CN110282127A - A kind of tailstock formula unmanned plane - Google Patents
A kind of tailstock formula unmanned plane Download PDFInfo
- Publication number
- CN110282127A CN110282127A CN201910586739.8A CN201910586739A CN110282127A CN 110282127 A CN110282127 A CN 110282127A CN 201910586739 A CN201910586739 A CN 201910586739A CN 110282127 A CN110282127 A CN 110282127A
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- tail
- supporting rod
- unmanned plane
- vertical
- wing
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- 230000007704 transition Effects 0.000 description 3
- 238000006243 chemical reaction Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/02—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis vertical when grounded
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/25—Fixed-wing aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
A kind of tailstock formula unmanned plane, belongs to unmanned aerial vehicle design field.Consistent with existing unmanned plane for the basic structure of tailstock formula unmanned plane, it is as follows to improve place: the tail supporting rod totally two, top is separately connected propeller and engine；The side of wing is fixed on tail supporting rod top；The lower part of tail supporting rod is arranged tailplane and vertical tail, the blower tray that verts is set among two tailplanes, setting on blower tray of verting is verted fan and its driving motor, and the surfaces of revolution of vert fan and its driving motor is perpendicular to the ground, parallel with wing place plane；Rudder is set on vertical tail；Bracket at tail part is arranged in tail supporting rod bottom end, and bracket at tail part is vertical with plane where wing.The Novel platform of vertical take-off and landing drone can be developed using the placement scheme, carries different task load, and there is broad prospect of application.
Description
Technical field
The invention belongs to unmanned aerial vehicle design fields, and in particular to a kind of vertical take-off and landing drone.
Background technique
Carry out the fast development of unmanned plane market in recent years, application field is constantly widened.Presently, fixed-wing and rotor class
It is most common two kinds of unmanned plane types.They have respective advantage and disadvantage.The pneumatic efficiency of fixed wing aircraft is high, voyage, boat
When, the speed of a ship or plane it is all dominant, but its landing needs runway, or by catapult-assisted take-off, parachuting/net collision recovery.Rotor class is (comprising straight
Rising machine and more rotors) VTOL (VTOL), spot hover may be implemented in layout, and low-speed maneuver performance is good, but pneumatic efficiency is remote
Not as good as fixed-wing, voyage, endurance and the speed of a ship or plane are all not so good as fixed wing aircraft.Therefore, fusion fixed wing aircraft cruise advantage and rotor
The hybrid aircraft of machine VTOL function is always the emphasis of aviation field research.Tailstock formula aircraft is mixed type unmanned plane
A kind of placement scheme, structure is simple, and efficiency is higher, there is very big application potential.But the cloth of the current mainstream of tailstock formula unmanned plane
Office's scheme type is seldom, there is its respective defect.
Summary of the invention
The fan that verts the purpose of the present invention is to propose to a double hair, double shoes, using tail portion realizes horizontal vertical flight mould
The unmanned placement scheme of tailstock formula of formula transition, the Novel platform of vertical take-off and landing drone can be developed using the placement scheme,
Different task load is carried, there is broad prospect of application.
Technical solution of the present invention:
A kind of tailstock formula unmanned plane, the tailstock formula unmanned plane include fuselage 1, wing 2, aileron 3, propeller and start
Machine 4, tail supporting rod 5, tailplane 6, vertical tail 7, the blower tray 8 that verts, vert fan and its driving motor 9, rudder 10
With bracket at tail part 11.It is consistent with existing unmanned plane for the basic structure of tailstock formula unmanned plane, it is as follows to improve place:
The tail supporting rod 5 totally two, top is separately connected propeller and engine 4；Machine is fixed on 5 top of tail supporting rod
The side of the wing 2；The lower part of tail supporting rod 5 is arranged tailplane 6 and vertical tail 7, and the fan that verts is arranged among two tailplanes 6
Bracket 8, setting is verted fan and its driving motor 9 on the blower tray 8 that verts, the surfaces of revolution of vert fan and its driving motor 9
It is perpendicular to the ground, parallel with 2 place plane of wing；Rudder 10 is set on vertical tail 7；Tail portion is arranged in 5 bottom end of tail supporting rod
Bracket 11, bracket at tail part 11 are vertical with 2 place plane of wing.
Beneficial effects of the present invention:
(1) it is horizontal without runway, the advantage that can vertically hover and fixed wing aircraft to combine rotor class aircraft for unmanned plane
The speed of a ship or plane is fast when cruise, loads biggish advantage.
(1) double hair Bi-Tail-Boom Layout structures are simple, and pneumatic efficiency is high.Twin screw reversely rotates, and that just offsets is respective
Reaction torque, the anti-twisted moment problem for avoiding single-shot single screw from being laid out, also unlike single-shot coaxial spirals paddle structures is complicated, pneumatic effect
Rate is lower.Relative to four or even more multi-engined layout, two motors can provide enough pulling force and realize hanging down for aircraft
Straight landing and transition of verting, avoid engine number redundancy from increasing weight.
(2) fan that verts is separately provided in the middle part of tailplane vertically to hover for realizing unmanned plane and level cruise state
Between transition flight, manipulate it is simple and reliable；And mainstream tailstock formula unmanned plane generally utilizes the rudder being immersed in screw current
Posture conversion is realized in face, and control difficulty is larger.
Detailed description of the invention
Fig. 1 is the isometric drawing of unmanned plane.
In figure: 1 fuselage, 2 wings, 3 ailerons, 4 propellers and engine, 5 tail supporting rods, 6 tailplanes, 7 vertical tails, 8
Vert blower tray, and 9 vert fan and its driving motor, 10 rudders, 11 bracket at tail part
Specific embodiment
Technical solution of the present invention is further described below according to specific embodiment.
When tailstock formula unmanned plane grounds, ground is vertically stood on by bracket at tail part 11.Twin screw and engine 4 when taking off
Work, the lift that propeller generates are gradually increased, and when lift is more than gravity, aircraft is liftoff, into hovering mode.At this moment it manipulates
It verts the fan rotation of verting of fan and its driving motor 9, unmanned plane can be made to be moved forward and backward.Continue to increase turning for the fan that verts
Speed, the unmanned plane angle of attack are gradually reduced from 90 degree, and aircraft forward flight speed increases, and lift is gradually increased, until being transitioned into level cruise
Mode.
Unmanned plane landing is the inverse process to take off.When landing, manipulates the fan that verts and the unmanned plane angle of attack is made to increase to 90 degree,
Aircraft enters vertical floating state, and subsequent twin screw and 4 revolving speed of engine are gradually reduced, unmanned plane height decline, until tail
Portion's bracket 11 and ground face contact, complete descent.
Claims (1)
1. a kind of tailstock formula unmanned plane, which is characterized in that the tailstock formula unmanned plane includes fuselage (1), wing (2), aileron
(3), propeller and engine (4), tail supporting rod (5), tailplane (6), vertical tail (7), the blower tray that verts (8), vert
Fan and its driving motor (9), rudder (10) and bracket at tail part (11)；
The tail supporting rod (5) totally two, top are separately connected propeller and engine (4)；Tail supporting rod (5) top is fixed on
The side of wing (2)；The lower part of tail supporting rod (5) is arranged tailplane (6) and vertical tail (7), and two tailplanes (6) are intermediate
Setting is verted blower tray (8), and setting is verted fan and its driving motor (9) on the blower tray that verts (8), vert fan and its
The surfaces of revolution of driving motor (9) is perpendicular to the ground, parallel with plane where wing (2)；Rudder (10) is set to vertical tail
(7) on；Bracket at tail part (11) are arranged in tail supporting rod (5) bottom end, and bracket at tail part (11) is vertical with plane where wing (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910586739.8A CN110282127A (en) | 2019-07-01 | 2019-07-01 | A kind of tailstock formula unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910586739.8A CN110282127A (en) | 2019-07-01 | 2019-07-01 | A kind of tailstock formula unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110282127A true CN110282127A (en) | 2019-09-27 |
Family
ID=68021587
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910586739.8A Withdrawn CN110282127A (en) | 2019-07-01 | 2019-07-01 | A kind of tailstock formula unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110282127A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111619800A (en) * | 2020-06-05 | 2020-09-04 | 中国科学院长春光学精密机械与物理研究所 | Tail sitting type vertical take-off and landing unmanned aerial vehicle |
| CN112208757A (en) * | 2020-10-21 | 2021-01-12 | 中山大学 | Three-rotor tailstock type vertical take-off and landing unmanned aerial vehicle |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2394723C1 (en) * | 2009-04-13 | 2010-07-20 | Дмитрий Сергеевич Дуров | Multi-purpose cryogenic convertiplane |
| CN102133926A (en) * | 2011-03-08 | 2011-07-27 | 上海大学 | Tailstock type vertical take-off and landing unmanned aerial vehicle |
| CN105857605A (en) * | 2016-04-11 | 2016-08-17 | 河北科技大学 | Single sitting type fixed-wing unmanned aerial vehicle taking off and landing vertically |
| CN106828920A (en) * | 2017-02-20 | 2017-06-13 | 西安爱生技术集团公司 | It is a kind of can VTOL tailstock formula tailless configuration aircraft |
| CN107804456A (en) * | 2016-09-08 | 2018-03-16 | 朗星无人机系统有限公司 | A kind of how culvert vertical take-off and landing unmanned machine |
| CN108128448A (en) * | 2018-01-08 | 2018-06-08 | 浙江大学 | The coaxial tilting rotor wing unmanned aerial vehicle of double shoe formulas and its control method |
| KR20180089086A (en) * | 2017-01-31 | 2018-08-08 | (주)지이에스 | A Vertical Take off and Landing Quadrotor Drone having A Fixed Wing |
-
2019
- 2019-07-01 CN CN201910586739.8A patent/CN110282127A/en not_active Withdrawn
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2394723C1 (en) * | 2009-04-13 | 2010-07-20 | Дмитрий Сергеевич Дуров | Multi-purpose cryogenic convertiplane |
| CN102133926A (en) * | 2011-03-08 | 2011-07-27 | 上海大学 | Tailstock type vertical take-off and landing unmanned aerial vehicle |
| CN105857605A (en) * | 2016-04-11 | 2016-08-17 | 河北科技大学 | Single sitting type fixed-wing unmanned aerial vehicle taking off and landing vertically |
| CN107804456A (en) * | 2016-09-08 | 2018-03-16 | 朗星无人机系统有限公司 | A kind of how culvert vertical take-off and landing unmanned machine |
| KR20180089086A (en) * | 2017-01-31 | 2018-08-08 | (주)지이에스 | A Vertical Take off and Landing Quadrotor Drone having A Fixed Wing |
| CN106828920A (en) * | 2017-02-20 | 2017-06-13 | 西安爱生技术集团公司 | It is a kind of can VTOL tailstock formula tailless configuration aircraft |
| CN108128448A (en) * | 2018-01-08 | 2018-06-08 | 浙江大学 | The coaxial tilting rotor wing unmanned aerial vehicle of double shoe formulas and its control method |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111619800A (en) * | 2020-06-05 | 2020-09-04 | 中国科学院长春光学精密机械与物理研究所 | Tail sitting type vertical take-off and landing unmanned aerial vehicle |
| CN112208757A (en) * | 2020-10-21 | 2021-01-12 | 中山大学 | Three-rotor tailstock type vertical take-off and landing unmanned aerial vehicle |
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| PB01 | Publication | ||
| PB01 | Publication | ||
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Application publication date: 20190927 |