CN201284014Y - Discs type helicopters - Google Patents
Discs type helicopters Download PDFInfo
- Publication number
- CN201284014Y CN201284014Y CNU2008200151887U CN200820015188U CN201284014Y CN 201284014 Y CN201284014 Y CN 201284014Y CN U2008200151887 U CNU2008200151887 U CN U2008200151887U CN 200820015188 U CN200820015188 U CN 200820015188U CN 201284014 Y CN201284014 Y CN 201284014Y
- Authority
- CN
- China
- Prior art keywords
- joint
- cockpit
- universal
- permanent magnet
- dish
- 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
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Abstract
A disc-type helicopter includes disc leaves, a disc leaves ring, an adjusting permanent magnet, a cockpit, an emergency parachute compartment, an outer gimbal, an inner gimbal, a vertical balance adjustment wing, an adjusting electromagnet, a permanent magnet motor, a storage battery and a landing gear, which is characterized in that the disc leaves are provided on the emergency parachute compartment, the emergency parachute compartment is connected to the cockpit though the outer gimbal and the inner gimbal, the permanent magnet motor and the storage battery are provided in the cockpit and a vertical balance adjustment wing for adjusting the electromagnet is provided above the cockpit.
Description
Technical field
The utility model relates to the vehicle technology field, particularly a kind of dish formula helicopter.
Background technology
Present autogyro exists flight resistance and noise is big, and safety factor is low and control the high shortcoming of difficulty, because it makes complicated and productive costs height, can not be extensive use of in forest fire protection, frontier defense patrol and coastal patrol.
Summary of the invention
The purpose of this utility model provides a kind of cheap, and productive costs is low, and safety factor is high to be easy to dish formula helicopter with controlling.
The utility model is to realize like this, it comprises dish leaf, dish leaf joint, adjustment permanent magnet, cockpit, escape chute storehouse, outer universal-joint, interior universal-joint, the vertical equilibrium adjustment wing, adjusts electromagnet, permanent magnet motor, storage battery and alighting gear, it is characterized in that the dish leaf is arranged on the escape chute storehouse, the escape chute storehouse is connected with cockpit with interior universal-joint by outer universal-joint, in cockpit, be provided with permanent magnet motor and storage battery, above cockpit, be provided with the vertical equilibrium adjustment wing that band is adjusted electromagnet.
The utility model is owing to be to be provided with the dish leaf on the escape chute storehouse, the escape chute storehouse is connected with cockpit with interior universal-joint by outer universal-joint, in cockpit, be provided with permanent magnet motor and storage battery, so productive costs is low, the safety factor height is adapted at being extensive use of in forest fire protection, frontier defense patrol and the coastal patrol.
Description of drawings
Below in conjunction with accompanying drawing the utility model is done further description;
Fig. 1 is the structural representation of dish formula helicopter,
Fig. 2 is outer universal-joint and the interior universal-joint structural representation partly that is connected with cockpit,
Fig. 3 is the structural representation of alighting gear.
The specific embodiment
Shown in Fig. 1-3, dish formula helicopter comprises dish leaf 1, dish leaf joint 2, adjust permanent magnet 3, cockpit 4, escape chute storehouse 5, outer universal-joint 6, interior universal-joint 7, vertical equilibrium is adjusted the wing 8, permanent magnet motor 9, storage battery 10, alighting gear 11, bearing 12, main shaft 13, connecting rod 14, screw slide block 15, motor 16, leading screw 17, screw 18, leading screw 19 and adjustment electromagnet 20, dish leaf 1 is arranged on the escape chute storehouse 5, on dish leaf joint 2, be provided with and adjust permanent magnet 3, there is escape chute storehouse 5 to be connected with cockpit 4 with interior universal-joint 7 by outer universal-joint 6, in cockpit 4, be provided with permanent magnet motor 9 and storage battery 10, above cockpit 4, be provided with band and adjust the vertical equilibrium adjustment wing 8 of electromagnet 20, outer universal-joint 6 is arranged on the dish leaf main shaft 13 by bearing 12, the lower end of outer universal-joint 6 is connected with interior universal-joint 7, outer universal-joint 6 is connected with screw slide block 15 by connecting rod 14, motor 16 is connected with screw slide block 15 by leading screw 17, alighting gear 11 is by motor 17, screw 18 and leading screw 19 are formed, during flight under the running of leading screw 19 positive and negative rotations, by connecting rod about in the of 14, about variation, rotation dish leaf 1 is climbed at translation-angle, or when descending, about realizing, dish leaf 1 turns to, the vertical equilibrium adjustment wing 8 makes the 3 moment folding of adjustment permanent magnet by the control of switch, make electromagnetic field produce the deviation that the magnetic identical with adjusting permanent magnet 3 is revised the helicopter vertical equilibrium, guarantee that cockpit 4 do not follow rotation because of the inertia that dish leaf 1 rotates.
Claims (3)
1, a kind of dish formula helicopter, it comprises dish leaf, dish leaf joint, adjustment permanent magnet, cockpit, escape chute storehouse, outer universal-joint, interior universal-joint, the vertical equilibrium adjustment wing, adjusts electromagnet, permanent magnet motor, storage battery and alighting gear, it is characterized in that the dish leaf is arranged on the escape chute storehouse, the escape chute storehouse is connected with cockpit with interior universal-joint by outer universal-joint, in cockpit, be provided with permanent magnet motor and storage battery, above cockpit, be provided with the vertical equilibrium adjustment wing that band is adjusted electromagnet.
2, the described dish formula of root a tree name claim 1 helicopter, it is characterized in that outer universal-joint is arranged on the dish leaf main shaft by bearing, the lower end of outer universal-joint is connected with interior universal-joint, and outer universal-joint is connected with the screw slide block by connecting rod, and motor is connected with the screw slide block by leading screw.
3, the described dish formula of root a tree name claim 1 helicopter is characterized in that alighting gear is made up of motor, screw and leading screw.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008200151887U CN201284014Y (en) | 2008-08-25 | 2008-08-25 | Discs type helicopters |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008200151887U CN201284014Y (en) | 2008-08-25 | 2008-08-25 | Discs type helicopters |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201284014Y true CN201284014Y (en) | 2009-08-05 |
Family
ID=40948997
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2008200151887U Expired - Fee Related CN201284014Y (en) | 2008-08-25 | 2008-08-25 | Discs type helicopters |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201284014Y (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102085912A (en) * | 2009-12-03 | 2011-06-08 | 范磊 | Dishing magnetic suspension ring-wing aircraft |
| CN104326084A (en) * | 2014-07-22 | 2015-02-04 | 深圳市先驰科技有限公司 | Dish-shaped aircraft |
| CN105083552A (en) * | 2014-05-23 | 2015-11-25 | 漯河市宇祥余热利用科技有限公司 | Saucer-shaped aircraft |
-
2008
- 2008-08-25 CN CNU2008200151887U patent/CN201284014Y/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102085912A (en) * | 2009-12-03 | 2011-06-08 | 范磊 | Dishing magnetic suspension ring-wing aircraft |
| CN105083552A (en) * | 2014-05-23 | 2015-11-25 | 漯河市宇祥余热利用科技有限公司 | Saucer-shaped aircraft |
| CN104326084A (en) * | 2014-07-22 | 2015-02-04 | 深圳市先驰科技有限公司 | Dish-shaped aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20090805 Termination date: 20100825 |