CN206561946U - The rotatable wing vertically taking off and landing flyer of multistage - Google Patents
The rotatable wing vertically taking off and landing flyer of multistage Download PDFInfo
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- CN206561946U CN206561946U CN201720221540.1U CN201720221540U CN206561946U CN 206561946 U CN206561946 U CN 206561946U CN 201720221540 U CN201720221540 U CN 201720221540U CN 206561946 U CN206561946 U CN 206561946U
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- wing
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- rotatable
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- landing flyer
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Abstract
The utility model provides a kind of rotatable wing vertically taking off and landing flyer of multistage, belongs to field of mechanical technique.It solves the problem of existing aircraft is poor for applicability.The rotatable wing vertically taking off and landing flyer of this multistage, including the internal body for cavity, there is power supply in described body, the body in strip and has empennage in the afterbody of body, the both sides at the middle part of body have symmetrically arranged wing, the wing includes connecting rod, outer wing, inner wing and propeller, above-mentioned connecting rod is connected with body and both are vertically arranged, above-mentioned outer wing and inner wing are connected on connecting rod and inner wing is close to body, being fixed with the outer wing and inner wing also has the Servo-controller being connected with outer wing and inner wing in propeller, described body.The rotatable wing vertically taking off and landing flyer applicability of this multistage is high.
Description
Technical field
The utility model belongs to field of mechanical technique, is related to a kind of rotatable wing vertically taking off and landing flyer of multistage.
Background technology
Helicopter can be hiked vertically, break away from dependence of the fixed wing aircraft to going to, but the cruising speed of helicopter
It is its fatal defects.Although fixed wing aircraft cruising speed is high, it is fatal that the requirement taken off when landing to place turns into its
Shortcoming.
The content of the invention
The purpose of this utility model is that there is provided a kind of higher many of applicability in view of the above-mentioned problems existing in the prior art
The rotatable wing vertically taking off and landing flyer of section.
The purpose of this utility model can be realized by following technical proposal：
Have in a kind of rotatable wing vertically taking off and landing flyer of multistage, including the internal body for cavity, described body
There is a power supply, the body in strip and has an empennage in the afterbody of body, the both sides at the middle part of body have symmetrically arranged
Wing, it is characterised in that the wing includes connecting rod, outer wing, inner wing and propeller, and above-mentioned connecting rod is connected with body and both hang down
Straight to set, above-mentioned outer wing and inner wing are connected on connecting rod and inner wing is close to body, and spiral shell is fixed with the outer wing and inner wing
Revolving also has the Servo-controller being connected with outer wing and inner wing in oar, described body.
This aircraft it is creative wing is divided into inner wing and outer wing, therefore, Servo-controller is passed through during vertical lift state
Inner wing and outer wing is all swung and put plumbness, aircraft, which can be stablized, to be lifted.
Risen to once aircraft after setting height, Servo-controller controls above-mentioned inner wing and outer wing to swing, make inner wing and
Outer wing is in horizontality.Now, aircraft can be advanced with cruise mode.
In the above-mentioned rotatable wing vertically taking off and landing flyer of multistage, described inner wing includes brshless DC motor, electricity
Sub- speed regulator, two Servo-controllers and a lifting rudder face, above-mentioned brshless DC motor, electron speed regulator and two servorudders
Machine is connected with power supply, and described electron speed regulator is used for the output speed for controlling brshless DC motor, above-mentioned propeller and nothing
Brushless motor is connected, and two Servo-controllers are used for the swing angle for controlling inner wing.
Brshless DC motor is used to control the propeller rotational on inner wing, and electron speed regulator is used to control turning for propeller
Speed.Two Servo-controllers are used for the swing position for controlling inner wing.
In the above-mentioned rotatable wing vertically taking off and landing flyer of multistage, the front portion of described inner wing is connected with propeller,
The rear portion of the inner wing is lifting rudder face in the form of sheets.
In the above-mentioned rotatable wing vertically taking off and landing flyer of multistage, described outer wing includes brshless DC motor, electricity
Sub- speed regulator, two Servo-controllers and a lifting rudder face, above-mentioned brshless DC motor, electron speed regulator and two servorudders
Machine is connected with power supply, and described electron speed regulator is used for the output speed for controlling brshless DC motor, above-mentioned propeller and nothing
Brushless motor is connected, and two Servo-controllers are used for the swing angle for controlling outer wing.
Brshless DC motor is used to control the propeller rotational on outer wing, and electron speed regulator is used to control turning for propeller
Speed.Two Servo-controllers are used for the swing position for controlling outer wing.
In the above-mentioned rotatable wing vertically taking off and landing flyer of multistage, the front portion of described outer wing is connected with propeller,
The rear portion of the outer wing is lifting rudder face in the form of sheets.
In the above-mentioned rotatable wing vertically taking off and landing flyer of multistage, the inner wing and outer wing are respectively provided with and a pair of one
Brshless DC motor, electron speed regulator, two Servo-controllers and the lifting rudder face answered.
Decline in order to stable, the inner wing on two wings can first overturn 180 degree and be in plumbness；Then, two machines
Outer wing on the wing is in plumbness in synchronously upset 180 degree.Stable uphill process is also similar process steps, herein no longer
Repeat.
Certainly, also there is processor in body, processor can receive external control signal, then turns the control signal
It is changed into controlling correspondence Servo-controller, the signal of machine governor action.
In the above-mentioned rotatable wing vertically taking off and landing flyer of multistage, described underpart has three supporting legs
Frame, one of support leg support is located at front part of a body, and two other support leg support is symmetrically connected to After-Body.
It can make this aircraft is stable to rise and fall by three support leg supports.
In the above-mentioned rotatable wing vertically taking off and landing flyer of multistage, described support leg support includes what is be connected with body
Leg bar and the roller being movably connected on leg bar.
In the above-mentioned rotatable wing vertically taking off and landing flyer of multistage, the body both sides are respectively provided with the connection of protrusion
Portion, inner wing, outer wing and the equal flush of connecting portion when aircraft is in average flight state.
The setting of connecting portion can be such that wing is seamlessly transitted with body junction.
In the above-mentioned rotatable wing vertically taking off and landing flyer of multistage, the rotation direction of the propeller of the body both sides
Conversely.
Such rotation direction can make stability of aircraft advance.
Compared with prior art, the positive technique effect that the utility model has has：Aircraft is by vertical lift state
When being changed to fixed-wing average flight state, it is segmented and is verted step by step by multi element wing, process control complexity of verting reduction is inclined
Roll angle during turning is successively by the aileron control of two sections of wings of the rotating speed control of two sections of inner side or so rotor, outside or so
System, step by step segmentation is verted, and can become model of flight transient process is gentle, control complexity reduction.
Brief description of the drawings
Fig. 1 is the dimensional structure diagram of the rotatable wing vertically taking off and landing flyer of this multistage.
Fig. 2 is the cross section structure diagram of the rotatable wing vertically taking off and landing flyer of this multistage.
In figure, 1, body；2nd, empennage；3rd, inner wing；4th, outer wing；5th, connecting rod；6th, propeller；7th, rudder face is lifted；8th, leg bar；9、
Roller.
Embodiment
As depicted in figs. 1 and 2, the rotatable wing vertically taking off and landing flyer of this multistage, including the internal body 1 for cavity,
There is power supply, the body 1 in strip and has empennage 2 in the afterbody of body 1, the middle part of body 1 in described body 1
Both sides have symmetrically arranged wing, and the wing includes connecting rod 5, outer wing 4, inner wing 3 and propeller 6, above-mentioned connecting rod 5 and body
1 be connected and both be vertically arranged, above-mentioned outer wing 4 and inner wing 3 are connected on connecting rod 5 and inner wing 3 is close to body 1, the outer wing 4
With being fixed with inner wing 3 also there is the Servo-controller being connected with outer wing 4 and inner wing 3 in propeller 6, described body 1.
Described inner wing 3 includes brshless DC motor, electron speed regulator, two Servo-controllers and a lifting rudder face,
Above-mentioned brshless DC motor, electron speed regulator and two Servo-controllers are connected with power supply, and described electron speed regulator is used to control
The output speed of brshless DC motor processed, above-mentioned propeller is connected with brshless DC motor, and two Servo-controllers are interior for controlling
The swing angle of the wing 3.
The front portion of described inner wing 3 is connected with propeller 6, and the rear portion of the inner wing 3 is lifting rudder face 7 in the form of sheets.
Described outer wing 4 includes brshless DC motor, electron speed regulator, two Servo-controllers and a lifting rudder face 7,
Above-mentioned brshless DC motor, electron speed regulator and two Servo-controllers are connected with power supply, and described electron speed regulator is used to control
The output speed of brshless DC motor processed, above-mentioned propeller is connected with brshless DC motor, and two Servo-controllers are outer for controlling
The swing angle of the wing 4.
The front portion of described outer wing 4 is connected with propeller 6, and the rear portion of the outer wing 6 is lifting rudder face 7 in the form of sheets.When
So, each outer wing 6 has and its one-to-one propeller 6 and lifting rudder face 7；Each inner wing 3 has and a pair of one
The propeller 6 and lifting rudder face 7. answered
The inner wing 3 and outer wing 4 are respectively provided with and its one-to-one brshless DC motor, electron speed regulator, two servos
Steering wheel and a lifting rudder face.
The described bottom of body 1 has three support leg supports, and it is anterior that one of support leg support is located at body 1, and in addition two
Individual support leg support is symmetrically connected to the rear portion of body 1.
Described support leg support includes the leg bar 8 being connected with body 1 and the roller 9 being movably connected on leg bar 8.
The both sides of body 1 are respectively provided with the connecting portion of protrusion, inner wing 3, outer wing 4 when aircraft is in average flight state
With the equal flush of connecting portion.
The rotation direction of the propeller of the both sides of body 1 is opposite.
This aircraft it is creative wing is divided into inner wing and outer wing, therefore, Servo-controller is passed through during vertical lift state
Inner wing and outer wing is all swung and put plumbness, aircraft, which can be stablized, to be lifted.
Risen to once aircraft after setting height, Servo-controller controls above-mentioned inner wing and outer wing to swing, make inner wing and
Outer wing is in horizontality.Now, aircraft can be advanced with cruise mode.
Claims (10)
1. have in a kind of rotatable wing vertically taking off and landing flyer of multistage, including the internal body for cavity, described body
Power supply, the body in strip and has empennage in the afterbody of body, and the both sides at the middle part of body have symmetrically arranged machine
The wing, it is characterised in that the wing includes connecting rod, outer wing, inner wing and propeller, and above-mentioned connecting rod is connected with body and both are vertical
Set, above-mentioned outer wing and inner wing are connected on connecting rod and inner wing is close to body, and spiral is fixed with the outer wing and inner wing
Also there is the Servo-controller being connected with outer wing and inner wing in oar, described body.
2. the rotatable wing vertically taking off and landing flyer of multistage according to claim 1, it is characterised in that described inner wing bag
Include brshless DC motor, electron speed regulator, two Servo-controllers and a lifting rudder face, above-mentioned brshless DC motor, electronics
Speed regulator and two Servo-controllers are connected with power supply, and described electron speed regulator is used to control the output of brshless DC motor to turn
Speed, above-mentioned propeller is connected with brshless DC motor, and two Servo-controllers are used for the swing angle for controlling inner wing.
3. the rotatable wing vertically taking off and landing flyer of multistage according to claim 2, it is characterised in that described inner wing
Front portion is connected with propeller, and the rear portion of the inner wing is lifting rudder face in the form of sheets.
4. the rotatable wing vertically taking off and landing flyer of multistage according to claim 3, it is characterised in that described outer wing bag
Include brshless DC motor, electron speed regulator, two Servo-controllers and a lifting rudder face, above-mentioned brshless DC motor, electronics
Speed regulator and two Servo-controllers are connected with power supply, and described electron speed regulator is used to control the output of brshless DC motor to turn
Speed, above-mentioned propeller is connected with brshless DC motor, and two Servo-controllers are used for the swing angle for controlling outer wing.
5. the rotatable wing vertically taking off and landing flyer of multistage according to claim 4, it is characterised in that described outer wing
Front portion is connected with propeller, and the rear portion of the outer wing is lifting rudder face in the form of sheets.
6. the rotatable wing vertically taking off and landing flyer of multistage according to claim 5, it is characterised in that the inner wing and outer
The wing is respectively provided with and its one-to-one brshless DC motor, electron speed regulator, two Servo-controllers and a lifting rudder face.
7. the rotatable wing vertically taking off and landing flyer of multistage according to claim 1, it is characterised in that under described body
Portion has three support leg supports, and one of support leg support is located at front part of a body, and two other support leg support is symmetrically connected to
After-Body.
8. the rotatable wing vertically taking off and landing flyer of multistage according to claim 7, it is characterised in that described supporting leg
Frame includes the leg bar being connected with body and the roller being movably connected on leg bar.
9. the rotatable wing vertically taking off and landing flyer of multistage according to claim 5, it is characterised in that the body both sides
The connecting portion of protrusion is respectively provided with, inner wing, outer wing and the equal flush of connecting portion when aircraft is in average flight state.
10. the rotatable wing vertically taking off and landing flyer of multistage according to claim 5, it is characterised in that the body two
The rotation direction of the propeller of side is opposite.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720221540.1U CN206561946U (en) | 2017-03-08 | 2017-03-08 | The rotatable wing vertically taking off and landing flyer of multistage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720221540.1U CN206561946U (en) | 2017-03-08 | 2017-03-08 | The rotatable wing vertically taking off and landing flyer of multistage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206561946U true CN206561946U (en) | 2017-10-17 |
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ID=60030799
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720221540.1U Active CN206561946U (en) | 2017-03-08 | 2017-03-08 | The rotatable wing vertically taking off and landing flyer of multistage |
Country Status (1)
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106965928A (en) * | 2017-03-08 | 2017-07-21 | 贾杰 | The rotatable wing vertically taking off and landing flyer of multistage |
| WO2022082962A1 (en) * | 2020-10-21 | 2022-04-28 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Aircraft propulsion system |
| CN116215852A (en) * | 2023-05-08 | 2023-06-06 | 成都沃飞天驭科技有限公司 | Vertical take-off and landing aircraft and control method thereof |
-
2017
- 2017-03-08 CN CN201720221540.1U patent/CN206561946U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106965928A (en) * | 2017-03-08 | 2017-07-21 | 贾杰 | The rotatable wing vertically taking off and landing flyer of multistage |
| WO2022082962A1 (en) * | 2020-10-21 | 2022-04-28 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Aircraft propulsion system |
| EP4023557A4 (en) * | 2020-10-21 | 2022-11-23 | Comac Beijing Aircraft Technology Research Institute | Aircraft propulsion system |
| CN116215852A (en) * | 2023-05-08 | 2023-06-06 | 成都沃飞天驭科技有限公司 | Vertical take-off and landing aircraft and control method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20200117 Address after: 311121 Room 401, Building 9, 1818-2 Wenyi West Road, Yuhang Street, Hangzhou City, Zhejiang Province Patentee after: Hangzhou Ruijie Intelligent Air Robot Technology Co., Ltd. Address before: 330000 Jiangxi Province, Nanchang Honggutan Feng and South Road No. 696 Building 2 Room 202 Patentee before: Jia Jie |