CN206050074U - VTOL Fixed Wing AirVehicle - Google Patents
VTOL Fixed Wing AirVehicle Download PDFInfo
- Publication number
- CN206050074U CN206050074U CN201621064731.3U CN201621064731U CN206050074U CN 206050074 U CN206050074 U CN 206050074U CN 201621064731 U CN201621064731 U CN 201621064731U CN 206050074 U CN206050074 U CN 206050074U
- Authority
- CN
- China
- Prior art keywords
- wing
- port
- starboard
- aileron
- fuselage
- 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.)
- Expired - Fee Related
Links
Abstract
This utility model is related to a kind of VTOL Fixed Wing AirVehicle, and which includes：Fuselage, the port wing for being respectively arranged in fuselage opposite sides, starboard wing, the empennage for being installed on fuselage tail end.Fuselage is provided with an image recorder, image recorder is located at the front end of fuselage, port wing is provided with a left-hand airscrew and port aileron, left-hand airscrew is located at the front end of port wing, port aileron is located at the rear end of port wing, and starboard wing is provided with a right-hand screw oar and starboard aileron, and right-hand screw oar is located at the front end of starboard wing, starboard aileron is located at the rear end of starboard wing, and empennage extends to the both sides up and down of fuselage.Above VTOL Fixed Wing AirVehicle can realize VTOL in different places, it is not necessary to duty runway, and place is limited little, is the flat winged state of fixed-wing, can grow boat and use after taking off, very useful.
Description
Technical field
This utility model is related to vehicle technology field, more particularly to a kind of VTOL Fixed Wing AirVehicle.
Background technology
With the continuous development of society, the continuous improvement of the living standard of people, aircraft are risen in daily life
Irreplaceable effect is arrived, quickly transmission etc. is obtained for application in investigation, aerial survey, forest protection, small-sized emergency article.Pass
The aircraft of system is gone straight up to for rotary wings and is taken off and two kinds of fixed-wing horizontal take-off, and the requirement to place that rotary wings take off vertically is not
Height, but the voyage navigated by water is shorter, it is impossible to the longer requirement of voyage is completed, and fixed-wing horizontal take-off needs longer runway to slide
OK, to be taken off and limited larger by place.
Utility model content
Based on this, it is necessary to for the problem that traditional aircraft is present, there is provided a kind of place be limited it is little, hanging down for boat can be grown
Straight landing Fixed Wing AirVehicle.
A kind of VTOL Fixed Wing AirVehicle, including：Fuselage, the left machine for being respectively arranged in the fuselage left and right sides
The wing, starboard wing, the empennage for being installed on the fuselage tail end, the fuselage are provided with an image recorder, the image recorder position
In the front end of the fuselage；The port wing is provided with a left-hand airscrew and port aileron, and the left-hand airscrew is located at the port wing
Front end, the port aileron be located at the port wing rear end；The starboard wing is provided with a right-hand screw oar and starboard aileron, the right side
Propeller is located at the front end of the starboard wing, and the starboard aileron is located at the rear end of the starboard wing, and the empennage is to the fuselage
Both sides up and down extend.
Wherein in one embodiment, the port wing is additionally provided with a left motor, left rudder machine, left drive rod, the left electricity
Machine is connected the driving left-hand airscrew rotation with the left-hand airscrew, and the left rudder machine is located in the middle of the port wing by described
Left drive rod is connected with the port aileron；The starboard wing is additionally provided with a right motor, right standard rudder machine, right drive rod, the right motor
It is connected the driving right-hand screw oar rotation with the right-hand screw oar, the right standard rudder machine is located in the middle of the starboard wing and passes through the right side
Drive rod is connected with the starboard aileron.
Wherein in one embodiment, the fuselage is additionally provided with a glass cover, cover and two blow vents, the glass cover position
Relative with the image recorder in the front end of the fuselage, the cover is located at the top surface of the fuselage, the blow vent point
Not Wei Yu the image recorder both sides.
Wherein in one embodiment, the fuselage is additionally provided with a touch pole, and the touch pole is used to control the cover
Locked state.
Wherein in one embodiment, the port aileron, starboard aileron be rectangle, the port aileron, the thickness of starboard aileron
It is gradually reduced from front end to the back-end.
Wherein in one embodiment, the port aileron, starboard aileron can swing up and down.
Above-mentioned VTOL Fixed Wing AirVehicle, constitutes major architectural by fuselage, port wing, starboard wing and empennage, uses
When, port wing, starboard wing and empennage define a corner base bracing frame, and whole VTOL Fixed Wing AirVehicle can lead to
Cross the base bracing frame to be placed in ground or other support platforms.Left-hand airscrew, right-hand screw oar quickly rotate offer afterwards
, so as to complete to take off, the VTOL can be by adjusting port aileron, starboard aileron conversion after fixing aircraft takeoff for one climbing power
To level flight condition, it is also possible to be transformed into vertical landing state from level flight condition.The VTOL Fixed Wing AirVehicle
VTOL can be realized in different places, it is not necessary to duty runway, place is limited little, is the flat winged state of fixed-wing after taking off,
Boat can be grown to use, it is very useful.
Description of the drawings
Schematic diagrams of the Fig. 1 for one preferred embodiment VTOL Fixed Wing AirVehicle of this utility model；
Schematic diagrams of the Fig. 2 for another visual angle of VTOL Fixed Wing AirVehicle shown in Fig. 1；
Fig. 3 is the schematic diagram that VTOL Fixed Wing AirVehicle shown in Fig. 1 lacks glass cover；
Fig. 4 is the enlarged diagram at A in VTOL Fixed Wing AirVehicle shown in Fig. 3；
Accompanying drawing marks explanation：
10- VTOL Fixed Wing AirVehicles, 20- fuselages, 21- affect monitor, 22- glass covers, 23- covers, 24- to lead to
QI KOU, 25- touch poles, 30- port wings, 31- left-hand airscrews, 32- port ailerons, the left motors of 33-, 34- left rudder machines, the left drivings of 35-
Bar, 40- starboard wings, 41- right-hand screw oars, 42- starboard ailerons, the right motors of 43-, 44- right standard rudder machines, the right drive rods of 45-, 50- empennages.
Specific embodiment
For the ease of understanding this utility model, this utility model is more fully retouched below with reference to relevant drawings
State.Preferred embodiment of the present utility model is given in accompanying drawing.But, this utility model can come real in many different forms
It is existing, however it is not limited to embodiment described herein.On the contrary, the purpose for providing these embodiments is made to public affairs of the present utility model
The understanding for opening content is more thorough comprehensive.
It should be noted that when element is referred to as " being fixed on " another element, it can directly on another element
Or can also there is element placed in the middle.When an element is considered as " connection " another element, it can be directly connected to
To another element or may be simultaneously present centering elements.
Unless otherwise defined, all of technology used herein and scientific terminology are led with technology of the present utility model is belonged to
The implication that the technical staff in domain is generally understood that is identical.In term used in the description of the present utility model it is simply herein
The purpose of description specific embodiment, it is not intended that in limiting this utility model.
Fig. 1 to Fig. 3 is refer to, is the VTOL Fixed Wing AirVehicle 10 of one preferred embodiment of this utility model, this hangs down
Straight landing Fixed Wing AirVehicle 10 include fuselage 20, the port wing 30 for being respectively arranged in 20 opposite sides of fuselage, starboard wing 40, and
The empennage 50 of 20 tail end of fuselage is installed on, empennage 50 extends to the both sides up and down of fuselage 20.During use, in takeoff and landing state
The base bracing frame that port wing 30, starboard wing 40 and empennage 50 are formed is used to support whole VTOL Fixed Wing AirVehicle 10,
In flat winged state, port wing 30, starboard wing 40, empennage 50 play a part of to be oriented to and split air-flow.
Fuselage 20 has an image recorder 21, glass cover 22, cover 23, touch pole 25 and two blow vents 24, image
Monitor 21 is located at the front end of fuselage 20, and the front end that glass cover 22 is located at fuselage 20 is relative with image recorder 21, and image is remembered
Record instrument 21 plays a protective role, and also allows for the projection identification record of image recorder 21.Cover 23 is located at the top surface and machine of fuselage 20
Body 20 is hinged, and respectively positioned at the both sides of image recorder 21, touch pole 25 is located at one end of cover 23 to blow vent 24, for controlling
The locked state of cover 23, above-mentioned cover 23 play a protective role to each part inside fuselage 20, and maintainer can pass through
The each part for opening 23 pairs of the insides of cover is keeped in repair, and blow vent 24 is easy to airflow, and each part inside fuselage 20 is entered
Row cooling.
Port wing 30 has a left-hand airscrew 31, port aileron 32, left motor 33, left rudder machine 34 and left drive rod 35, left spiral shell
Rotation oar 31 is connected with left motor 33 positioned at the front end of port wing 30, and left motor 33 is used to drive left-hand airscrew 31 to rotate so as to provide
Power.The rear end that port aileron 32 is located at port wing 30 is relative with left motor 33, and left rudder machine 34 is located at the centre of port wing 30, ascends the throne
Between left motor 33, port aileron 32, left rudder machine 34 is connected with port aileron 32 by left drive rod 35.Port aileron 32 is rectangle
And its thickness is gradually reduced to the back-end from front end, during use, drives left drive rod 35 so as to drive port aileron by left rudder machine 34
32 swing up and down, and the state of flight of VTOL Fixed Wing AirVehicle 10 is adjusted, the pendulum angle model of the port aileron 32
Enclose for 0 °～90 °.
Starboard wing 40 is provided with a right-hand screw oar 41, starboard aileron 42, right motor 43, right standard rudder machine 44 and right drive rod 45, right spiral shell
Rotation oar 41 is connected with right motor 43 positioned at the front end of starboard wing 40, and right motor 43 is used to drive right-hand screw oar 41 to rotate so as to provide
Power.The rear end that starboard aileron 42 is located at starboard wing 40 is relative with right motor 43, and right standard rudder machine 44 is located at the centre of starboard wing 40, ascends the throne
Between right motor 43, starboard aileron 42, right standard rudder machine 44 is connected with starboard aileron 42 by right drive rod 45.Starboard aileron 42 is rectangle
And its thickness is gradually reduced to the back-end from front end, during use, drives right drive rod 45 so as to drive starboard aileron by right standard rudder machine 44
42 swing up and down, and the state of flight of VTOL Fixed Wing AirVehicle 10 is adjusted, the pendulum angle model of the starboard aileron 32
Enclose for 0 °～90 °.
The run action that all parts in different flight state of aircraft 10 are fixed in the VTOL is as follows:Take off vertically
Pattern, during use, VTOL Fixed Wing AirVehicle 10 is first vertically placed, and restarts left motor 33, right motor 43, port aileron
32nd, starboard aileron 42 does not swing and is in same plane with port wing 30, starboard wing 40 respectively.Now, VTOL fixed-wing flight
Device 10 is subject to the climbing power that the high speed rotation of left-hand airscrew 31, right-hand screw oar 41 is provided to start to take off, and VTOL fixed-wing flies
Row device 10 vertically climb speed and height is by controlling the rotating speed of left motor 33, right motor 43 controlling.It is vertical to turn flat
Winged pattern, during VTOL Fixed Wing AirVehicle 10 vertically climbs, starts left rudder machine 34, right standard rudder machine 44 control left secondary
The wing 32, starboard aileron 42 are subject to air flow impulse, afterbody to be subject to oblique to lower swing certain angle, now port aileron 32, starboard aileron 42
On pulling force, change over time, VTOL Fixed Wing AirVehicle 10 is just changed into flat winged state from the state of taking off vertically.It is flat
Winged pattern, port aileron 32, starboard aileron 42 are not swung respectively with port wing 30, starboard wing 40 in same plane, and VTOL is solid
Determining rotor aircraft 10 keeps flat winged state, flight speed to pass through left motor 33, right electricity under left motor 33, the drive of right motor 43
43 synchronous rotational speed of machine is provided, when needing to carry out left and right turn, can be by controlling the rotating speed of left motor 33, right motor 43 come complete
Into.The rotating speed of left motor 33 carries out right-hand rotation control when being more than the rotating speed of right motor 43, the rotating speed of right motor 43 is more than left motor 33
Rotating speed when carry out left-hand rotation control.Flat to fly to turn vertical mode, VTOL Fixed Wing AirVehicle 10 is by increasing left motor 33, the right side
The rotating speed of motor 43 controls port aileron 32, starboard aileron 42 simultaneously and is swung up certain angle, and now port aileron 32, starboard aileron 42 are received
To air flow impulse, afterbody is subject to downward pressure, so as to change direction.Vertical landing pattern, a left side for VTOL fixed-wing 10
Aileron 32, starboard aileron 42 do not swung respectively with port wing 30, starboard wing 40 in same plane, left motor 33, right motor 43
Rotating speed reduces so that left-hand airscrew 31 and the rotation of right-hand screw oar 41 bring pulling force and VTOL Fixed Wing AirVehicle 10 from
Heavy sensation of the body power is equal or slightly less than, and now VTOL Fixed Wing AirVehicle 10 just can be with stable landing.
Above-mentioned VTOL Fixed Wing AirVehicle 10, is made up of mainly fuselage 20, port wing 30, starboard wing 40 and empennage 50
Framework, during use, port wing 30, starboard wing 40 and empennage 50 define a corner base bracing frame, and whole VTOL is solid
Determine rotor aircraft 10 to be placed on ground or other support platforms by the base bracing frame.Afterwards left-hand airscrew 31,
The 41 quick rotation of right-hand screw oar provides a climbing power so as to complete to take off, and the VTOL is fixed after aircraft 10 takes off and can be led to
Overregulate port aileron 32, starboard aileron 42 and be transformed into level flight condition, it is also possible to vertical landing is transformed into from level flight condition
State.The VTOL Fixed Wing AirVehicle 10 can realize VTOL in different places, it is not necessary to which duty runway, place are received
Limit is little, in the flat winged state of fixed-wing after taking off, can grow boat and use, very useful.
Each technical characteristic of embodiment described above arbitrarily can be combined, to make description succinct, not to above-mentioned reality
Apply all possible combination of each technical characteristic in example to be all described, as long as however, the combination of these technical characteristics is not deposited
In contradiction, the scope of this specification record is all considered to be.
Embodiment described above only expresses several embodiments of the present utility model, and its description is more concrete and detailed,
But therefore can not be interpreted as the restriction to utility model patent scope.It should be pointed out that for the common skill of this area
For art personnel, without departing from the concept of the premise utility, some deformations and improvement can also be made, these belong to
Protection domain of the present utility model.Therefore, the protection domain of this utility model patent should be defined by claims.
Claims (6)
1. a kind of VTOL Fixed Wing AirVehicle, including：Fuselage, the port wing for being respectively arranged in the fuselage opposite sides,
Starboard wing and it is installed on the empennage of the fuselage tail end, it is characterised in that the fuselage is provided with an image recorder, the shadow
As monitor is located at the front end of the fuselage；The port wing is provided with a left-hand airscrew and port aileron, and the left-hand airscrew is located at
The front end of the port wing, the port aileron are located at the rear end of the port wing；The starboard wing is provided with a right-hand screw oar and the right side
Aileron, the right-hand screw oar are located at the front end of the starboard wing, and the starboard aileron is located at the rear end of the starboard wing, the empennage
Extend to the both sides up and down of the fuselage.
2. VTOL Fixed Wing AirVehicle according to claim 1, it is characterised in that it is left that the port wing is additionally provided with
Motor, left rudder machine, left drive rod, the left motor are connected the driving left-hand airscrew rotation, the left side with the left-hand airscrew
Steering wheel is located in the middle of the port wing and is connected with the port aileron by the left drive rod；The starboard wing is additionally provided with a right electricity
Machine, right standard rudder machine, right drive rod, the right motor are connected the driving right-hand screw oar rotation, the right standard rudder with the right-hand screw oar
Machine is located in the middle of the starboard wing and is connected with the starboard aileron by the right drive rod.
3. VTOL Fixed Wing AirVehicle according to claim 1, it is characterised in that the fuselage is additionally provided with a glass
Lid, cover and two blow vents, the front end that the glass cover is located at the fuselage are relative with the image recorder, the cover position
In the top surface of the fuselage, the blow vent is respectively positioned at the both sides of the image recorder.
4. VTOL Fixed Wing AirVehicle according to claim 3, it is characterised in that the fuselage is additionally provided with a shake-up
Bar, the touch pole are used for the locked state for controlling the cover.
5. VTOL Fixed Wing AirVehicle according to claim 1, it is characterised in that the port aileron, starboard aileron are
Rectangle, the port aileron, the thickness of starboard aileron are gradually reduced to the back-end from front end.
6. VTOL Fixed Wing AirVehicle according to claim 5, it is characterised in that the port aileron, starboard aileron can
Swing up and down.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621064731.3U CN206050074U (en) | 2016-09-19 | 2016-09-19 | VTOL Fixed Wing AirVehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621064731.3U CN206050074U (en) | 2016-09-19 | 2016-09-19 | VTOL Fixed Wing AirVehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206050074U true CN206050074U (en) | 2017-03-29 |
Family
ID=58370563
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621064731.3U Expired - Fee Related CN206050074U (en) | 2016-09-19 | 2016-09-19 | VTOL Fixed Wing AirVehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206050074U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107315420A (en) * | 2017-07-01 | 2017-11-03 | 山东翔鸿电子科技有限公司 | A kind of unmanned plane turning method |
| CN107985589A (en) * | 2017-10-18 | 2018-05-04 | 沈阳航空航天大学 | Vertical take-off and landing drone with vectored thrust duct engine |
| CN108750103A (en) * | 2018-06-14 | 2018-11-06 | 广东伟力智能科技有限公司 | A kind of aircraft that vertical height-lock control and horizontal height-lock control can be achieved |
| CN108854104A (en) * | 2017-05-11 | 2018-11-23 | 王贺 | The air bag fixed-wing model of an airplane |
-
2016
- 2016-09-19 CN CN201621064731.3U patent/CN206050074U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108854104A (en) * | 2017-05-11 | 2018-11-23 | 王贺 | The air bag fixed-wing model of an airplane |
| CN107315420A (en) * | 2017-07-01 | 2017-11-03 | 山东翔鸿电子科技有限公司 | A kind of unmanned plane turning method |
| CN107985589A (en) * | 2017-10-18 | 2018-05-04 | 沈阳航空航天大学 | Vertical take-off and landing drone with vectored thrust duct engine |
| CN107985589B (en) * | 2017-10-18 | 2022-02-01 | 沈阳航空航天大学 | Take VTOL unmanned aerial vehicle of vector thrust duct engine |
| CN108750103A (en) * | 2018-06-14 | 2018-11-06 | 广东伟力智能科技有限公司 | A kind of aircraft that vertical height-lock control and horizontal height-lock control can be achieved |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206050074U (en) | VTOL Fixed Wing AirVehicle | |
| CN206125423U (en) | VTOL fixed wing uavs with power device verts | |
| CN105691613A (en) | Unmanned aerial vehicle ascending and descending smoothly and control method | |
| CN106043696A (en) | Flying system for unmanned aerial vehicle | |
| CN205150238U (en) | Unmanned aerial vehicle | |
| CN207417149U (en) | A kind of double lift culvert vertical take-off and landing aircrafts based on tilting duct | |
| CN205076045U (en) | Combined type aircraft of varistructure | |
| CN208134611U (en) | A kind of DCB Specimen bionic Aircraft | |
| CN107963209A (en) | Tandem wing tilting rotor wing unmanned aerial vehicle | |
| CN214566145U (en) | Fixed wing unmanned aerial vehicle with VTOL and hover function | |
| CN105129088B (en) | Spherical uniaxial rudder oriented intelligent aircraft | |
| CN111959819B (en) | Multi-rotor unmanned aerial vehicle algorithm verification and parameter adjustment system and use method thereof | |
| CN107323660A (en) | A kind of VTOL method of dalta wing unmanned plane | |
| CN204548497U (en) | A kind of many rotor flight devices | |
| CN210391552U (en) | Vertical take-off and landing fixed wing unmanned aerial vehicle | |
| CN108583867B (en) | Torque self-balancing three-duct fan bionic aircraft | |
| CN109911185A (en) | A kind of high speed single rotor helicopter without tail surface | |
| CN209176908U (en) | A kind of rotor fixed-wing unmanned plane of composite drive | |
| CN107444632A (en) | It is a kind of can VTOL dalta wing unmanned plane | |
| CN207523932U (en) | Tandem wing tilting rotor wing unmanned aerial vehicle | |
| CN202219839U (en) | Omnidirectional flight wing structure of vertically taking-off and landing aircraft | |
| CN206031774U (en) | Wing reaches decides wing machine | |
| CN213168535U (en) | Can accomodate VTOL unmanned aerial vehicle of screw | |
| CN205602092U (en) | Duct formula unmanned aerial vehicle | |
| CN104229130A (en) | Four-rotor wing unmanned aerial vehicle with pneumatic structure |
Legal Events
| 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: 20170329 Termination date: 20170919 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |