CN207580174U - A kind of vector power tailstock formula unmanned plane - Google Patents
A kind of vector power tailstock formula unmanned plane Download PDFInfo
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- CN207580174U CN207580174U CN201721754641.1U CN201721754641U CN207580174U CN 207580174 U CN207580174 U CN 207580174U CN 201721754641 U CN201721754641 U CN 201721754641U CN 207580174 U CN207580174 U CN 207580174U
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- steering engine
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- aileron
- vector
- unmanned plane
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Abstract
The utility model belongs to unmanned vehicle field, and in particular to a kind of vector power tailstock formula unmanned plane, including fuselage and wing, the wing is arranged on the both sides of fuselage, further includes empennage and vector power plant, and the empennage is arranged on afterbody；The vector power plant is arranged on wing, and the tail portion of the wing is hinged with aileron；Aileron steering engine is additionally provided on the wing, aileron steering engine rocking arm is provided on the aileron steering engine, the aileron steering engine rocking arm connects aileron by aileron steering engine connecting rod；The unmanned plane of the utility model has vector power plant, propeller can be rotated in certain range, and aileron and rudder are equipped with corresponding steering engine, can awing coordinate rotation, makes operability of the unmanned plane in wind stronger, flies more stable；It can realize the smooth transition between the vertical flight of unmanned plane and horizontal flight, reduce because wing stops, and the flight resistance generated.
Description
Technical field
The invention belongs to unmanned vehicle fields, and in particular to a kind of vector power tailstock formula unmanned plane.
Background technology
With the quick universal and extensive use of unmanned plane, people are to performances such as the landing of unmanned plane, speed and endurances
Requirement be continuously improved, can VTOL fixed-wing unmanned plane come into being.Can VTOL fixed-wing unmanned plane both had it is solid
Determine the advantages that wing unmanned plane during flying speed is fast, flying height is high, the cruise time is long, and the energy with VTOL and hovering
Power, can VTOL fixed-wing unmanned plane by common concern and extensively research.It currently can VTOL fixed-wing unmanned plane
Mainly there are three kinds of more rotor combination fixed-wing formulas, tilting rotor formula and tailstock formula forms, tailstock formula unmanned plane combines fixed-wing
It the advantages of unmanned plane and rotor wing unmanned aerial vehicle, has been favored by people, but since wing area is larger, can stop wind,
Rudder face driving efficiency is low, it is impossible to is adjusted well according to wind direction, when flight is easily interfered by wind, and wind resistance is poor, steady
Qualitative difference.
Utility model content
The utility model provides a kind of tailstock formula unmanned plane, and there is vector power plant can adjust in a certain range
The angle of propeller coordinates aileron and vertical fin to be manipulated, and control difficulty is small, and stability is good.
In order to solve the above-mentioned technical problem, the utility model provides a kind of vector power tailstock formula unmanned plane, including machine
Body and wing, the wing are arranged on the both sides of fuselage, further include empennage and vector power plant, and the empennage is arranged on fuselage
Tail portion；The vector power plant is arranged on wing, and the tail portion of the wing is hinged with aileron；It is additionally provided on the wing
Aileron steering engine is provided with aileron steering engine rocking arm on the aileron steering engine, and the aileron steering engine rocking arm passes through aileron steering engine connecting rod
Connect aileron.
Preferably, the vector power plant includes motor, propeller and vector steering engine, it is provided on the wing solid
Reservation, the motor are movably connected in by rotary shaft in fixed seat, the power output end connection propeller of the motor, described
Vector steering engine is arranged in fixed seat, and the vector steering engine is equipped with vector steering engine rocking arm, and the vector steering engine rocking arm passes through arrow
Measure the connection of steering engine connecting rod on the rotary shaft.
Preferably, the fixed seat is arranged on the leading edge in the middle part of wing.
Preferably, the empennage includes upper vertical fin and the lower vertical fin identical with upper vertical fin, the upper vertical fin and lower vertical fin
It is respectively placed in above and below afterbody.
Preferably, the tail portion of the upper vertical fin and lower vertical fin is hinged with rudder.
Preferably, being additionally provided with empennage steering engine on the upper vertical fin, the empennage steering engine is equipped with rudder steering engine rocking arm,
The rudder steering engine rocking arm is connected to by rudder steering engine connecting rod on rudder.
Preferably, the aileron steering engine is arranged in fixed seat.
Advantageous effect：
The unmanned plane of the utility model has vector power plant, and propeller, and aileron can be rotated in certain range
Corresponding steering engine is equipped with rudder, can awing coordinate rotation, makes operability of the unmanned plane in wind stronger, flies
Row is more stable；It can realize the smooth transition between the vertical flight of unmanned plane and horizontal flight, reduce because wing stops, and produce
Raw flight resistance.
The direction of propeller can be adjusted in certain angle by vector steering engine, flexible adjustment facilitates control to operate；Gu
Reservation is arranged on the leading edge in the middle part of wing, is easy for installation and removal；Upper vertical fin and lower vertical fin are respectively placed in the top of afterbody
And lower section, with symmetrical form design, the balance of fuselage can be kept with multi-angle；The tail portion of upper vertical fin and lower vertical fin is hinged with
Rudder, it is convenient to change angle with the wind；Rudder facilitates manual operation by empennage steering engine hue angle.
Description of the drawings
Fig. 1 is the structure diagram of the utility model unmanned plane；
Fig. 2 is vector powerplant configuration schematic diagram；
Attached drawing marks：1- fuselages, 2- wings, the upper vertical fins of 3-, 4- motors, 5- fixed seats, 6- vectors steering engine, 7- rudders,
8- empennages steering engine, 9- ailerons steering engine, 10- ailerons, 61- vector steering engines rocking arm, 62- vector steering engines connecting rod, 81- rudder steering engines
Rocking arm, 82- rudder steering engines connecting rod, 91- aileron steering engines rocking arm, 92- aileron steering engines connecting rod, 11- propellers, 12- rotations
Vertical fin under axis, 13-.
Specific embodiment
The embodiment of the utility model is further illustrated below in conjunction with the accompanying drawings.
A kind of vector power tailstock formula unmanned plane as shown in Figure 1, including fuselage 1 and wing 2, the wing 2 is arranged on
The both sides of fuselage 1, further include empennage and vector power plant, and the empennage is arranged on 1 tail portion of fuselage；The vector power plant
It is arranged on wing 2, the tail portion of the wing 2 is hinged with aileron 10；Aileron steering engine 9, the pair are additionally provided on the wing 2
Aileron steering engine rocking arm 91 is provided on wing steering engine 9, the aileron steering engine rocking arm 91 connects aileron by aileron steering engine connecting rod 91
10。
In the present embodiment, the vector power plant includes motor 4, propeller 11 and vector steering engine 6 as shown in Figure 2,
Fixed seat 5 is provided on the wing 2, the motor 4 is movably connected in by rotary shaft 12 in fixed seat 5, the motor 4
Power output end connects propeller 11, and the vector steering engine 6 is arranged in fixed seat 5, and the vector steering engine 6 is equipped with vector rudder
Machine rocking arm 61, the vector steering engine rocking arm 61 are connected to by vector steering engine connecting rod 62 in rotary shaft 12；The fixed seat 5 is set
Put the leading edge at 2 middle part of wing；The empennage includes upper vertical fin 3 and the lower vertical fin 13 identical with upper vertical fin 3, the upper vertical fin 3
It is respectively placed in above and below 1 tail portion of fuselage with lower vertical fin 13；The tail portion side of being hinged with of the upper vertical fin 3 and lower vertical fin 13
To rudder 7；Empennage steering engine 8 is additionally provided on the upper vertical fin 3, the empennage steering engine 8 is equipped with rudder steering engine rocking arm 81, the side
It is connected on rudder 7 by rudder steering engine connecting rod 82 to rudder steering engine rocking arm 81；The aileron steering engine 9 is arranged on fixed seat
On 5.In the present embodiment, the end of the wing of upper vertical fin, lower vertical fin and fuselage both sides is equipped with support column, the support of support column
It puts in same level, can realize the support to fuselage；It is additionally provided on unmanned plane and receives the device that controller sends out signal, it should
Reception device is existing wireless signal receiver, can receive the control signal that controller is sent out.
During takeoff and landing, the support column of the end of the wing of upper vertical fin, lower vertical fin and fuselage both sides lands, head to
On, it is taken off vertically by the synchronization for making motor on both sides wing 2 to realize；By the rotating speed for making motor on both sides wing 2
Rollover that is different and realizing unmanned plane；Propeller 10 is adjusted by vector steering engine 6 to rotate, while aileron steering engine 9 is made to adjust aileron
10 rotations, to realize the movement of leaning forward and swing back of unmanned plane；The adjustment propeller 10 of vector steering engine 6 is crossed to rotate, while make aileron rudder
Machine 9 adjusts aileron 10 and rotates or by empennage steering engine 8 come the rotation of adjustment direction rudder 7, to control the yaw of unmanned plane.
Specific embodiment of the utility model is described in detail above, but it is intended only as example, this practicality is new
Type is not restricted to above description specific embodiment.To those skilled in the art, it is any to the utility model carry out
It equivalent modifications and substitutes also all among the scope of the utility model.Therefore, in the spirit and scope for not departing from the utility model
Lower made impartial conversion and modification, all cover in the scope of the utility model.
Claims (7)
1. a kind of vector power tailstock formula unmanned plane, including fuselage (1) and wing (2), the wing (2) is arranged on fuselage (1)
Both sides, it is characterised in that：Empennage and vector power plant are further included, the empennage is arranged on fuselage (1) tail portion；The vector
Power plant is arranged on wing (2), and the tail portion of the wing (2) is hinged with aileron (10)；It is additionally provided on the wing (2)
Aileron steering engine (9) is provided with aileron steering engine rocking arm (91) on the aileron steering engine (9), and the aileron steering engine rocking arm (91) passes through
Aileron steering engine connecting rod (92) connection aileron (10).
2. a kind of vector power tailstock formula unmanned plane as described in claim 1, it is characterised in that：The vector power plant packet
Motor (4), propeller (11) and vector steering engine (6) are included, fixed seat (5) is provided on the wing (2), the motor (4) is logical
It crosses rotary shaft (12) to be movably connected in fixed seat (5), the power output end connection propeller (11) of the motor (4) is described
Vector steering engine (6) is arranged in fixed seat (5), and the vector steering engine (6) is equipped with vector steering engine rocking arm (61), the vector rudder
Machine rocking arm (61) is connected to by vector steering engine connecting rod (62) in rotary shaft (12).
3. a kind of vector power tailstock formula unmanned plane as claimed in claim 2, it is characterised in that：Fixed seat (5) setting
Leading edge in the middle part of wing (2).
4. a kind of vector power tailstock formula unmanned plane as described in any one in claims 1 to 3, it is characterised in that：It is described
Empennage includes upper vertical fin (3) and the lower vertical fin (13) identical with upper vertical fin (3), and the upper vertical fin (3) and lower vertical fin (13) are respectively
It is placed in above and below fuselage (1) tail portion.
5. a kind of vector power tailstock formula unmanned plane as claimed in claim 4, it is characterised in that：The upper vertical fin (3) and under
The tail portion of vertical fin (13) is hinged with rudder (7).
6. a kind of vector power tailstock formula unmanned plane as claimed in claim 5, it is characterised in that：On the upper vertical fin (3) also
Equipped with empennage steering engine (8), the empennage steering engine (8) is equipped with rudder steering engine rocking arm (81), the rudder steering engine rocking arm
(81) it is connected on rudder (7) by rudder steering engine connecting rod (82).
7. a kind of vector power tailstock formula unmanned plane as claimed in claim 6, it is characterised in that：The aileron steering engine (9) sets
It puts in fixed seat (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721754641.1U CN207580174U (en) | 2017-12-15 | 2017-12-15 | A kind of vector power tailstock formula unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721754641.1U CN207580174U (en) | 2017-12-15 | 2017-12-15 | A kind of vector power tailstock formula unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207580174U true CN207580174U (en) | 2018-07-06 |
Family
ID=62738040
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721754641.1U Expired - Fee Related CN207580174U (en) | 2017-12-15 | 2017-12-15 | A kind of vector power tailstock formula unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207580174U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109229367A (en) * | 2018-10-30 | 2019-01-18 | 南京航空航天大学 | A kind of new configuration vertical take-off and landing drone and its flight control method |
| CN110466754A (en) * | 2019-09-09 | 2019-11-19 | 西安交通大学 | A kind of tailstock formula tilting rotor vertical take-off and landing drone |
-
2017
- 2017-12-15 CN CN201721754641.1U patent/CN207580174U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109229367A (en) * | 2018-10-30 | 2019-01-18 | 南京航空航天大学 | A kind of new configuration vertical take-off and landing drone and its flight control method |
| CN110466754A (en) * | 2019-09-09 | 2019-11-19 | 西安交通大学 | A kind of tailstock formula tilting rotor vertical take-off and landing drone |
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180706 Termination date: 20191215 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |