CN203916079U - Have the fixed wing aircraft toy of helicopter function concurrently - Google Patents
Have the fixed wing aircraft toy of helicopter function concurrently Download PDFInfo
- Publication number
- CN203916079U CN203916079U CN201420258078.9U CN201420258078U CN203916079U CN 203916079 U CN203916079 U CN 203916079U CN 201420258078 U CN201420258078 U CN 201420258078U CN 203916079 U CN203916079 U CN 203916079U
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- China
- Prior art keywords
- fuselage
- screw
- rotating shaft
- steering wheel
- tailplane
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- Expired - Fee Related
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- 230000007423 decrease Effects 0.000 description 7
- 230000009194 climbing Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
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Abstract
A kind of fixed wing aircraft toy that has helicopter function concurrently, comprise fuselage, the left and right sides of fuselage is installed with fixedly main wing, the rear portion of fuselage is provided with tailplane, the front end of fuselage is provided with screw, the rotating shaft of screw extends longitudinally, the rotating shaft of screw is driven by main motor, the quantity of described screw is two pairs, and two pairs of screws are arranged as context, the direction of rotation of screw under main motor drives, before the rotating shaft of screw overlap and in the rotating shaft of screw in the back, form coaxial relation; Described tailplane is arranged on afterbody swingably, and the rotating shaft left and right of tailplane is laterally extending, and the first steering wheel is also installed in fuselage, and the first steering wheel is connected and driven tailplane to swing by the first pull bar.The utility model can either carry out gliding flight as fixed wing aircraft, the action style that can carry out again vertical lifting as helicopter, vertically declines or hover.
Description
Technical field
The utility model belongs to the technical field of flying toy, relates in particular to a kind of fixed wing aircraft toy that has helicopter function concurrently.
Background technology
Fixed wing aircraft toy is installed with fixedly main wing in the left and right sides of fuselage, front end at fuselage is provided with screw, the rotating shaft of screw extends longitudinally, when screw is under driven by motor during high speed rotating, produce pulling force forward, make fuselage high-speed motion forward, then air-flow high velocity stream cross fixing main wing and produce the lift that overcomes fuselage deadweight, realize thus rise or decline, flat flying.From above-mentioned, existing fixed wing aircraft toy only, carrying out when high speed moves horizontally producing lift, that is to say, existing fixed wing aircraft toy can not have and is similar to helicopter vertical lifting, vertically declines or the function of hovering.
Utility model content
The purpose of this utility model is to overcome above-mentioned shortcoming and a kind of fixed wing aircraft toy that has helicopter function concurrently is provided, it can either carry out gliding flight as fixed wing aircraft, the action style that can carry out again vertical lifting as helicopter, vertically declines or hover.
Its object can realize by following scheme: this have concurrently helicopter function fixed wing aircraft toy comprise fuselage, the left and right sides of fuselage is installed with fixedly main wing, the rear portion of fuselage is provided with tailplane, the front end of fuselage is provided with screw, the rotating shaft of screw extends longitudinally, the rotating shaft of screw is driven by main motor, it is characterized in that, the quantity of described screw is two pairs, and two pairs of screws are arranged as context, the direction of rotation of screw under main motor drives, the rotating shaft of screw is above overlapped and in the rotating shaft of screw in the back, is formed coaxial relation, described tailplane is arranged on afterbody swingably, and the rotating shaft left and right of tailplane is laterally extending, and the first steering wheel is also installed in fuselage, and the first steering wheel is connected and driven tailplane to swing by the first pull bar.
Fuselage is also provided with gyroscope and microprocessor, and gyroscope connects microprocessor by holding wire, and microprocessor connects the control circuit of described main motor, the control circuit of the first steering wheel by holding wire.
The rear portion of fuselage is also rotatably mounted with vertical empennage, and vertically the rotating shaft of empennage is vertically extended, and the second steering wheel is also installed in fuselage, and the second steering wheel is connected and driven vertical empennage by the second pull bar; Microprocessor connects the control circuit of described the second steering wheel by holding wire.
The utlity model has following advantage and effect:
One, two pairs of screws of the present utility model not only can drive fuselage horizontal flight as the common fixed wing aircraft, and can drive fuselage as the helicopter vertical lifting, vertically decline, hovering, strengthen interesting.
Two,, when being fixed the flight of wing pattern, as long as by the upper and lower beat of the first steering wheel level of control empennage, just can realizing fuselage and upwards climb, dive downwards.When carrying out horizontal flight, as long as control vertical empennage beat by the second steering wheel, just can realize left-hand rotation, the right-hand rotation of fuselage.
Three, due to two pairs of screws, be set to the structure of coaxial double-oar, therefore can only by a main motor, be driven, reduce the quantity of main motor, thereby significantly alleviate complete machine weight.
Accompanying drawing explanation
Fig. 1 is the perspective view of the plane toy of a kind of specific embodiment of the utility model.
Fig. 2 is the plan structure schematic diagram of plane toy shown in Fig. 1.
Fig. 3 is the side-looking structural representation of plane toy shown in Fig. 1.
Fig. 4 is the local structure for amplifying schematic diagram of the front end of plane toy shown in Fig. 3.
The specific embodiment
Shown in Fig. 1, Fig. 2, Fig. 3, Fig. 4, this have concurrently helicopter function fixed wing aircraft toy comprise fuselage 6, the left and right sides of fuselage 6 is installed with fixedly main wing 61, the front end of fuselage 6 is provided with two pairs of screws 1,2, and two pairs of screws 1,2 are arranged as context, the rotating shaft 20 of screw 2 is hollow shaft below, before the rotating shaft 10 of screw 1 overlap and in the rotating shaft 20 of screw 2 in the back, form coaxial relation; The rotating shaft 10,20 of two screws extends longitudinally, the rotating shaft 10,20 of two screws is driven by same main motor 5, this main motor 5 drives respectively the rotating shaft 10,20 of two screws to rotate by different gear train assemblies, and make their direction of rotation, the therefore two pairs of screws 1,2 direction of rotation under main motor 5 drives.The rear portion of fuselage 6 is provided with tailplane 62, vertical empennage 63 swingably, the rotating shaft of tailplane 62 (as shown in AB in Fig. 2) left and right is laterally extending, the first steering wheel 31, the first steering wheels 31 are also installed in fuselage to be connected and is driven tailplane 62 to swing by the first pull bar 41.Vertically the rotating shaft (as shown in CD in Fig. 3) of empennage 63, along vertically extending, is also provided with the second steering wheel 32, the second steering wheels 32 and is connected and driven vertical empennage 63 to swing by the second pull bar 42 in fuselage.
Fuselage is also provided with gyroscope and microprocessor, and gyroscope connects microprocessor by holding wire, and microprocessor connects the control circuit of described main motor, the control circuit of the control circuit of the first steering wheel, the second steering wheel by holding wire..
The fixed wing aircraft toy of above-described embodiment can have following multiple flight function:
One, be similar to the flight function of fixed wing aircraft:
Standard of fuselage is placed.Make main motor 5 drive before and after two pairs of screw 1,2 high speed rotating, make two pairs of screws 1,2 produce pulling force forward, just can make fuselage high-speed mobile forward, the air-flow high velocity stream fixedly main wing 61 and then produce to climbing power of both sides of coming, realizes and rises or decline, put down and fly.When needs are turned, only need to control vertical empennage 63 beat to the left or to the right by the second steering wheel 32, just can realize left-hand rotation, the right-hand rotation of fuselage.As long as by the first steering wheel 31 level of control empennages beat 62 Shang Xia, just can realize upwards the climbing of fuselage, underriding downwards.
Two, be similar to the vertical lifting of helicopter, vertical decline, hovering function:
When needs carry out vertical lifting, vertical decline, during hovering, first by the first steering wheel 31 level of control empennages 62, swing, the elevation angle of fuselage is constantly increased, when the elevation angle of fuselage increases to, approach or equal 90 while spending, the central axis of fuselage close to or in plumbness, gyroscope detects this attitude of fuselage and notifies microprocessor, microprocessor instructs the first steering wheel 31 level of control empennage 62 backswings, make tailplane place plane parallel with the central axis of fuselage, and the pulling force of two pairs of screw high speed rotating generations becomes vertical force, at this moment just can by the order of remote controller, make plane toy realize vertical lifting, vertical decline, the function of hovering.For example, when this screw produces vertical force and complete machine and is equal in weight, plane toy is the floating state in not rising and also not declining just, and because screw 1 above equates with torque that screw 2 both high speed rotating produce below, opposite direction, cancel each other, so fuselage 6 can be around its central axis twisting; The in the situation that of hovering or vertical decline, if strengthen two pairs of revolution speed of propeller, the vertical force that two pairs of screws are produced is greater than complete machine weight, fuselage vertical lifting; The in the situation that of hovering or vertical lifting, if reduce by two pairs of revolution speed of propeller, the vertical force that two pairs of screws are produced is less than complete machine weight, and fuselage vertically declines.
Claims (3)
- One kind have concurrently helicopter function fixed wing aircraft toy, comprise fuselage, the left and right sides of fuselage is installed with fixedly main wing, the rear portion of fuselage is provided with tailplane, the front end of fuselage is provided with screw, the rotating shaft of screw extends longitudinally, the rotating shaft of screw is driven by main motor, it is characterized in that: the quantity of described screw is two pairs, and two pairs of screws are arranged as context, the direction of rotation of screw under main motor drives, before the rotating shaft of screw overlap and in the rotating shaft of screw in the back, form coaxial relation; Described tailplane is arranged on afterbody swingably, and the rotating shaft left and right of tailplane is laterally extending, and the first steering wheel is also installed in fuselage, and the first steering wheel is connected and driven tailplane to swing by the first pull bar.
- According to claim 1 have concurrently helicopter function fixed wing aircraft toy, it is characterized in that: fuselage is also provided with gyroscope and microprocessor, gyroscope connects microprocessor by holding wire, and microprocessor connects the control circuit of described main motor, the control circuit of the first steering wheel by holding wire.
- According to claim 1 and 2 have concurrently helicopter function fixed wing aircraft toy, it is characterized in that: the rear portion of fuselage is also rotatably mounted with vertical empennage, vertically the rotating shaft of empennage is vertically extended, the second steering wheel is also installed in fuselage, and the second steering wheel is connected and is driven vertical empennage to swing by the second pull bar; Microprocessor connects the control circuit of described the second steering wheel by holding wire.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420258078.9U CN203916079U (en) | 2014-05-20 | 2014-05-20 | Have the fixed wing aircraft toy of helicopter function concurrently |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420258078.9U CN203916079U (en) | 2014-05-20 | 2014-05-20 | Have the fixed wing aircraft toy of helicopter function concurrently |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203916079U true CN203916079U (en) | 2014-11-05 |
Family
ID=51811963
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420258078.9U Expired - Fee Related CN203916079U (en) | 2014-05-20 | 2014-05-20 | Have the fixed wing aircraft toy of helicopter function concurrently |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203916079U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107161324A (en) * | 2017-06-12 | 2017-09-15 | 河北天启通宇航空器材科技发展有限公司 | Gyroplane empennage assembly structure |
| CN107364572A (en) * | 2017-08-11 | 2017-11-21 | 红河学院 | Fixed-wing vector unmanned plane |
| CN110090457A (en) * | 2019-05-30 | 2019-08-06 | 成都航空职业技术学院 | A kind of Three-wing-surface adjustable hand throwing aircraft |
-
2014
- 2014-05-20 CN CN201420258078.9U patent/CN203916079U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107161324A (en) * | 2017-06-12 | 2017-09-15 | 河北天启通宇航空器材科技发展有限公司 | Gyroplane empennage assembly structure |
| CN107364572A (en) * | 2017-08-11 | 2017-11-21 | 红河学院 | Fixed-wing vector unmanned plane |
| CN107364572B (en) * | 2017-08-11 | 2024-01-30 | 昆明学院 | Fixed wing vector unmanned plane |
| CN110090457A (en) * | 2019-05-30 | 2019-08-06 | 成都航空职业技术学院 | A kind of Three-wing-surface adjustable hand throwing aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| ASS | Succession or assignment of patent right |
Owner name: WANG LIYUN Free format text: FORMER OWNER: SHANTOU BODI TECHNOLOGY CO., LTD. Effective date: 20150504 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20150504 Address after: 515000 Guangdong Province, Shantou city Longhu District Zhuchi Street Changping Road 182, Sunshine Coast Garden six district 20 building 1104 room Patentee after: Wang Liyun Address before: Chenghai District of Guangdong city in Shantou province 515000 Cheng Hua Street South of Cheng Hua Lu Shang Dai Bai Ge Pu Patentee before: SHANTOU BODI TECHNOLOGY CO., LTD. |
|
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20141105 Termination date: 20180520 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |