircraft can be moved to required suitable place.
Under some special environments, aircraft can pass through mobile device, and autonomous postpones to specific bit
Carry out flight of taking off again, after completing task, move meeting operator at one's side again after can landing, do so
Aircraft can be made to enter working environment when silent, also can leave work under silent state
Make environment.
Meanwhile, mobile aircraft when, electricity can be saved to battery by mobile device so that unmanned
It is more long that machine aloft flies.
Further, according to mobile aircraft of the present invention, also include that steering wheel electric control gear (is not schemed
Show) and the aircraft that is separately provided fly to control device (not shown).
Wherein, steering wheel electric control gear control flaps machine 5, aircraft flies to control device and controls the flight of aircraft.
The automatically controlled part of steering wheel and aircraft fly to carry out radio communication between control device.
Operator can fly to control device (not shown) remotely-piloted vehicle, including to shifting by aircraft
The remote manipulation of the helm gear 5 in dynamic device.
As in figure 2 it is shown, helm gear 5 includes steering wheel 6, main body 7, connector 8, wheel 9, fastening
Part 10 and wheel shaft 11.
Wherein, main body 7 is vertical platy structure, is connecting plate 8 at its top, for by fastening
Helm gear 5 is arranged on the body 2 of aircraft by part.
Install steering wheel 6 in the bottom of main body 7, wherein steering wheel is arranged on body 2 by securing member 10.
Wheel shaft 11, the rotation of steering wheel 6 live axle 11, wheel shaft 11 end is crossed out from steering wheel 6
End arranges wheel 9, and wheel 9 is followed wheel shaft and rotated.Further, steering wheel 6 drives wheel 9 by differential control
System turns to.
By above description, according to mobile aircraft of the present invention, it is unmanned based on many rotors
The expansive approach of machine platform, by aircraft and the combination of walking function so that unmanned plane simultaneously can be complete
Become airflight task, as investigated, taking photo by plane, the function such as article transport, also can be after completing aerial mission
Be automatically moved to specific bit postpone take off completing on ground, it is also possible to silent enter to specify region after
Complete aerial mission again.
Have the advantage that according to mobile flying instrument of the present invention
1. the limitation before decreasing the taking off of unmanned plane, after landing；
2. unmanned plane can be allowed at silent flight range of entering；
3. improve the exercisable limitation of unmanned plane, give the more working place of unmanned plane；
4. decrease people and manually move the operation of unmanned plane；
The above, only presently preferred embodiments of the present invention, it is not intended to limit the protection of the present invention
Scope, all any amendment, equivalent and improvement etc. made within the spirit and principles in the present invention,
Should be included within the scope of the present invention.
Claims (9)
1. a mobile aircraft, it is characterised in that:
Including: aircraft and mobile device；
Wherein, aircraft is many rotary wind types unmanned plane, including criss-cross body (2), at the four of body
Individual summit respectively arranges a rotor (3), and the downward vertical at each rotor (3) arranges a mobile device；
And wherein, mobile device includes universal wheel unit (4) and helm gear (5).
Mobile aircraft the most according to claim 1, it is characterised in that:
The lower end of two rotors (3) arranges and each arranges a universal wheel unit (4), other two wherein
The lower end of individual rotor (3) respectively arranges a helm gear (5).
Mobile aircraft the most according to claim 2, it is characterised in that:
Two universal wheel units (4) are arranged on side, and two helm gears (5) are arranged on opposite side.
Mobile aircraft the most according to claim 3, it is characterised in that:
Helm gear (5) includes steering wheel (6), main body (7), connector (8), wheel (9), tight
Firmware (10) and wheel shaft (11).
Mobile aircraft the most according to claim 4, it is characterised in that:
Main body (7) is vertical platy structure, is connecting plate (8) at its top, for by helm gear
(5) it is arranged on the body (2) of aircraft；
Install steering wheel (6) in the bottom of main body (7), wherein steering wheel is arranged on by securing member (10)
On body (2)；
Crossing out wheel shaft (11) from steering wheel (6), steering wheel (6) live axle (11) rotates,
Wheel shaft (11) end arranges wheel (9), and wheel (9) is followed wheel shaft and rotated.
Mobile aircraft the most according to claim 5, it is characterised in that:
Mobile aircraft also includes that steering wheel electric control gear and the aircraft being separately provided fly to control device；
Wherein, steering wheel electric control gear control flaps machine (5), aircraft flies to control device and controls aircraft
Flight.
Mobile aircraft the most according to claim 6, it is characterised in that:
The automatically controlled part of steering wheel and aircraft fly to carry out radio communication between control device.
Mobile aircraft the most according to claim 1, it is characterised in that:
Body (2) central authorities at aircraft also include attachment structure (1), can be used for being connected with operation device,
Carry out operation.
Mobile aircraft the most according to claim 4, it is characterised in that:
Steering wheel (6) controls it by differential mode when driving wheel (9) and turns to.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610369106.8A CN105905290A (en) | 2016-05-30 | 2016-05-30 | Movable flight vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610369106.8A CN105905290A (en) | 2016-05-30 | 2016-05-30 | Movable flight vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105905290A true CN105905290A (en) | 2016-08-31 |
Family
ID=56741673
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610369106.8A Pending CN105905290A (en) | 2016-05-30 | 2016-05-30 | Movable flight vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105905290A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106394893A (en) * | 2016-12-12 | 2017-02-15 | 中国民用航空飞行学院 | Multifunctional solar multi-rotor |
| CN107985579A (en) * | 2017-12-11 | 2018-05-04 | 王美航 | A kind of cargo aircraft |
| CN115157947A (en) * | 2022-08-04 | 2022-10-11 | 哈尔滨工业大学 | Air-ground amphibious reconfigurable robot |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1944091A (en) * | 2006-11-07 | 2007-04-11 | 北京航空航天大学 | Multifunction aircraft |
| CN103128730A (en) * | 2013-02-27 | 2013-06-05 | 广东工业大学 | Multi-form real-time information transmission rescue robot |
| KR20130098062A (en) * | 2012-02-27 | 2013-09-04 | 한국과학기술원 | Flying and wall climbing robot |
| CN104816821A (en) * | 2015-04-20 | 2015-08-05 | 上海交通大学 | Multi-rotor wing triphibian aircraft |
| CN105416585A (en) * | 2015-11-25 | 2016-03-23 | 上海云犀智能系统有限公司 | Unmanned aerial vehicle capable of freely switching moving modes |
-
2016
- 2016-05-30 CN CN201610369106.8A patent/CN105905290A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1944091A (en) * | 2006-11-07 | 2007-04-11 | 北京航空航天大学 | Multifunction aircraft |
| KR20130098062A (en) * | 2012-02-27 | 2013-09-04 | 한국과학기술원 | Flying and wall climbing robot |
| CN103128730A (en) * | 2013-02-27 | 2013-06-05 | 广东工业大学 | Multi-form real-time information transmission rescue robot |
| CN104816821A (en) * | 2015-04-20 | 2015-08-05 | 上海交通大学 | Multi-rotor wing triphibian aircraft |
| CN105416585A (en) * | 2015-11-25 | 2016-03-23 | 上海云犀智能系统有限公司 | Unmanned aerial vehicle capable of freely switching moving modes |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106394893A (en) * | 2016-12-12 | 2017-02-15 | 中国民用航空飞行学院 | Multifunctional solar multi-rotor |
| CN107985579A (en) * | 2017-12-11 | 2018-05-04 | 王美航 | A kind of cargo aircraft |
| CN115157947A (en) * | 2022-08-04 | 2022-10-11 | 哈尔滨工业大学 | Air-ground amphibious reconfigurable robot |
| CN115157947B (en) * | 2022-08-04 | 2023-04-07 | 哈尔滨工业大学 | Air-ground amphibious allosteric robot |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C41 | Transfer of patent application or patent right or utility model | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20161213 Address after: 150000 Heilongjiang Province, Harbin City Economic Development Zone haping Road District Dalian road and Xingkai road junction Applicant after: Hagongda robot group (Harbin) Asset Management Co., Ltd. Address before: 150000 Heilongjiang Province, Harbin City Economic Development Zone haping Road District Dalian road and Xingkai road junction Applicant before: HIT ROBOT GROUP CO., LTD. |
|
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20160831 |
|
| RJ01 | Rejection of invention patent application after publication |