CN206577385U - A kind of remote control class dalta wing flight vector device - Google Patents
A kind of remote control class dalta wing flight vector device Download PDFInfo
- Publication number
- CN206577385U CN206577385U CN201720180890.8U CN201720180890U CN206577385U CN 206577385 U CN206577385 U CN 206577385U CN 201720180890 U CN201720180890 U CN 201720180890U CN 206577385 U CN206577385 U CN 206577385U
- Authority
- CN
- China
- Prior art keywords
- motor
- vector device
- steering wheel
- remote control
- dalta wing
- 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.)
- Active
Links
Abstract
The utility model discloses a kind of remote control class dalta wing flight vector device, the aircraft includes dalta wing fuselage (1), the motor rack (2) arranged along dalta wing fuselage (1) center line, positioned at the motor (5) of the motor rack (2) afterbody, steering wheel (6) in the middle part of the motor rack (2) and the vector device (3) between the steering wheel (6) and the motor (5), the steering wheel (6) controls the motor (5) to carry out vector motion by the vector device (3), the motor (5) is driven the propeller (9) of the aircraft.The utility model makes delta-wing aircraft more stablize and be easy to operation, is relatively beneficial to the popularization of model aeroplane sport.
Description
Technical field
The utility model is related to model airplane technical field, and in particular to a kind of remote control class dalta wing flight vector device.
Background technology
Model airplane, as the term suggests being a kind of recyclable model of imitative spacecraft shape fabricating, is under the jurisdiction of Aero-Space mould
Type, it is a kind of that delta-wing aircraft belongs to model airplane.
Publication No. CN201338727U Chinese patent literature discloses a kind of power aerial vehicle for having dalta wing, bag
Include：Cabin, its bottom is provided with landing wheel, and both sides, which are equipped with hatch, cabin, is provided with seat；Power drive unit, is arranged at machine
On rear side of cabin；Dalta wing, above the cabin, including an axis and the double-vane that deploys along formed symmetrical, dalta wing axis and machine
Connected between cabin by connecting bracket；Triangle control frame, including two vertical rods, a cross bar, two vertical rods are intersecting be fixedly connected on it is described
On the axis of dalta wing, cross bar passes through cabin from the hatch of cabin both sides, and cross bar two ends by before control wire and dalta wing,
Trailing edge is connected.The power aerial vehicle of the tool dalta wing can hold number people seating, and the design of cabin avoids passenger from being directly exposed to outside, increased
Strong security.When needing to take off, rear end propeller-driven aircraft advances, while adjusting dalta wing by triangle control frame
Windward angle, being provided for aircraft to buoyancy makes aircraft takeoff, and flight side is controlled by triangle control frame in flight
To and rise and fall.
Publication No. CN2446061U Chinese patent literature discloses one kind and can advanced along fixed cableway, safety system
The high delta-winged suspension aerobats of number, its delta-winged suspension aerobat body including skeleton, are provided with skeleton
At least one supplies in the cableway desludging device passed through by fixed cableway, cableway desludging device to be provided with top roller axle, bottom roller axle and side
Roll shaft；Counter weight device is provided with the bottom of aircraft；The utility model is moved along the cableway fixed, and at this moment aviator both has
The flying feel of common delta-winged suspension aerobat is manipulated, has and is required no before absolute safety guarantee, flight specially again
Training, men and women, old and young can use.
Existing remote control class delta-wing aircraft did not use the back of the body and pushes away vectoring technology.Existing remote control class dalta wing flight
Device all has that pitching is unstable, it is difficult to meet the demand of dalta wing remotely-piloted vehicle user.
Utility model content
The purpose of this utility model is to provide a kind of remote control class dalta wing flight vector device, in the flight of remote control class dalta wing
The back of the body is installed on device to push away vector device and can greatly strengthen the pitching stability of delta-wing aircraft, made on operator is more prone to
Hand is operated, and is that popularizing for remote control class model airplane makes a significant contribution.
To achieve the above object, the utility model discloses a kind of remote control class dalta wing flight vector device, the aircraft
Including dalta wing fuselage, along the motor rack of dalta wing fuselage center line arrangement, the motor positioned at the motor rack afterbody, it is located at
Steering wheel in the middle part of the motor rack and the vector device between the steering wheel and the motor, the steering wheel passes through described
Vector device controls the motor to carry out vector motion, and the motor is driven the propeller of the aircraft.
Optionally, the vector device passes sequentially through attachment means and steering wheel rocking arm is connected with the steering wheel, the connection
Device includes the center rod of the front and rear two Z-shaped bars set and the connection Z-shaped bar, and institute is passed through positioned at anterior Z-shaped bar
State steering wheel rocking arm with the steering wheel to be connected, the Z-shaped bar positioned at rear portion is connected with the vector device.
Optionally, the vector device includes central plate, the securing plate positioned at the central plate opposite sides, fixes described
The crossbeam and the connecting rod installing port positioned at the center front edge of board of central plate and securing plate, the connecting rod installing port with it is described
The Z-shaped bar at rear portion is connected, and the motor is fixed on the rear side of the central plate.
Optionally, the remote control class dalta wing flight vector device also includes controlling the motor operation speed electronic speed regulation
Device.
Optionally, it is cased with positioning tension sleeve on the outside of the vector device.
The utility model has the following advantages that：
The utility model is according to the characteristics of delta-wing aircraft, with reference to hydrodynamics, is on remote control class delta-wing aircraft
The back of the body is installed and pushes away vector device, aircraft can be allowed according to the line of pull of the requirement change of flight device at any time of operator, make dalta wing
Operation is more stablized and be easy to aircraft.The utility model makes delta-wing aircraft more stablize and be easy to operation, more has
Beneficial to the popularization of model aeroplane sport.
Brief description of the drawings
Fig. 1 is a kind of structural representation of embodiment of the utility model remote control class dalta wing flight vector device.
Fig. 2 is the utility model attachment means and a kind of structural representation of embodiment of steering wheel rocking arm.
Fig. 3 is the utility model attachment means and a kind of structural representation of embodiment of steering wheel rocking arm.
Fig. 4 be a kind of structural representation of embodiment of the utility model vector device (in Fig. 1 relative to flight
The rearview in direction).
Embodiment
Following examples are used to illustrate the utility model, but are not limited to scope of the present utility model.
As shown in figure 1, the utility model provides a kind of remote control class dalta wing flight vector device, the aircraft includes triangle
Wing fuselage 1, along the center line of dalta wing fuselage 1 arrange motor rack 2, the motor 5 positioned at the afterbody of motor rack 2, positioned at institute
The steering wheel 6 and the vector device 3 between the steering wheel 6 and the motor 5 at the middle part of motor rack 2 are stated, the steering wheel 6 passes through
The vector device 3 controls the motor 5 to carry out the horizontal vector motion perpendicular to heading, and the motor 5 is driven described
The propeller 9 of aircraft.The utility model is connected by vector device with steering wheel, meanwhile, set receiver 10 to receive remote control
Signal to control the direction of steering wheel, vector device then changes remote control class three by changing the direction of propeller output gas flow
The line of pull direction of angle blade aircraft, is delta-wing aircraft enhancing pitching stability.
Steering wheel is well-known to those skilled in the art, is the power resources of telecontrolled model control action, can be used for adjusting
Control a kind of embodiment such as figure in the direction of vector device 3 and then the direction of controlled motor, attachment means and steering wheel rocking arm
Shown in 2-3, the vector device 3 passes sequentially through attachment means 4 and steering wheel rocking arm 8 and is connected with the steering wheel 6, the attachment means
4 include the center rod 42 of the front and rear two Z-shaped bars 41 set and the connection Z-shaped bar 41, lead to positioned at anterior Z-shaped bar 41
Cross the steering wheel rocking arm 8 with the steering wheel 6 to be connected, the Z-shaped bar 41 positioned at rear portion is connected with the vector device 3.Steering wheel rocking arm 8
Swing drive center rod 42 to be swung with dynamic vector device 3, change aircraft line of pull direction.
Vector device is well-known to those skilled in the art, for the direction of regulation motor, it is carried out vector motion,
As shown in figure 3, so as to adjust aircraft traffic direction, as shown in figure 4, the vector device 3 is included perpendicular to the fuselage 1
Central plate 31, the securing plate 32 positioned at the opposite sides of central plate 31, the crossbeam of the fixed central plate 31 and securing plate 32
34 and the connecting rod installing port 33 positioned at the front end of central plate 31, the connecting rod installing port 33 and the Z-shaped bar 41 at the rear portion
It is connected, the motor 5 is fixed on the rear side of the crossbeam 34, the two ends of crossbeam 34 of the vector device 3 are solid by fixing axle 35
It is scheduled in the fixed seat 21 of motor rack 2 and can be moved between fixed seat 21.Z-shaped bar is connected tightly with vector device and steering wheel rocking arm
It is close, without diastema, it is easy to precisely operation.
A kind of embodiment, the remote control class dalta wing flight vector device also includes controlling the motor operation speed
Electron speed regulator 11.Electron speed regulator 11 is the control device of a controlled motor rotating speed.It is received according to receiver 10
Electric signal, change the size of powering quantity by controller and actuator.Can by electron speed regulator 11 and vector device
With controlled motor operation speed and direction simultaneously.Receiver 10 is well-known to those skilled in the art, in specifically may be referred to
State patent document CN103457620A.
As shown in figure 1, the outside of the vector device can also be cased with positioning tension sleeve 7.Positioning tension sleeve 7 is prevented
Vector device is connected device and pulls and fall apart.
Although above having made detailed description to the utility model with generality explanation and instantiation,
On the basis of the utility model, it can be made some modifications or improvements, this will be apparent to those skilled in the art.
Therefore, the these modifications or improvements on the basis of without departing from the utility model spirit, belong to the utility model requirement
The scope of protection.
Claims (5)
1. a kind of remote control class dalta wing flight vector device, it is characterised in that the aircraft includes dalta wing fuselage (1), along institute
State dalta wing fuselage (1) center line arrangement motor rack (2), the motor (5) positioned at the motor rack (2) afterbody, positioned at the electricity
Steering wheel (6) in the middle part of frame (2) and the vector device (3) between the steering wheel (6) and the motor (5), the rudder
Machine (6) controls the motor (5) moved perpendicular to the horizontal vector of heading by the vector device (3), described
Motor (5) is driven the propeller (9) of the aircraft.
2. remote control class dalta wing flight vector device according to claim 1, it is characterised in that the vector device (3) according to
Secondary to be connected by attachment means (4) and steering wheel rocking arm (8) with the steering wheel (6), the attachment means (4) include front and rear setting
Two Z-shaped bars (41) and the center rod (42) of the connection Z-shaped bar (41), positioned at anterior Z-shaped bar (41) by described
Steering wheel rocking arm (8) is connected with the steering wheel (6) transmission, and the Z-shaped bar (41) positioned at rear portion is connected with the vector device (3).
3. remote control class dalta wing flight vector device according to claim 2, it is characterised in that vector device (3) bag
Include the central plate (31) perpendicular to the fuselage (1), the securing plate (32) positioned at the central plate (31) opposite sides, fixed institute
State central plate (31) and the crossbeam (34) and the connecting rod installing port positioned at the central plate (31) front end of securing plate (32)
(33), the connecting rod installing port (33) is connected with the Z-shaped bar (41) at the rear portion, and the motor (5) is fixed on the crossbeam
(34) rear side, crossbeam (34) two ends of the vector device (3) are fixed on the fixed seat of motor rack (2) by fixing axle (35)
(21) it can move on and between fixed seat (21).
4. remote control class dalta wing flight vector device according to claim 1, it is characterised in that the remote control class dalta wing arrow
Measure the electron speed regulator (11) that aircraft also includes controlling the motor (5) to run speed.
5. the remote control class dalta wing flight vector device according to claim 1 or 3, it is characterised in that the vector device (3)
Outside be cased with positioning tension sleeve (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720180890.8U CN206577385U (en) | 2017-02-27 | 2017-02-27 | A kind of remote control class dalta wing flight vector device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720180890.8U CN206577385U (en) | 2017-02-27 | 2017-02-27 | A kind of remote control class dalta wing flight vector device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206577385U true CN206577385U (en) | 2017-10-24 |
Family
ID=60091720
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720180890.8U Active CN206577385U (en) | 2017-02-27 | 2017-02-27 | A kind of remote control class dalta wing flight vector device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206577385U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107970622A (en) * | 2017-12-29 | 2018-05-01 | 王子铭 | Remote-controlled model aircraft vector motor cabinet |
-
2017
- 2017-02-27 CN CN201720180890.8U patent/CN206577385U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107970622A (en) * | 2017-12-29 | 2018-05-01 | 王子铭 | Remote-controlled model aircraft vector motor cabinet |
| CN107970622B (en) * | 2017-12-29 | 2024-03-15 | 王子铭 | Remote control model plane vector motor base |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US3539133A (en) | Inherently stable tapered wing flaperon airplane | |
| US6554229B1 (en) | Aileron for fixed wing aircraft | |
| US20190291863A1 (en) | Vertical takeoff and landing aircraft with tilted-wing configurations | |
| CN106143898A (en) | A kind of VTOL tilting rotor fixed wing airplane | |
| CN109606672A (en) | Tilting rotor formula aircraft with the rear rotor that can be verted downwards | |
| US3659810A (en) | Inherently stable tapered wing flaperon airplane | |
| US3438597A (en) | Aircraft | |
| CN106394856A (en) | Composite wing unmanned aerial vehicle | |
| CN104816824A (en) | Fixed structure type vertical takeoff and landing aircraft based on dual-flight control system and control method for fixed structure type vertical takeoff and landing aircraft | |
| CN107416200B (en) | Electric composite wing aircraft | |
| CN207758993U (en) | The aerofoil system of unmanned plane | |
| WO2012068136A2 (en) | Mechanical control mixer and method therefor | |
| CN104276277A (en) | Fixed-wing propeller flying wing provided with front wing and capable of moving up and down vertically | |
| CN206577385U (en) | A kind of remote control class dalta wing flight vector device | |
| CN104787306A (en) | Low-speed safety aircraft capable of controlling flight attitude by aerodynamic force | |
| US9296478B2 (en) | Aircraft having at least two aircraft fuselages and a first wing arrangement with at least two wing sections that are not connected to each other | |
| CN202414162U (en) | Micro flapping-wing air vehicle with front horizontal swing and front vertical swing | |
| CN110466754A (en) | A kind of tailstock formula tilting rotor vertical take-off and landing drone | |
| US9038943B1 (en) | Safety aileron system | |
| CN110116802A (en) | A kind of big loading small-sized unmanned aircraft of high universalizable | |
| CN205256672U (en) | Manpower drive fixed -wing aircraft | |
| CN105775121A (en) | Wing-variable type unmanned aerial vehicle and method thereof | |
| CN204701764U (en) | Based on the fixed sturcture formula vertical take-off and landing aircraft (VTOL aircraft) of round trip flight Ore-controlling Role | |
| CN204473119U (en) | Lightweight unmanned plane | |
| US4121791A (en) | Aircraft built up from individual readily assembled and disassembled segments or components |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |