CN107972856A - One kind balance multi-rotor aerocraft - Google Patents
One kind balance multi-rotor aerocraft Download PDFInfo
- Publication number
- CN107972856A CN107972856A CN201711254365.7A CN201711254365A CN107972856A CN 107972856 A CN107972856 A CN 107972856A CN 201711254365 A CN201711254365 A CN 201711254365A CN 107972856 A CN107972856 A CN 107972856A
- Authority
- CN
- China
- Prior art keywords
- rotor
- fuselage
- jack
- post
- small
- 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- Withdrawn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
- 238000000034 method Methods 0.000 claims description 5
- 230000006378 damage Effects 0.000 claims 2
- 230000007812 deficiency Effects 0.000 description 1
- 230000009187 flying Effects 0.000 description 1
- 230000001771 impaired effect Effects 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
-
- 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
- B64D47/08—Arrangements of cameras
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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
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Stereoscopic And Panoramic Photography (AREA)
Abstract
One kind balance multi-rotor aerocraft, belongs to vehicle technology field, more particularly to a kind of multi-rotor aerocraft, including video camera, remote controler, fuselage, rack, jack-post, big rotor, supporting rod, motor, ring protection shell and small rotor.It is furnished with control system and airborne equipment in fuselage.Video camera is embedded in fore-body and energy 360 rotates freely exploration.Big rotor fin is symmetrical and is mutually 30 degree of angles of attack.Small rotor fin is symmetrical and is mutually 30 degree of angles of attack.Supporting bar structure formed objects are equally symmetrically distributed in fuselage both sides.Motor is separately fixed on respective supporting rod.Small rotor is placed on motor.Interior smooth recessed structure can place small rotor wing tip wherein ring protection shell marginal center in a ring.Big rotor agree with jack-post can on jack-post opening and closing.Jack-post can on fuselage free vertical telescopic.A kind of balance multi-rotor aerocraft of the present invention, safety and stability is full-featured, can carry out operation with land in the air, save production cost.
Description
Technical field
One kind balance multi-rotor aerocraft, belongs to vehicle technology field, more particularly to a kind of multi-rotor aerocraft.
Background technology
Aircraft has come into the sight of people gradually with advances in technology, thus be widely used in exploration, agricultural,
People need the place of operation in the air in military, postal delivery, rescue and relief work and daily life, but traditional aircraft can only
Working at height is carried out, but is difficult to save oneself and aircraft is recycled, stability and safety in the event of unexpected run out of steam
Property is poor.
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 balance multi-rotor aerocraft of efficiency.
One kind balance multi-rotor aerocraft, including video camera, remote controler, fuselage, rack, jack-post, big rotor, supporting rod,
Motor, ring protection shell and small rotor.
It is furnished with control system and airborne equipment in the fuselage.The video camera is embedded in fore-body and energy 360 is free
Rotation exploration.The big rotor fin is symmetrical and is mutually 30 degree of angles of attack.The small rotor fin is symmetrical and is mutually 30 degree and meets
Angle.The supporting bar structure formed objects are equally symmetrically distributed in fuselage both sides.The motor is separately fixed at each self-supporting
On bar.The small rotor is placed on motor.Interior smooth recessed structure can be by small rotation in a ring for the ring protection shell marginal center
Cautiously point is placed wherein.The big rotor agree with jack-post can on jack-post opening and closing.The jack-post can be on fuselage certainly
By vertical telescopic.
It is described balance multi-rotor aerocraft working method be:Pass through remote controler after balance multi-rotor aerocraft standby for takeoff
Control the lift-off operation of electric motor starting small rotor, go up to the air operation when video camera be actuated for comprehensive prospecting and carry out relevant work,
The balance small rotor of multi-rotor aerocraft is caused to be damaged if running into harsh climate and burst factor in operation process, at this time
Jack-post will be stretched out out of fuselage, and the big rotor agreed with it, which will open, carries out spiraling, while small rotor stops rotating,
Reach and balance multi-rotor aerocraft landing after specifying ground.
A kind of balance multi-rotor aerocraft of the present invention, safety and stability is full-featured, can be made in the air with land
Industry, saves production cost.
Brief description of the drawings
Fig. 1 is the schematic perspective view for balancing multi-rotor aerocraft；Fig. 2 is the schematic side view for balancing multi-rotor aerocraft；
Fig. 3 is the schematic top plan view for balancing multi-rotor aerocraft.
In figure, 1- video cameras, 2- remote controlers, 3- fuselages, 4- racks, 5- jack-posts, the big rotors of 6-, 7- supporting rods, 8- motors,
9- ring protection shells, the small rotors of 10-.
Embodiment
The present invention is illustrated in conjunction with attached drawing, one kind balance multi-rotor aerocraft, including video camera 1, remote control
Device 2, fuselage 3, rack 4, jack-post 5, big rotor 6, supporting rod 7, motor 8, ring protection shell 9 and small rotor 10.
It is furnished with control system and airborne equipment in the fuselage 3.The video camera 1 be embedded in fuselage 3 it is anterior and can 360 from
Surveyed by rotation.6 fin of big rotor is symmetrical and is mutually 30 degree of angles of attack.10 fin of small rotor is symmetrical and is mutually 30
Spend the angle of attack.The 7 structure formed objects of supporting rod are equally symmetrically distributed in 3 both sides of fuselage.The motor 8 is separately fixed at respectively
On self-supporting bar 7.The small rotor 10 is placed on motor 8.9 marginal center of ring protection shell interior smooth recessed knot in a ring
Structure can place small 10 wing tip of rotor wherein.The big rotor 6 agree with jack-post 5 can on jack-post 5 opening and closing.The axis
Column 5 can on fuselage 3 free vertical telescopic.
The small lift-off of rotor 10 operation of electric motor starting is controlled by remote controler 2 after balance multi-rotor aerocraft standby for takeoff, it
Control motor 8 to start small rotor 10 by remote controler 2 afterwards to go up to the air operation, go up to the air operation when video camera 1 be actuated for it is comprehensive
Prospecting carries out relevant work, if harsh climate and burst factor are run into operation process to be caused to balance more rotor flyings
The small rotor 10 of device is impaired, and jack-post 5 will be stretched out out of fuselage 3 at this time, and opening is carried out rotation and flown by the big rotor 6 agreed with it
OK, while small rotor 10 stops rotating, and multi-rotor aerocraft landing is balanced after specified ground is reached.
A kind of balance multi-rotor aerocraft of the present invention, safety and stability is full-featured, can be made in the air with land
Industry, saves production cost.
Claims (3)
1. one kind balance multi-rotor aerocraft, it is characterised in that：Including video camera（1）, remote controler（2）, fuselage（3）, rack
（4）, jack-post（5）, big rotor（6）, supporting rod（7）, motor（8）, ring protection shell（9）With small rotor（10）；The fuselage（3）
It is interior to be furnished with control system and airborne equipment；The video camera（1）It is embedded in fuselage（3）Anterior and energy 360 rotates freely exploration；Institute
State big rotor（6）Fin is symmetrical and is mutually 15 degree of angles of attack；The small rotor（10）Fin is symmetrical and is mutually 15 degree of angles of attack；Institute
State supporting rod（7）Structure formed objects are equally symmetrically distributed in fuselage（3）Both sides；The motor（8）It is separately fixed at each
Supporting rod（7）On；The small rotor（10）It is placed on motor（8）On；The ring protection shell（9）Marginal center interior light in a ring
Sliding recessed structure can be by small rotor（10）Wing tip is placed wherein；The big rotor（6）Agree with jack-post（5）On can be in jack-post（5）On
Opening and closing；The jack-post（5）Can be in fuselage（3）Upper free vertical telescopic.
A kind of 2. balance multi-rotor aerocraft according to claim 1, it is characterised in that：Its working method is：It is accurate
It is standby take off after pass through remote controler（2）Control the small rotor of electric motor starting（10）Lift-off operation, passes through remote controler afterwards（2）Control motor
（8）Start small rotor（10）Go up to the air operation, go up to the air operation when video camera（1）It is actuated for comprehensive prospecting and carries out corresponding work
Make, if harsh climate and burst factor are run into operation process to be caused to balance the small rotor of multi-rotor aerocraft（10）By
Damage, at this time jack-post（5）Will be from fuselage（3）Interior stretching, agrees with big rotor on it（6）Spiraling is carried out by opening, at the same time
Small rotor（10）Stop rotating, multi-rotor aerocraft landing is balanced after specified ground is reached.
A kind of 3. balance multi-rotor aerocraft according to claim 1 or 2, it is characterised in that：In small rotor（10）It is subject to
Big rotor can be used after destruction（6）Continue operation.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711254365.7A CN107972856A (en) | 2017-12-03 | 2017-12-03 | One kind balance multi-rotor aerocraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711254365.7A CN107972856A (en) | 2017-12-03 | 2017-12-03 | One kind balance multi-rotor aerocraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107972856A true CN107972856A (en) | 2018-05-01 |
Family
ID=62008932
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711254365.7A Withdrawn CN107972856A (en) | 2017-12-03 | 2017-12-03 | One kind balance multi-rotor aerocraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107972856A (en) |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2733068A2 (en) * | 2012-11-15 | 2014-05-21 | Aviron Consulting Development and Manufacture for Advanced Aviation | A fixed winged aircraft with foldable auto-rotation rotor |
| CN105366046A (en) * | 2015-12-15 | 2016-03-02 | 江苏艾锐泰克无人飞行器科技有限公司 | Fixed-wing air vehicle and control method in vertical posture |
| CN205891232U (en) * | 2016-07-08 | 2017-01-18 | 上海工程技术大学 | Urgent safe launching appliance of four rotor unmanned aerial vehicle |
-
2017
- 2017-12-03 CN CN201711254365.7A patent/CN107972856A/en not_active Withdrawn
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2733068A2 (en) * | 2012-11-15 | 2014-05-21 | Aviron Consulting Development and Manufacture for Advanced Aviation | A fixed winged aircraft with foldable auto-rotation rotor |
| CN105366046A (en) * | 2015-12-15 | 2016-03-02 | 江苏艾锐泰克无人飞行器科技有限公司 | Fixed-wing air vehicle and control method in vertical posture |
| CN205891232U (en) * | 2016-07-08 | 2017-01-18 | 上海工程技术大学 | Urgent safe launching appliance of four rotor unmanned aerial vehicle |
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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 |
Application publication date: 20180501 |
|
| WW01 | Invention patent application withdrawn after publication |