CN205469803U - Manned aircraft - Google Patents
Manned aircraft Download PDFInfo
- Publication number
- CN205469803U CN205469803U CN201620100036.1U CN201620100036U CN205469803U CN 205469803 U CN205469803 U CN 205469803U CN 201620100036 U CN201620100036 U CN 201620100036U CN 205469803 U CN205469803 U CN 205469803U
- Authority
- CN
- China
- Prior art keywords
- horn
- propeller
- passenger cabin
- manned vehicle
- driving means
- 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.)
- Active
Links
- 238000009434 installation Methods 0.000 claims description 3
- 108010066057 cabin-1 Proteins 0.000 description 7
- 238000010586 diagram Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 3
- 238000010276 construction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005286 illumination Methods 0.000 description 1
- 230000005923 long-lasting effect Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
Classifications
-
- 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
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
- B64C27/10—Helicopters with two or more rotors arranged coaxially
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
- B64C27/14—Direct drive between power plant and rotor hub
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Toys (AREA)
Abstract
The utility model discloses a manned aircraft, including passenger cabin and bilge, the passenger cabin have can be manned the chamber that holds, the bilge setting the below of passenger cabin and with passenger cabin fixed connection, be provided with at least three horn on the bilge, all be equipped with first screw and second screw on every horn, first screw lies in the top of horn, the second screw lies in the below of horn, first screw is rotatory through the drive arrangement drive that corresponds, the second screw is rotatory through the 2nd drive arrangement drive that corresponds. Above -mentioned manned aircraft for ordinary unipolar aircraft or biax aircraft, can provide sufficient power for manned aircraft, keeps long -time flight. Satisfying under the condition of self load, replacing traditional scheme that disposes a jumbo size screw on every horn alone through disposing in every horn top and below than small -size's screw, can reduce the complete machine area occupied effectively.
Description
Technical field
This utility model relates to vehicle technology field, particularly to a kind of manned vehicle.
Background technology
The mankind have the ideal aloft flown as birds very early.For a long time, the mankind are for flying up into the sky
Various way has been use up in fantasy.Along with the development of science and technology, the dream that the mankind aloft fly becomes
Reality.Existing most of aircraft is mainly used in scientific research, and cost is sufficiently expensive, is not particularly suited for
Popular.Universal along with aircraft, simple to operate, use manned vehicle flexibly to arise at the historic moment.But mesh
Front manned vehicle mobility is poor, is only suitable for the flight under static conditions, it is impossible to fly in hovering, side
And the switching that is well between the state of flight such as rotation.
Summary of the invention
Based on this, this utility model is to overcome the defect of prior art, it is provided that a kind of manned vehicle, energy
Enough flying in hovering, side switches between the state of flight such as rotation smoothly, and mobility is good with handling.
Its technical scheme is as follows:
A kind of manned vehicle, including passenger cabin and hold, described passenger cabin has receiving chamber that can be manned, described
Hold is arranged on the lower section of passenger cabin and fixing with described passenger cabin is connected, and described hold is provided with at least three machine
Arm, each horn is equipped with the first propeller and the second propeller, and described first propeller is positioned at horn
Top, described second propeller is positioned at the lower section of horn, and described first propeller is by the first corresponding driving
Device drives and rotates, and described second propeller is driven by the second corresponding driving means and rotates.
Wherein in an embodiment, described horn is provided with mounting seat, and described first propeller is with corresponding
Connect between mounting seat and have described first driving means, connect between described second propeller and corresponding mounting seat
It is connected to described second driving means.
Wherein in an embodiment, the end of described horn is fixed with sleeve, and described mounting seat is fixed on set
In cylinder.
Wherein in an embodiment, described manned vehicle also includes fixed mechanism and connector, described solid
Determining mechanism to be fixed on hold, one end of described horn is hinged on fixed mechanism, and described fixed mechanism sets
Have the first installing hole, described horn to be provided with the second installing hole, when horn be in folding put state time, described company
One end of fitting is detachably connected on fixed mechanism by the first securing member, and the other end of described connector leads to
Cross the second securing member to be detachably connected on horn so that fixed mechanism and horn keep the first angle；Work as machine
When arm is in use state, the 3rd securing member is also cross the first installing hole and the second installing hole so that fixing
Mechanism is fixing with horn to be connected and keeps the second angle.
Wherein in an embodiment, on same horn, described first driving means drives described first spiral shell
Direction and described second driving means that rotation oar rotates drive the in opposite direction of described second propeller rotation.
Wherein in an embodiment, the front of described passenger cabin is provided with head lamp.
Wherein in an embodiment, described passenger cabin is provided with hatch door to be opened/closed.
Wherein in an embodiment, the bottom of described hold is provided with undercarriage.
Wherein in an embodiment, the top of described passenger cabin is provided with signal antenna, and described receiving intracavity is provided with
Seat.
Wherein in an embodiment, described horn is four, and four described horns are along the circumference of described hold
It is evenly arranged.
Advantage or principle to preceding solution illustrate below:
Above-mentioned manned vehicle, the horn arranged on hold is at least three, the top of each horn and under
Side is respectively equipped with a propeller, for common single shaft aircraft or twin shaft aircraft, it is possible to for
Manned vehicle provides enough power, keeps flying for long time.In the case of meeting self load-carrying, logical
Cross the propeller configuring reduced size above and below each horn to replace traditional list on each horn
Solely configure the scheme of a large scale propeller, it is possible to efficiently reduce complete machine area occupied.Meanwhile, manned
Aircraft can complete various flight by the rotating speed of adjustment different driving device respectively in flight course and move
Make, convenient control, it is possible to fly in hovering, side to switch smoothly between the state of flight such as rotation, mobility
Good with handling.
Accompanying drawing explanation
Fig. 1 is schematic diagram when being in use state of the manned vehicle described in this utility model embodiment；
Fig. 2 is the structural representation of the horn described in this utility model embodiment；
Fig. 3 is schematic diagram when being in use state of the horn described in this utility model embodiment；
Fig. 4 is that the manned vehicle described in this utility model embodiment is in the schematic diagram rolled over when putting state；
Fig. 5 is that the horn described in this utility model embodiment is in the schematic diagram rolled over when putting state.
Description of reference numerals:
1, passenger cabin, 2, hold, 3, horn, the 4, first propeller, the 5, second propeller, 6, first
Driving means, the 7, second driving means, 8, fixed mechanism, 9, connector, 10, accommodate chamber, 11, head
Lamp, 12, hatch door, 13, signal antenna, 14, seat, 20, undercarriage, 30, mounting seat, 31, set
Cylinder, the 32, second installing hole, the 80, first installing hole.
Detailed description of the invention
Below embodiment of the present utility model is described in detail:
As it is shown in figure 1, the manned vehicle described in the present embodiment, including passenger cabin 1 and hold 2, described passenger cabin
1 has receiving chamber 10 that can be manned, and described hold 2 is arranged on the lower section of passenger cabin 1 and consolidates with described passenger cabin 1
Fixed connect, described hold 2 be provided with four horns 3, each horn 3 is equipped with the first propeller 4 and
Second propeller 5, described first propeller 4 is positioned at the top of horn 3, and described second propeller 5 is positioned at machine
The lower section of arm 3, described first propeller 4 is driven by the first corresponding driving means 6 and rotates, and described the
Two propellers 5 are driven by the second corresponding driving means 7 and rotate.Above-mentioned manned vehicle, at hold 2
The horn 3 of upper setting is four, each horn 3 be respectively equipped with a propeller over and under, totally eight
Individual propeller, for common single shaft aircraft or twin shaft aircraft, it is possible to carry for manned vehicle
For enough power, keep flying for long time.In the case of meeting self load-carrying, by each horn 3
Above and below configure the propeller of reduced size and traditional on each horn 3, be separately configured one replacing
The scheme of large scale propeller, it is possible to efficiently reduce complete machine area occupied.Meanwhile, manned vehicle is flying
Various flare maneuver can be completed by the rotating speed of adjustment different driving device respectively during row, conveniently control,
Can fly to switch smoothly between the state of flight such as rotation in hovering, side, mobility and handling are good.
Preferably, four described horns 3 are evenly arranged along the circumference of described hold 2, and flight stability is higher.Can
With understand, the quantity of horn 2 can also be other number of three and more than three, preferably even number.
As in figure 2 it is shown, described horn 3 is provided with mounting seat 30, described first propeller 4 and corresponding peace
Connect between dress seat 30 and have described first driving means 6, described second propeller 5 and corresponding mounting seat 30
Between connect have described second driving means 7.First propeller the 4, first driving means the 6, second propeller
5 and second driving means 7 be fixed on horn 3 by mounting seat 30, install connect simple, final assembly
More stable.Under the strength conditions ensureing hold 2, reduce the weight of aircraft, it is achieved more longlasting flight.
In the present embodiment, the end of described horn 3 is fixed with sleeve 31, and described mounting seat 30 is fixed on set
In cylinder 31.Mounting seat 30 is inlaid in the end of horn 3, reduces the moment that driving means produces, make machine
The weight of arm 3 end is down to minimum, is effectively reduced weight, extends the flight time.In other embodiments,
First propeller 4 and the second propeller 5 can also be fixed on other position of horn 3 according to actual needs.
As in Figure 3-5, described manned vehicle also includes fixed mechanism 8 and connector 9, described fixing machine
Structure 8 is fixed on hold 2, and one end of described horn 3 is hinged on fixed mechanism 8, described fixed mechanism 8
Being provided with the first installing hole 80, described horn 3 is provided with the second installing hole 32, puts shape when horn 3 is in folding
During state, one end of described connector 9 is detachably connected on fixed mechanism 8 by the first securing member, described
The other end of connector 9 is detachably connected on horn 3 by the second securing member so that fixed mechanism 8 with
Horn 3 keeps the first angle；When horn 3 is in use state, the 3rd securing member is also cross the first peace
Dress hole 80 and the second installing hole 32 so that fixed mechanism 8 is fixing with horn 3 to be connected and keeps the second angle.
Horn 3 is hinged with fixed mechanism 8, can change the angle between horn 3 and fixed mechanism 8, it is achieved horn 3
Folding put state with use state switching.When transport and collection aircraft, by the first securing member, the
Two securing member installation connecting elements 9 so that fixed mechanism 8 and horn 3 keep the first angle, effectively reduce and take
Space；Pull down connector 9 when using aircraft, and connect fixed mechanism 8 and horn by the 3rd securing member
3 so that fixed mechanism 8 and horn 3 keep the second angle, simple in construction is easy for installation.
Preferably, on same horn 3, described first driving means 6 drives described first propeller 4 to revolve
The direction turned and described second driving means 7 drive the in opposite direction of described second propeller 5 rotation, described
First propeller 4 is arranged vertically with described second propeller 5 so that manned vehicle is logical in flight course
The rotating speed crossing adjustment different driving device respectively can complete various flare maneuver, and handling is more preferable, and
Achieve equalising torque, fly more stable.The central axis of described first propeller 4 and described second spiral
The central axis of oar 5 is positioned on same vertical curve, makes manned vehicle be easier to holding when changing course and flies
Line height, flies safer.
As it is shown in figure 1, the front of described passenger cabin 1 is provided with head lamp 11, it is used for driving illumination, enhances dark
The safety of middle driving.Described passenger cabin 1 is provided with hatch door 12 to be opened/closed, and pilot can be entered by hatch door 12
Accommodate in chamber 10 and drive.The bottom of described hold 2 is provided with undercarriage 20, rising for manned vehicle
Fly and landing.The top of described passenger cabin 1 is provided with signal antenna 13, is used for receiving signal.Described receiving chamber 10
Inside it is provided with the seat 14 providing pilot to drive use.
In the present embodiment, the first driving means 6 and the second driving means 7 are motor.First drives dress
Put 6 and second driving means 7 can also use other actuating unit according to actual needs.
Each technical characteristic of embodiment described above can combine arbitrarily, for making description succinct, the most right
The all possible combination of each technical characteristic in above-described embodiment is all described, but, if these skills
There is not contradiction in the combination of art feature, is all considered to be the scope that this specification is recorded.
Embodiment described above only have expressed several embodiments of the present utility model, its describe more concrete and
In detail, but therefore can not be interpreted as the restriction to utility model patent scope.It should be pointed out that, it is right
For those of ordinary skill in the art, without departing from the concept of the premise utility, it is also possible to do
Going out some deformation and improvement, these broadly fall into protection domain of the present utility model.Therefore, this utility model is special
The protection domain of profit should be as the criterion with claims.
Claims (10)
1. a manned vehicle, it is characterised in that including that passenger cabin and hold, described passenger cabin have can be manned
Receiving chamber, described hold is arranged on the lower section of passenger cabin and fixing with described passenger cabin is connected, described hold sets
It is equipped with at least three horn, each horn is equipped with the first propeller and the second propeller, described first spiral shell
Rotation oar is positioned at the top of horn, and described second propeller is positioned at the lower section of horn, and described first propeller passes through
The first corresponding driving means drives and rotates, and described second propeller is driven by the second corresponding driving means
Rotate.
Manned vehicle the most according to claim 1, it is characterised in that described horn is provided with installation
Seat, connects between described first propeller and corresponding mounting seat and has described first driving means, and described second
Connect between propeller and corresponding mounting seat and have described second driving means.
Manned vehicle the most according to claim 2, it is characterised in that the end of described horn is fixed
Sleeve, described mounting seat is had to be fixed in sleeve.
Manned vehicle the most according to claim 1, it is characterised in that also include fixed mechanism and company
Fitting, described fixed mechanism is fixed on hold, and one end of described horn is hinged on fixed mechanism, described
Fixed mechanism is provided with the first installing hole, and described horn is provided with the second installing hole, puts shape when horn is in folding
During state, one end of described connector is detachably connected on fixed mechanism by the first securing member, described connection
The other end of part is detachably connected on horn by the second securing member so that fixed mechanism and horn keep the
One angle；When horn is in use state, the 3rd securing member is installed also cross the first installing hole and second
Hole so that fixed mechanism is fixing with horn to be connected and keeps the second angle.
Manned vehicle the most according to claim 1, it is characterised in that on same horn, described
The direction that first driving means drives described first propeller to rotate drives described the with described second driving means
It is in opposite direction that two propellers rotate.
Manned vehicle the most according to claim 1, it is characterised in that the front of described passenger cabin is provided with
Head lamp.
Manned vehicle the most according to claim 1, it is characterised in that described passenger cabin is provided with can be opened
The hatch door closed.
Manned vehicle the most according to claim 1, it is characterised in that the bottom of described hold is provided with
Undercarriage.
Manned vehicle the most according to claim 1, it is characterised in that the top of described passenger cabin is provided with
Signal antenna, described receiving intracavity is provided with seat.
10. according to the manned vehicle described in any one of claim 1-9, it is characterised in that described horn
Being four, four described horns are evenly arranged along the circumference of described hold.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620100036.1U CN205469803U (en) | 2016-02-01 | 2016-02-01 | Manned aircraft |
| PCT/CN2016/106632 WO2017133302A1 (en) | 2016-02-01 | 2016-11-21 | Manned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620100036.1U CN205469803U (en) | 2016-02-01 | 2016-02-01 | Manned aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205469803U true CN205469803U (en) | 2016-08-17 |
Family
ID=56673049
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620100036.1U Active CN205469803U (en) | 2016-02-01 | 2016-02-01 | Manned aircraft |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN205469803U (en) |
| WO (1) | WO2017133302A1 (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2017107720A1 (en) * | 2015-12-25 | 2017-06-29 | 广州亿航智能技术有限公司 | Multirotor manned aerial vehicle |
| CN106986012A (en) * | 2017-04-26 | 2017-07-28 | 青岛福瑞泰科智能科技有限公司 | Low latitude manned vehicle |
| WO2017133302A1 (en) * | 2016-02-01 | 2017-08-10 | 广州亿航智能技术有限公司 | Manned aerial vehicle |
| CN108313280A (en) * | 2018-03-05 | 2018-07-24 | 上海市第中学 | A kind of aircraft |
| CN111315654A (en) * | 2017-06-01 | 2020-06-19 | 舒尔弗莱股份有限公司 | Auxiliary power system for rotorcraft having folding rotor arms and crush zone landing gear |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101575004A (en) * | 2009-06-09 | 2009-11-11 | 徐锦法 | Flight-mode-variable unmanned aircraft with multiple sets of coaxial rotors |
| CN201849660U (en) * | 2010-11-15 | 2011-06-01 | 佛山市安尔康姆航拍科技有限公司 | Supporting arm structure of multi-rotary aerofoil |
| KR20130130116A (en) * | 2012-01-06 | 2013-12-02 | 서울대학교산학협력단 | Multi-rotor aircraft |
| US20140231582A1 (en) * | 2012-10-03 | 2014-08-21 | Sean Headrick | Methods and Systems of Constructing a Multi Rotor Aircraft Fuselage |
| CN103721421A (en) * | 2012-10-16 | 2014-04-16 | 田瑜 | Aircraft with a plurality of rotors |
| DE202013004664U1 (en) * | 2013-05-17 | 2013-07-12 | AIRVIONIC UG (haftungsbeschränkt) | LED flood Multicopter. A multirotor aircraft with a high-power LED attached to illuminate large areas. |
| CN103625632A (en) * | 2013-11-29 | 2014-03-12 | 陈科学 | Manned aircraft |
| CN203601559U (en) * | 2013-11-29 | 2014-05-21 | 陈科学 | Manned craft |
| CN105014687A (en) * | 2015-08-07 | 2015-11-04 | 东北电力大学 | Mechanical arm with multi-rotor-wing unmanned aerial vehicle |
| CN205469803U (en) * | 2016-02-01 | 2016-08-17 | 广州亿航智能技术有限公司 | Manned aircraft |
-
2016
- 2016-02-01 CN CN201620100036.1U patent/CN205469803U/en active Active
- 2016-11-21 WO PCT/CN2016/106632 patent/WO2017133302A1/en active Application Filing
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2017107720A1 (en) * | 2015-12-25 | 2017-06-29 | 广州亿航智能技术有限公司 | Multirotor manned aerial vehicle |
| WO2017133302A1 (en) * | 2016-02-01 | 2017-08-10 | 广州亿航智能技术有限公司 | Manned aerial vehicle |
| CN106986012A (en) * | 2017-04-26 | 2017-07-28 | 青岛福瑞泰科智能科技有限公司 | Low latitude manned vehicle |
| CN111315654A (en) * | 2017-06-01 | 2020-06-19 | 舒尔弗莱股份有限公司 | Auxiliary power system for rotorcraft having folding rotor arms and crush zone landing gear |
| CN108313280A (en) * | 2018-03-05 | 2018-07-24 | 上海市第中学 | A kind of aircraft |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2017133302A1 (en) | 2017-08-10 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |