CN107933904A - A kind of flexible aircraft - Google Patents
A kind of flexible aircraft Download PDFInfo
- Publication number
- CN107933904A CN107933904A CN201711276770.9A CN201711276770A CN107933904A CN 107933904 A CN107933904 A CN 107933904A CN 201711276770 A CN201711276770 A CN 201711276770A CN 107933904 A CN107933904 A CN 107933904A
- Authority
- CN
- China
- Prior art keywords
- supporting rod
- fuselage
- rotor
- placing
- motor
- 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.)
- Withdrawn
Links
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
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/34—Alighting gear characterised by elements which contact the ground or similar surface wheeled type, e.g. multi-wheeled bogies
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
A kind of flexible aircraft, belongs to vehicle technology field, more particularly to a kind of flexible aircraft, including fuselage, rotor, supporting rod, motor, ring protection shell and motor apparatus for placing.It is furnished with control system and airborne equipment in the fuselage.The rotor fin is symmetrical and can adjust fin Windward angle.The supporting bar structure formed objects are equally symmetrically distributed in fuselage both sides.The supporting rod can on standard of fuselage face 360 degree move horizontally.Motor is separately fixed at upper and lower on the supporting rod.Interior smooth recessed structure can place rotor wing tip wherein the ring protection shell marginal center in a ring.The motor apparatus for placing can be rotated horizontally in supporting rod outer end.A kind of flexible aircraft of the present invention, takeoff speed is fast, safety and stability, is not easy to damage, and can do Ground Operation.
Description
Technical field
A kind of flexible aircraft, belongs to vehicle technology field, more particularly to a kind of flexible aircraft.
Background technology
Aircraft has come into the sight of people gradually with advances in technology, thus be widely used in exploration, agricultural,
The place of people's needs operation in the air in military, postal delivery, rescue and relief work and daily life, but traditional aircraft takeoff
Time takes longer, is not easily accessible operation in narrow space, and be unable to land operation.
The content of the invention
The purpose of the present invention is overcoming the above-mentioned deficiency of traditional aircraft, it is simple to invent a kind of structure of convenient control
The higher flexible aircraft of efficiency.
A kind of flexible aircraft, including fuselage, rotor, supporting rod, motor, ring protection shell and motor apparatus for placing.
It is furnished with control system and airborne equipment in the fuselage.The rotor fin is symmetrical and can adjust fin angle windward
Degree.The supporting bar structure formed objects are equally symmetrically distributed in fuselage both sides.The supporting rod can be in standard of fuselage face
Upper 360 degree move horizontally.Motor is separately fixed at upper and lower on the supporting rod.The ring protection shell marginal center is in a ring
Interior smooth recessed structure can place rotor wing tip wherein.The motor apparatus for placing can be rotated horizontally in supporting rod outer end.
The flexibly working method of aircraft is:Flexible aircraft goes up to the air operation after quickly taking off, awing can be with
It is used for being suitable for each working space to adjust flight area by moving horizontally supporting rod and motor apparatus for placing, when landing can
To be used for doing wheel Ground Operation easy to use to adjust rotor angle by moving horizontally supporting rod and motor apparatus for placing.
A kind of flexible aircraft of the present invention, takeoff speed is fast, safety and stability, is not easy to damage, and can do Ground Operation.
Brief description of the drawings
Fig. 1 is the schematic perspective view of flexible aircraft.
In figure, 1- fuselages, 2- rotors, 3- supporting rods, 4- motors, 5- ring protection shells, 6- motor apparatus for placing.
Embodiment
The present invention is illustrated in conjunction with attached drawing, a kind of flexible aircraft, including fuselage 1, rotor 2, supporting rod
3rd, motor 4, ring protection shell 5 and motor apparatus for placing 6.It is furnished with control system and airborne equipment in the fuselage 1.The rotor
2 fins are symmetrical and can adjust fin Windward angle.The 3 structure formed objects of supporting rod are equally symmetrically distributed in fuselage 1
Both sides.The supporting rod 3 can on 1 horizontal plane of fuselage 360 degree move horizontally.Motor 4 is separately fixed on the supporting rod 3
Upper and lower.Interior smooth recessed structure can place rotor wing tip wherein 5 marginal center of ring protection shell in a ring.The motor
Apparatus for placing 6 can be rotated horizontally in 3 outer end of supporting rod.
The flexibly working method of aircraft is:Flexible aircraft goes up to the air operation after quickly taking off, awing can be with
It is used for being suitable for each working space to adjust flight area by moving horizontally supporting rod 3 and motor apparatus for placing 6, during landing
It can be used for making wheel ground work easy to use to adjust 2 angle of rotor by moving horizontally supporting rod 3 and motor apparatus for placing 6
Industry.
A kind of flexible aircraft of the present invention, takeoff speed is fast, safety and stability, is not easy to damage, and can do Ground Operation.
Claims (2)
- A kind of 1. flexible aircraft, it is characterised in that：Including fuselage（1）, rotor（2）, supporting rod（3）, motor（4）, annular protect Protective case（5）With motor apparatus for placing（6）；The fuselage（1）It is interior to be furnished with control system and airborne equipment；The rotor（2）Fin It is symmetrical and fin Windward angle can be adjusted；The supporting rod（3）Structure formed objects are equally symmetrically distributed in fuselage（1）Two Side；The supporting rod（3）Can be in fuselage（1）Moved horizontally for 360 degree on horizontal plane；The supporting rod（3）Upper motor（4）Respectively It is fixed on upper and lower；The ring protection shell（5）Interior smooth recessed structure can be by rotor in a ring for marginal center（2）Wing tip places it In；The motor apparatus for placing（6）Can be in supporting rod（3）Outer end rotates horizontally.
- A kind of 2. flexible aircraft according to claim 1, it is characterised in that：Its working method is：Flexible aircraft It is quick take off after go up to the air operation, awing can be by moving horizontally supporting rod（3）With motor apparatus for placing（6）It is winged to adjust Row area is used for being suitable for each working space, and when landing can be by moving horizontally supporting rod（3）With motor apparatus for placing（6） To adjust rotor（2）Angle is used for doing wheel Ground Operation easy to use.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711276770.9A CN107933904A (en) | 2017-12-06 | 2017-12-06 | A kind of flexible aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711276770.9A CN107933904A (en) | 2017-12-06 | 2017-12-06 | A kind of flexible aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107933904A true CN107933904A (en) | 2018-04-20 |
Family
ID=61945914
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711276770.9A Withdrawn CN107933904A (en) | 2017-12-06 | 2017-12-06 | A kind of flexible aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107933904A (en) |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201800918U (en) * | 2010-09-16 | 2011-04-20 | 中国计量学院 | Rotating telescopic flying device with four rotor wings |
| CN103419942A (en) * | 2013-09-10 | 2013-12-04 | 北京臻迪科技有限公司 | Unmanned aerial vehicle |
| CN204297097U (en) * | 2014-11-26 | 2015-04-29 | 成都好飞机器人科技有限公司 | For four rotor wing unmanned aerial vehicles that agriculture Pesticides sprays |
| CN204406208U (en) * | 2015-03-04 | 2015-06-17 | 杨昊林 | A kind of quadrotor of patrolling and examining for street lamp |
| CN204507269U (en) * | 2015-03-27 | 2015-07-29 | 马鞍山市赛迪智能科技有限公司 | A kind of unmanned plane tackling airborne aircraft |
| CN105775128A (en) * | 2016-02-22 | 2016-07-20 | 武汉智能鸟无人机有限公司 | Flight vehicle |
| CN205738086U (en) * | 2016-05-13 | 2016-11-30 | 梅家崎 | A kind of rotor craft propeller protective cover and rotor craft |
| CN206186713U (en) * | 2016-09-30 | 2017-05-24 | 潍坊歌尔电子有限公司 | Amphibious unmanned vehicles |
| CN206367591U (en) * | 2016-12-25 | 2017-08-01 | 芜湖元一航空科技有限公司 | A kind of many rotor mechanisms of unmanned plane |
| CN107323192A (en) * | 2017-06-21 | 2017-11-07 | 北京理工大学 | A kind of air-ground amphibious mobile robot |
-
2017
- 2017-12-06 CN CN201711276770.9A patent/CN107933904A/en not_active Withdrawn
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201800918U (en) * | 2010-09-16 | 2011-04-20 | 中国计量学院 | Rotating telescopic flying device with four rotor wings |
| CN103419942A (en) * | 2013-09-10 | 2013-12-04 | 北京臻迪科技有限公司 | Unmanned aerial vehicle |
| CN204297097U (en) * | 2014-11-26 | 2015-04-29 | 成都好飞机器人科技有限公司 | For four rotor wing unmanned aerial vehicles that agriculture Pesticides sprays |
| CN204406208U (en) * | 2015-03-04 | 2015-06-17 | 杨昊林 | A kind of quadrotor of patrolling and examining for street lamp |
| CN204507269U (en) * | 2015-03-27 | 2015-07-29 | 马鞍山市赛迪智能科技有限公司 | A kind of unmanned plane tackling airborne aircraft |
| CN105775128A (en) * | 2016-02-22 | 2016-07-20 | 武汉智能鸟无人机有限公司 | Flight vehicle |
| CN205738086U (en) * | 2016-05-13 | 2016-11-30 | 梅家崎 | A kind of rotor craft propeller protective cover and rotor craft |
| CN206186713U (en) * | 2016-09-30 | 2017-05-24 | 潍坊歌尔电子有限公司 | Amphibious unmanned vehicles |
| CN206367591U (en) * | 2016-12-25 | 2017-08-01 | 芜湖元一航空科技有限公司 | A kind of many rotor mechanisms of unmanned plane |
| CN107323192A (en) * | 2017-06-21 | 2017-11-07 | 北京理工大学 | A kind of air-ground amphibious mobile robot |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20180420 |