CN107972860A - A kind of stabilized flight device - Google Patents
A kind of stabilized flight device Download PDFInfo
- Publication number
- CN107972860A CN107972860A CN201711255950.9A CN201711255950A CN107972860A CN 107972860 A CN107972860 A CN 107972860A CN 201711255950 A CN201711255950 A CN 201711255950A CN 107972860 A CN107972860 A CN 107972860A
- Authority
- CN
- China
- Prior art keywords
- rotor
- wing
- fuselage
- stabilized flight
- flight device
- 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- Withdrawn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
- 238000006243 chemical reaction Methods 0.000 claims abstract description 15
- 238000000034 method Methods 0.000 claims description 6
- 230000004888 barrier function Effects 0.000 claims description 3
- 239000007787 solid Substances 0.000 claims 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S15/00—Systems using the reflection or reradiation of acoustic waves, e.g. sonar systems
- G01S15/88—Sonar systems specially adapted for specific applications
- G01S15/93—Sonar systems specially adapted for specific applications for anti-collision purposes
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Computer Networks & Wireless Communication (AREA)
- General Physics & Mathematics (AREA)
- Toys (AREA)
Abstract
A kind of stabilized flight device, belong to vehicle technology field, more particularly to a kind of stabilized flight device, including left fixed-wing, right fixed-wing, left front rotor, it is right before rotor, left back rotor, it is right after rotor, camera, acoustic receiver device, sound wave feedback device, acoustic detector, fuselage and rack.It is furnished with control system and airborne equipment in fuselage.Left fixed-wing and right fixed-wing are symmetrically distributed in fuselage both sides.Rotor, left back rotor are identical with one spline structure of rotor size behind the right side before left front rotor, the right side.Left front rotor fin can free conversion angle.Rotor fin can free conversion angle before the right side.Left back rotor fin can free conversion angle.Rotor fin can free conversion angle behind the right side.Camera is embedded in scalable in fuselage.Acoustic receiver device is placed on acoustic detector.Sound wave feedback device is placed on acoustic detector.Acoustic detector carves conjunction on fuselage.A kind of stabilized flight device, safety and stability is full-featured, saves production cost.
Description
Technical field
A kind of stabilized flight device, belongs to vehicle technology field, more particularly to a kind of stabilized flight device.
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 it is poor moreover, and function it is single.
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
A kind of higher stabilized flight device of efficiency.
Before a kind of stabilized flight device, including left fixed-wing, right fixed-wing, left front rotor, the right side behind rotor, left back rotor, the right side
Rotor, camera, acoustic receiver device, sound wave feedback device, acoustic detector, fuselage and rack.
It is furnished with control system and airborne equipment in the fuselage.The left fixed-wing and right fixed-wing are symmetrically distributed in fuselage
Both sides.Rotor, left back rotor are identical with one spline structure of rotor size behind the right side before the left front rotor, the right side.The left front rotor wing
Piece can free conversion angle.Rotor fin can free conversion angle before the right side.The left back rotor fin can free half-convergency
Degree.Rotor fin can free conversion angle behind the right side.The camera is embedded in scalable in fuselage.The acoustic receiver dress
It is placed on acoustic detector.The sound wave feedback device is placed on acoustic detector.The acoustic detector carves conjunction in fuselage
On.
A kind of working method of stabilized flight device is:Lift-off operation, takes the photograph at the same time after a kind of stabilized flight device takes off
, can be true by the acoustic receiver device on acoustic detector in the blind area of camera as head is actuated for comprehensive survey
Determine barrier and then sound wave feedback device feeds back to ground command system and carries out dangerous avoidance, if running into evil in operation process
Bad weather and burst factor causes a kind of stabilized flight device rotor to be damaged, at this time rotor, left back rotor before left front rotor, the right side
Stop rotating with rotor behind the right side, ground is dropped to by left fixed-wing and the gliding of right fixed-wing.
A kind of stabilized flight device of the present invention, safety and stability is full-featured, saves production cost.
Brief description of the drawings
Fig. 1 is a kind of schematic diagram of stabilized flight device.
In figure, the left fixed-wings of 1-, the right fixed-wings of 2-, the left front rotors of 3-, rotor before the 4- right sides, the left back rotors of 5-, 6- revolves behind the right side
The wing, 7- cameras, 8- acoustic receiver devices, 9- sound wave feedback devices, 10- acoustic detectors, 11- fuselages, 12- racks.
Embodiment
The present invention is illustrated in conjunction with attached drawing, a kind of stabilized flight device, including left fixed-wing 1, right fixed-wing
2nd, left front rotor 3, it is right before rotor 4, left back rotor 5, it is right after rotor 6, camera 7, acoustic receiver device 8, sound wave feedback device
9th, acoustic detector 10, fuselage 11 and rack 12.
It is furnished with control system and airborne equipment in the fuselage 11.The left fixed-wing 1 and right fixed-wing 2 are symmetrically distributed in
Fuselage both sides.Rotor 4, left back rotor 5 are identical with 6 size, one spline structure of rotor behind the right side before the left front rotor 3, the right side.The left side
Preceding 3 fin of rotor can free conversion angle.4 fin of rotor can free conversion angle before the right side.5 fin of left back rotor can
Free conversion angle.6 fin of rotor can free conversion angle behind the right side.The camera 7 is embedded in scalable in fuselage 11.
The acoustic receiver device 8 is placed in 10 on acoustic detector.The sound wave feedback device 9 is placed on acoustic detector 10.It is described
Acoustic detector 10 carves conjunction on fuselage 11.
A kind of working method of stabilized flight device is:Lift-off operation, takes the photograph at the same time after a kind of stabilized flight device takes off
Comprehensive survey is actuated for as first 7, is filled in the acoustic receiver that the blind area of camera 7 can pass through on acoustic detector 10
Put 8 and determine that barrier and then sound wave feedback device 9 feed back to ground command system and carry out dangerous avoidance, if in operation process
Running into harsh climate and burst factor causes a kind of stabilized flight device rotor to be damaged, at this time left front rotor 3, it is right before rotor 4,
Rotor 6 stops rotating after left back rotor 5 and the right side, and ground is dropped to by left fixed-wing 1 and the gliding of right fixed-wing 2.
A kind of stabilized flight device of the present invention, safety and stability is full-featured, saves production cost.
Claims (6)
- A kind of 1. stabilized flight device, it is characterised in that：Including left fixed-wing（1）, right fixed-wing（2）, left front rotor（3）, it is right before Rotor（4）, left back rotor（5）, it is right after rotor（6）, camera（7）, acoustic receiver device（8）, sound wave feedback device（9）, sound Wave detector（10）, fuselage（11）And rack（12）；The fuselage（11）It is interior to be furnished with control system and airborne equipment；It is described left solid Determine the wing（1）With right fixed-wing（2）It is symmetrically distributed in fuselage（11）Both sides；The left front rotor（3）, it is right before rotor（4）, left back rotation The wing（5）With rotor behind the right side（6）One spline structure of size is identical；The camera（7）It is embedded in fuselage（11）It is interior scalable；The sound Wave receiving device（8）It is placed in acoustic detector（10）On；The sound wave feedback device（9）It is placed in acoustic detector（10）On；Institute State acoustic detector（10）Conjunction is carved in fuselage（11）On.
- A kind of 2. stabilized flight device according to claim 1, it is characterised in that：Its working method is：After it takes off Go up to the air operation, while camera（7）Comprehensive survey is actuated for, in camera（7）Blind area can be visited by sound wave Survey device（10）On acoustic receiver device（8）Determine barrier and then sound wave feedback device（9）Feed back to ground command system into Row is dangerous to be avoided, if run into harsh climate in operation process and burst factor cause a kind of stabilized flight device rotor by Damage, at this time left front rotor（3）, it is right before rotor（4）, left back rotor（5）With rotor behind the right side（6）Stop rotating, pass through left fixed-wing （1）With right fixed-wing（2）Gliding drops to ground.
- A kind of 3. stabilized flight device according to claim 1 or 2, it is characterised in that：The left front rotor（3）Fin can be certainly By conversion angle.
- A kind of 4. stabilized flight device according to claim 1 or 2, it is characterised in that：Rotor before the right side（4）Fin can be certainly By conversion angle.
- A kind of 5. stabilized flight device according to claim 1 or 2, it is characterised in that：The left back rotor（5）Fin can be certainly By conversion angle.
- A kind of 6. stabilized flight device according to claim 1 or 2, it is characterised in that：Rotor behind the right side（6）Fin can be certainly By conversion angle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711255950.9A CN107972860A (en) | 2017-12-03 | 2017-12-03 | A kind of stabilized flight device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711255950.9A CN107972860A (en) | 2017-12-03 | 2017-12-03 | A kind of stabilized flight device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107972860A true CN107972860A (en) | 2018-05-01 |
Family
ID=62008974
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711255950.9A Withdrawn CN107972860A (en) | 2017-12-03 | 2017-12-03 | A kind of stabilized flight device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107972860A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103935512A (en) * | 2014-05-12 | 2014-07-23 | 马轶 | High endurable multi-rotor craft |
| CN104364154A (en) * | 2012-06-01 | 2015-02-18 | 洛高-蒂姆有限责任公司 | Aircraft, preferably unmanned |
| CN104724284A (en) * | 2015-03-25 | 2015-06-24 | 朱威 | Multi-rotor-wing submersible unmanned aerial vehicle and control method thereof |
| CN204956914U (en) * | 2015-09-17 | 2016-01-13 | 广东中安金狮科创有限公司 | Automatic unmanned aerial vehicle of flight is dodged and passes through in three dimensions range finding |
| CN105905286A (en) * | 2016-05-10 | 2016-08-31 | 深圳市旋翼捷科技有限公司 | Unmanned aerial vehicle with thrust line variable device |
| CN106494608A (en) * | 2015-09-06 | 2017-03-15 | 陈康 | Many shrouded propeller variable geometry Electric aircrafts |
| US20170158320A1 (en) * | 2015-09-20 | 2017-06-08 | Daniel Bosch | Unmanned aerial system |
-
2017
- 2017-12-03 CN CN201711255950.9A patent/CN107972860A/en not_active Withdrawn
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104364154A (en) * | 2012-06-01 | 2015-02-18 | 洛高-蒂姆有限责任公司 | Aircraft, preferably unmanned |
| CN103935512A (en) * | 2014-05-12 | 2014-07-23 | 马轶 | High endurable multi-rotor craft |
| CN104724284A (en) * | 2015-03-25 | 2015-06-24 | 朱威 | Multi-rotor-wing submersible unmanned aerial vehicle and control method thereof |
| CN106494608A (en) * | 2015-09-06 | 2017-03-15 | 陈康 | Many shrouded propeller variable geometry Electric aircrafts |
| CN204956914U (en) * | 2015-09-17 | 2016-01-13 | 广东中安金狮科创有限公司 | Automatic unmanned aerial vehicle of flight is dodged and passes through in three dimensions range finding |
| US20170158320A1 (en) * | 2015-09-20 | 2017-06-08 | Daniel Bosch | Unmanned aerial system |
| CN105905286A (en) * | 2016-05-10 | 2016-08-31 | 深圳市旋翼捷科技有限公司 | Unmanned aerial vehicle with thrust line variable device |
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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: 20180501 |