CN107933903A - One kind stablizes more rotor hook goods aircraft - Google Patents
One kind stablizes more rotor hook goods aircraft Download PDFInfo
- Publication number
- CN107933903A CN107933903A CN201711254364.2A CN201711254364A CN107933903A CN 107933903 A CN107933903 A CN 107933903A CN 201711254364 A CN201711254364 A CN 201711254364A CN 107933903 A CN107933903 A CN 107933903A
- Authority
- CN
- China
- Prior art keywords
- rotor
- fuselage
- hook
- jack
- post
- 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
- 238000000034 method Methods 0.000 claims description 6
- 230000005611 electricity Effects 0.000 claims 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000001771 impaired 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
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Load-Engaging Elements For Cranes (AREA)
Abstract
One kind stablizes more rotor hook goods aircraft; belong to vehicle technology field; more particularly to a kind of more rotor hook goods aircraft, it includes exploration device, remote controler, fuselage, rack, jack-post, big rotor, supporting rod, motor, ring protection shell, small rotor and strip line hook.It is furnished with control system and airborne equipment in fuselage.Exploration device is embedded in fore-body and 360 ° of energy rotates freely exploration.Big rotor fin is symmetrical and is mutually 15 degree of angles of attack.Small rotor fin is symmetrical and is mutually 15 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.Strip line hook being capable of freedom retractable line in fuselage.One kind stablizes more rotor hook goods aircraft, and safety and stability is cost-effective.
Description
Technical field
One kind stablizes more rotor hook goods aircraft, belongs to vehicle technology field, more particularly to one kind stablizes more rotor hook goods
Aircraft.
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, especially in short-distance transport cargo
In have a larger effect, but be difficult to save oneself and aircraft is recycled, stability and safety in the event of unexpected run out of steam
Property it is poor and.
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
Efficiency it is higher stablize more rotor hook goods aircraft.
One kind stablizes more rotor hook goods aircraft, including exploration device, remote controler, fuselage, rack, jack-post, big rotor, support
Bar, motor, ring protection shell, small rotor and strip line hook.
It is furnished with control system and airborne equipment in the fuselage.The exploration device is embedded in fore-body and can 360 ° of freedom
Rotation exploration.The big rotor fin is symmetrical and is mutually 15 degree of angles of attack.The small rotor fin is symmetrical and is mutually 15 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.Strip line hook being capable of freedom retractable line in fuselage.
It is described stablize more rotor hook goods aircraft working method be:Stablize more rotor hook goods aircraft standby for takeoff, it
Gone up to the air operation by the small rotor of remote control control electric motor starting afterwards, go up to the air operation when exploration device be actuated for comprehensive prospecting into
Row relevant work, if harsh climate and burst factor are run into operation process to be caused to stablize more rotor hook goods aircraft
Small rotor is damaged, and jack-post will be stretched out out of fuselage at this time, and the big rotor agreed with it, which will open, carries out spiraling, while small
Rotor stops rotating, and stablizes more rotor hook goods aircraft release strip line hooks after assignment place is reached, hook picking thing into
Row operation.
One kind of the present invention stablizes more rotor hook goods aircraft, and safety and stability is full-featured, can be carried out in the air with land
Operation, saves production cost.
Brief description of the drawings
Fig. 1 is the schematic perspective view for stablizing more rotor hook goods aircraft；Fig. 2 is the side view for stablizing more rotor hook goods aircraft
Schematic diagram；Fig. 3 is the schematic top plan view for stablizing more rotor hook goods aircraft.
In figure, 1- exploration devices, 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-, 11- strip line hooks.
Embodiment
The present invention is illustrated in conjunction with attached drawing, one kind stablizes more rotor hook goods aircraft, including exploration device 1,
Remote controler 2, fuselage 3, rack 4, jack-post 5, big rotor 6, supporting rod 7, motor 8, ring protection shell 9, small rotor 10 and strip line hook
Son 11.
It is furnished with control system and airborne equipment in the fuselage 3.The exploration device 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 15 degree of angles of attack.10 fin of small rotor is symmetrical and is mutually 15
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.Strip line hook 11 being capable of freedom retractable line in fuselage 3.
It is described stablize more rotor hook goods aircraft working method be:Stablize more rotor hook goods aircraft 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 exploration device 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 stablize more rotor hook goods
The small rotor 10 of aircraft is impaired, and jack-post 5 will be stretched out out of fuselage 3 at this time, and the big rotor 6 agreed with it is rotated opening
Flight, while small rotor 10 stops rotating, and stablizes more rotor hook goods aircraft release strip line hooks after assignment place is reached
Son 11, hooks picking thing and carries out operation.
One kind of the present invention stablizes more rotor hook goods aircraft, and safety and stability is full-featured, can be carried out in the air with land
Operation, saves production cost.
Claims (3)
1. one kind stablizes more rotor hook goods aircraft, it is characterised in that：Including surveying device（1）, remote controler（2）, fuselage（3）, machine
Frame（4）, jack-post（5）, big rotor（6）, supporting rod（7）, motor（8）, ring protection shell（9）, small rotor（10）With strip line hook
（11）；The fuselage（3）It is interior to be furnished with control system and airborne equipment；The exploration device（1）It is embedded in fuselage（3）Anterior and energy
360 ° rotate freely exploration；The big rotor（6）Fin is symmetrical and is mutually 15 degree of angles of attack；The small rotor（10）Fin is right
Claim and be mutually 15 degree of angles of attack；The supporting rod（7）Structure formed objects are equally symmetrically distributed in fuselage（3）Both sides；The electricity
Machine（8）It is separately fixed at respective supporting rod（7）On；The small rotor（10）It is placed on motor（8）On；The ring protection shell
（9）Interior smooth recessed structure can be by small rotor in a ring for marginal center（10）Wing tip is placed wherein；The big rotor（6）Agree with axis
Column（5）On can be in jack-post（5）Upper opening and closing；The jack-post（5）Can be in fuselage（3）Upper free vertical telescopic；The strip line hook
Son（11）In fuselage（3）It is interior being capable of freedom retractable line.
2. one kind according to claim 1 stablizes more rotor hook goods aircraft, it is characterised in that：Its working method is：
Its standby for takeoff, 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 survey
Device（1）It is actuated for comprehensive prospecting and carries out relevant work, if runs into harsh climate and burst in operation process
Factor causes to stablize the small rotor of more rotor hook goods aircraft（10）It is damaged, at this time jack-post（5）Will be from fuselage（3）Interior stretching, agrees with
Big rotor on it（6）It will open and carry out spiraling, while small rotor（10）Stop rotating, reach assignment place
After stablize more rotor hook goods aircraft release strip line hooks（11）, hook picking thing and carry out operation.
3. one kind according to claim 1 or 2 stablizes more rotor hook goods aircraft, it is characterised in that：Strip line hook（11）
By spiral winded type freely stretch.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711254364.2A CN107933903A (en) | 2017-12-03 | 2017-12-03 | One kind stablizes more rotor hook goods aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711254364.2A CN107933903A (en) | 2017-12-03 | 2017-12-03 | One kind stablizes more rotor hook goods aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107933903A true CN107933903A (en) | 2018-04-20 |
Family
ID=61947454
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711254364.2A Pending CN107933903A (en) | 2017-12-03 | 2017-12-03 | One kind stablizes more rotor hook goods aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107933903A (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20150102175A1 (en) * | 2012-11-15 | 2015-04-16 | Aviron Consulting Developmentand Manufacture For Advanced Aviation | Fixed winged aircraft with foldable auto-rotation rotor |
| CN104973241A (en) * | 2015-07-08 | 2015-10-14 | 芜湖万户航空航天科技有限公司 | Unmanned aerial vehicle with main and auxiliary multi-rotor structure |
| 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 |
| CN205168923U (en) * | 2015-11-11 | 2016-04-20 | 杭州深空实业股份有限公司 | Many rotor unmanned aerial vehicle hybrid power system |
| CN205738086U (en) * | 2016-05-13 | 2016-11-30 | 梅家崎 | A kind of rotor craft propeller protective cover and rotor craft |
| 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 |
| CN106741904A (en) * | 2017-01-24 | 2017-05-31 | 天津曙光天成科技有限公司 | A kind of compound unmanned vehicle |
| CN107187593A (en) * | 2017-06-22 | 2017-09-22 | 云南高科新农科技有限公司 | A kind of multiple degrees of freedom unmanned plane with twin rotor system |
-
2017
- 2017-12-03 CN CN201711254364.2A patent/CN107933903A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20150102175A1 (en) * | 2012-11-15 | 2015-04-16 | Aviron Consulting Developmentand Manufacture For Advanced Aviation | Fixed winged aircraft with foldable auto-rotation rotor |
| CN104973241A (en) * | 2015-07-08 | 2015-10-14 | 芜湖万户航空航天科技有限公司 | Unmanned aerial vehicle with main and auxiliary multi-rotor structure |
| CN205168923U (en) * | 2015-11-11 | 2016-04-20 | 杭州深空实业股份有限公司 | Many rotor unmanned aerial vehicle hybrid power system |
| 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 |
| CN205738086U (en) * | 2016-05-13 | 2016-11-30 | 梅家崎 | A kind of rotor craft propeller protective cover and rotor craft |
| 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 |
| CN106741904A (en) * | 2017-01-24 | 2017-05-31 | 天津曙光天成科技有限公司 | A kind of compound unmanned vehicle |
| CN107187593A (en) * | 2017-06-22 | 2017-09-22 | 云南高科新农科技有限公司 | A kind of multiple degrees of freedom unmanned plane with twin rotor system |
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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 | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180420 |
|
| WD01 | Invention patent application deemed withdrawn after publication |