CN106672226A - Multi-rotor vehicle body structure capable of effectively reducing transport space - Google Patents
Multi-rotor vehicle body structure capable of effectively reducing transport space Download PDFInfo
- Publication number
- CN106672226A CN106672226A CN201710004216.9A CN201710004216A CN106672226A CN 106672226 A CN106672226 A CN 106672226A CN 201710004216 A CN201710004216 A CN 201710004216A CN 106672226 A CN106672226 A CN 106672226A
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- CN
- China
- Prior art keywords
- horn
- wing
- groove
- vehicle body
- transport space
- 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.)
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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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/46—Blades
- B64C27/473—Constructional features
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
The invention discloses a multi-rotor vehicle body structure capable of effectively reducing transport space. The multi-rotor vehicle body structure comprises a vehicle body and a plurality of arms, wherein bar-type grooves with the number identical with that of the arms are formed in the top of the vehicle body, central axes of the bar-type grooves and central axes of the arms are located in the same straight line, the arms are matched with the bar-type grooves, end plates are arranged on side walls of the vehicle body, tops of the end plates and bottoms of the bar-type grooves are level, and one end of each end plate is hinged to the corresponding arm; rotors are also arranged at tail ends of the arms, each rotor comprises two rotor sheets, grooves are also formed in tops of the arms, the width of the grooves is matched with that of the rotor sheets, and the depth of the grooves is larger than or equal to two times of the thickness of the rotor sheets. The multi-rotor vehicle body structure solves the problem that arms and rotors of the UAV are damaged easily during delivery.
Description
Technical field
The present invention relates to a kind of unmanned plane, and in particular to a kind of many rotor housing constructions for being effectively reduced transport space.
Background technology
Multi-rotor unmanned aerial vehicle realizes flight by the multiple propellers of multiple motor controls, is widely used in and takes photo by plane, monitors, searching
Rescue, the every field such as resource exploration, agricultural, with small volume, low lightweight, expense, flexible operation and it is safe the features such as.
Multi-rotor unmanned aerial vehicle possesses more horn, when unmanned plane is collected, needs to twist off screw, and horn is disassembled could more preferably
Transport, repeatedly dismantle and install both wasted time.
Both wasted time to solve the problems, such as to dismantle repeatedly and install, rolled on the wing of unmanned plane in prior art
It is folded, but in unmanned plane collection transportation, this kind of folding mode easily causes horn, wing abrasion, affects performance.
The content of the invention
It is an object of the invention to provide a kind of many rotor housing constructions for being effectively reduced transport space, solve transporting
During, the problem that the horn of unmanned plane, wing are easily damaged.
The present invention is achieved through the following technical solutions：
A kind of many rotor housing constructions for being effectively reduced transport space, including body, several horns, on the top of body
Portion is provided with the strip groove with the quantity such as horn, and the central axis of the strip groove is located at same with the central axis of horn
Straight line, the horn is matched with strip groove, and in the side wall of body end plate, the end plate top and strip groove bottom are additionally provided with
Portion's level, one end and the horn of end plate are hinged；Wing is additionally provided with the end of horn, the wing includes two fins,
Horn top is additionally provided with groove, and the width of the groove is matched with fin, and the depth of groove is more than or equal to foil thickness
Twice.
Further, the folding mode of unmanned plane of the prior art is varied, and oriented organism sidewall is folded, and also has picture
What body surrounding was folded, but the horn or wing without doubling poststack in prior art carries out further protection, causes
Horn, wing cause to damage in transportation.Novelty of the present invention devises a kind of foldable structure, by horn to body
Top fold, shape of the end plate of the strip groove matched with horn, horn and body end to be hinged is arranged at the top of body
Formula connects, and end plate is a linking arm integrated with body, and the horn after folding has just been placed in strip groove, so as to avoid
Horn abrasion.Groove is also provided with the top of horn, after two fins of wing are pulled down, in being put into groove, groove
Width is matched with fin, makes fin be not easy to drop, and is put into after then horn is folded again in strip groove so that wing, machine
Arm is obtained for protection, while also solving the problems, such as to be taken up room during transport.
Preferably, the bottom of the groove is provided with rotary wings seat, and at the top of the rotary wings seat wing is provided with, described
Wing includes two fins, and two fins are bolted.Further, this mode of the present invention is without fin is taken
Under, it is more convenient.The rotary wings seat for driving wing rotation is arranged on into the bottom of groove, wing is located at the top of rotary wings seat, two
Individual fin is bolted, and when needing to collect fin, the elasticity of adjustment bolt rotates fin, will rotate
Fin afterwards coincides together, and is then placed in groove, to protect fin.
Height adjustment mechanism is additionally provided between the rotary wings seat and wing.Further, height adjustment mechanism is used for
The height that wing rises is adjusted, makes wing more flexible, while being also to avoid groove from limiting the further improvement that wing rotation is done.
Preferably, the height adjustment mechanism is telescopic rod.The length of telescopic rod is preferably between 0.5cm to 2cm.
The present invention compared with prior art, has the following advantages and advantages：
1st, a kind of many rotor housing constructions for being effectively reduced transport space of the present invention, are provided with and machine at the top of body
The strip groove of the quantity such as arm, the central axis of the strip groove is located at same straight line, the machine with the central axis of horn
Arm is matched with strip groove, and above structure is solved during transport, the problem of the horn easy damaged of unmanned plane；
2nd, a kind of many rotor housing constructions for being effectively reduced transport space of the present invention, in the side wall of body end is additionally provided with
Plate, the end plate top and strip groove bottom level, one end and the horn of end plate are hinged；Also set up in the end of horn organic
The wing, the wing includes two fins, and groove is additionally provided with the top of horn, and the width of the groove is matched with fin, and recessed
The depth of groove is more than or equal to the twice of foil thickness, with upper type so that wing, horn are obtained for protection；
3rd, a kind of many rotor housing constructions for being effectively reduced transport space of the present invention, the bottom of the groove is provided with rotation
Rotor seat, is provided with wing at the top of the rotary wings seat, the wing includes two fins, and two fins are connected by bolt
Connect, wing is not only protected with upper type, and without fin is removed, it is more convenient.
Description of the drawings
Accompanying drawing described herein is used for providing further understanding the embodiment of the present invention, constitutes of the application
Point, do not constitute the restriction to the embodiment of the present invention.In the accompanying drawings：
Fig. 1 is schematic structural view of the invention.
Labelling and corresponding parts title in accompanying drawing：
1- bodies, 2- horns, 3- strip grooves, 4- end plates, 5- wings, 6- grooves, 7- fins, 8- bolts, 9- rotary wings
Seat.
Specific embodiment
To make the object, technical solutions and advantages of the present invention become more apparent, with reference to embodiment and accompanying drawing, to this
Invention is described in further detail, and the exemplary embodiment of the present invention and its explanation are only used for explaining the present invention, do not make
For limitation of the invention.
Embodiment 1
As shown in figure 1, a kind of many rotor housing constructions for being effectively reduced transport space of the present invention, including body 1,4
Horn 2, at the top of body 1 strip groove 3 with the quantity such as horn 2, the central axis and machine of the strip groove 3 are provided with
The central axis of arm 2 is located at same straight line, and the horn 2 is matched with strip groove 3, and in the side wall of body 1 end plate is additionally provided with
4, with the bottom level of strip groove 3 at the top of the end plate 4, one end and the horn 2 of end plate 4 are hinged；Also set up in the end of horn 2
There is wing 5, the wing 5 includes two fins 7, at the top of horn 2 groove 6, the width and fin of the groove 6 are additionally provided with
7 matchings, and the depth of groove 6 is 2.5 times of the thickness of fin 7.With upper type so that wing, horn are obtained for protection.
Embodiment 2
As shown in figure 1, a kind of many rotor housing constructions for being effectively reduced transport space of the present invention, in the base of embodiment 1
On plinth, the bottom of the groove 6 is provided with rotary wings seat 9, and wing 5 is provided with the top of the rotary wings seat, and the wing 5 is wrapped
Two fins 7 are included, two fins 7 are connected by bolt 8.Altitude mixture control machine is additionally provided between the rotary wings seat 9 and wing 5
Structure；The height adjustment mechanism is telescopic rod.Wing is not only protected with upper type, and without fin is removed, it is more convenient.
Above-described specific embodiment, has been carried out further to the purpose of the present invention, technical scheme and beneficial effect
Describe in detail, should be understood that the specific embodiment that the foregoing is only the present invention, be not intended to limit the present invention
Protection domain, all any modification, equivalent substitution and improvements within the spirit and principles in the present invention, done etc. all should include
Within protection scope of the present invention.
Claims (4)
1. a kind of many rotor housing constructions for being effectively reduced transport space, including body (1), several horns (2), its feature
It is that the strip groove (3) with the quantity such as horn (2), the center of the strip groove (3) are provided with the top of body (1)
Axis is located at same straight line with the central axis of horn (2), and the horn (2) matches with strip groove (3), in body (1)
Side wall is additionally provided with end plate (4), end plate (4) top and strip groove (3) bottom level, one end of end plate (4) and horn
(2) it is hinged；Wing (5) is additionally provided with the end of horn (2), the wing (5) includes two fins (7), on horn (2) top
Portion is additionally provided with groove (6), and the width of the groove (6) is matched with fin (7), and the depth of groove (6) is more than or equal to the wing
The twice of piece (7) thickness.
2. a kind of many rotor housing constructions for being effectively reduced transport space according to claim 1, it is characterised in that institute
The bottom for stating groove (6) is provided with rotary wings seat (9), and wing (5), the wing (5) are provided with the top of the rotary wings seat
Including two fins (7), two fins (7) are connected by bolt (8).
3. a kind of many rotor housing constructions for being effectively reduced transport space according to claim 2, it is characterised in that institute
State and be additionally provided with height adjustment mechanism between rotary wings seat (9) and wing (5).
4. a kind of many rotor housing constructions for being effectively reduced transport space according to claim 3, it is characterised in that institute
Height adjustment mechanism is stated for telescopic rod.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710004216.9A CN106672226A (en) | 2017-01-04 | 2017-01-04 | Multi-rotor vehicle body structure capable of effectively reducing transport space |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710004216.9A CN106672226A (en) | 2017-01-04 | 2017-01-04 | Multi-rotor vehicle body structure capable of effectively reducing transport space |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106672226A true CN106672226A (en) | 2017-05-17 |
Family
ID=58849847
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710004216.9A Pending CN106672226A (en) | 2017-01-04 | 2017-01-04 | Multi-rotor vehicle body structure capable of effectively reducing transport space |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106672226A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2233393A2 (en) * | 2009-03-23 | 2010-09-29 | Gregor Schnoell | Locking system |
| CN205031892U (en) * | 2015-10-11 | 2016-02-17 | 深圳市前海疆域智能科技股份有限公司 | Propeller component and have this propeller component's aircraft |
| WO2016066790A1 (en) * | 2014-10-30 | 2016-05-06 | École Polytechnique Fédérale de Lausanne | Fold able and self-deployable aerial vehicle |
| CN205327392U (en) * | 2016-01-29 | 2016-06-22 | 吴桂林 | Unmanned aerial vehicle centre frame structure |
| CN205633007U (en) * | 2016-05-20 | 2016-10-12 | 武汉科技大学 | Folding light energy is from four rotor unmanned aerial vehicle of electricity generation formula |
| CN106184729A (en) * | 2016-07-18 | 2016-12-07 | 山东龙翼航空科技有限公司 | A kind of many rotor wing unmanned aerial vehicles |
| CN206358358U (en) * | 2017-01-04 | 2017-07-28 | 四川克瑞斯航空科技有限公司 | A kind of many rotary wing aircraft foldable structures being readily transported |
-
2017
- 2017-01-04 CN CN201710004216.9A patent/CN106672226A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2233393A2 (en) * | 2009-03-23 | 2010-09-29 | Gregor Schnoell | Locking system |
| WO2016066790A1 (en) * | 2014-10-30 | 2016-05-06 | École Polytechnique Fédérale de Lausanne | Fold able and self-deployable aerial vehicle |
| CN205031892U (en) * | 2015-10-11 | 2016-02-17 | 深圳市前海疆域智能科技股份有限公司 | Propeller component and have this propeller component's aircraft |
| CN205327392U (en) * | 2016-01-29 | 2016-06-22 | 吴桂林 | Unmanned aerial vehicle centre frame structure |
| CN205633007U (en) * | 2016-05-20 | 2016-10-12 | 武汉科技大学 | Folding light energy is from four rotor unmanned aerial vehicle of electricity generation formula |
| CN106184729A (en) * | 2016-07-18 | 2016-12-07 | 山东龙翼航空科技有限公司 | A kind of many rotor wing unmanned aerial vehicles |
| CN206358358U (en) * | 2017-01-04 | 2017-07-28 | 四川克瑞斯航空科技有限公司 | A kind of many rotary wing aircraft foldable structures being readily transported |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170517 |
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| RJ01 | Rejection of invention patent application after publication |