CN202320779U - Common people airplane - Google Patents
Common people airplane Download PDFInfo
- Publication number
- CN202320779U CN202320779U CN2011200270568U CN201120027056U CN202320779U CN 202320779 U CN202320779 U CN 202320779U CN 2011200270568 U CN2011200270568 U CN 2011200270568U CN 201120027056 U CN201120027056 U CN 201120027056U CN 202320779 U CN202320779 U CN 202320779U
- Authority
- CN
- China
- Prior art keywords
- rotor
- common people
- overriding clutch
- base pipe
- lifting body
- 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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- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Abstract
The utility model provides a common people airplane which is characterized in that: the upper end of a central pipe (8) is coupled with a fixed lifting body (10) through a bolt (9); upper and lower rotary discs (6) are arranged through a ball bearing (7); the rotary discs (6) are provided with rotor wings (2) of small wings (1) with ends; an engine (11) transmits power to the rotor wings (2) through an overrun clutch (12); the lower end of the central pipe is connected with a cabin (15) by bolts (14) through a joint bearing (13); and the tail end of the central pipe (8) is provided with a control rod (13).
Description
Technical field
Utility model " common people's aircraft " relates to a kind of simple and easy aircraft, belongs to the aviation machine field.
Background technology
At present the rotor series products in the known simple and easy aircraft product engineering is as the background technology of the utility model, exist consumption of power big with need defective such as special-purpose place.
The utility model content
The purpose of the utility model " common people's aircraft " provides a kind of simple and easy aircraft and solves the big cost high-technology of the energy consumption difficult problem that prior art products exists.
The technical scheme that is provided of common people's aircraft:
1, utilize and to have a pair of counter-rotating rotor of hold wing lift member of deciding, complete machine is exerted oneself to be increased and energy consumption decline;
2, fixedly lifting body is equipped with on the top, and additional lift is provided in advancing;
3, rotor is connected with overriding clutch with many driving engines, guarantees when indivedual or whole engine off, and rotor still can rotate under air-flow promotes, and the lift of generation can guarantee that state flight landing falls in complete machine to waft, and safety greatly improves.
Embodiment is: a kind of common people's aircraft; Wherein pass through fixedly lifting body of bolted connection in the base pipe upper end; Through ball-bearing casing two rotating discs up and down are housed, the rotor of band edge winglet has been installed on rotating disc, driving engine is passed to rotor through overriding clutch with power; In the lower end of base pipe, through oscillating bearing and passenger cabin bolt together; End at base pipe is equipped with control stalk.
Further the wing of a pair of rotor of coaxial reverse has the end winglet slightly.
Further each driving engine all passes through overriding clutch and is connected with rotor; Its structure: engine output shaft is connected with the star-wheel of overriding clutch through key; The outer ring of overriding clutch is connected with magnetic gearing wheel through key, passes through magnetic drive between magnetic gearing wheel and the rotating disc.
Further have circular vortex generator at the fixing lower surface of lifting body.
Description of drawings
Fig. 1: complete machine conceptual scheme 2: rotor folding structure scheme
Fig. 3: power unidirectional delivery detail drawing Fig. 4: fixing lifting body constructional drawing
The specific embodiment:
The embodiment of the utility model, do following explanation in conjunction with accompanying drawing 1～4:
With reference to shown in Figure 1,, fixedly lifting body 10 is installed through bolt 9 in base pipe 8 upper ends; Through ball-bearing casing 7 two rotating discs 6 up and down are housed, the rotor that has winglet 12 with the number blade is installed on each rotating disk, the mode of operation of rotor 2 and folding state are with hinge knot axle 4 and bolt of rear end plate 5 determined (as shown in Figure 2).Each driving engine 11 is all passed to rotor, concrete structure through overriding clutch 12 with power
As shown in Figure 3.In Fig. 3; Engine output shaft 19 is connected with the star-wheel 22 of overriding clutch through key 20, and the outer ring 23 of overriding clutch is connected with magnetic gearing wheel 25 through key 24; Pass through magnetic drive between magnetic gearing wheel 25 and the rotor reaction plate 26, so need not to be provided with lubricating system in this scheme.
In the lower end of base pipe 8, be connected with passenger cabin 15 usefulness bolts 14 with oscillating bearing 13, soft seat 16 to be installed on the chair frame 17 in passenger cabin 15 have been formed seat, the passenger cabin bottom is equipped with landing land wheel 18.End at base pipe 8 is equipped with control stalk 3, promotes the axis direction that this bar can change base pipe, with this change of flight device state.
Fig. 4 representes the fixedly structure of lift, and this is the round pie parts that a upper surface is heaved.The middle part setting-in coupling sleeve, bottom the eddy current ring (shown in φ A, φ B) of two circle indents is arranged, its effect is to make the air-flow of the bottom of flowing through produce eddy current, reduces the speed through the bottom air-flow, improves the lift effect.
Claims (4)
1. common people's aircraft is characterized by: through the fixing lifting body of bolted connection, two rotating discs about being equipped with through ball-bearing casing have been installed the rotor of band edge winglet on rotating disc in the base pipe upper end, and driving engine is passed to rotor through overriding clutch with power; In the lower end of base pipe, through oscillating bearing and passenger cabin bolt together; End at base pipe is equipped with control stalk.
2. common people's aircraft according to claim 1 is characterized in that the wing of a pair of rotor of coaxial reverse has the end winglet slightly.
3. common people's aircraft according to claim 2; It is characterized in that each driving engine all passes through overriding clutch and is connected with rotor; Its structure: engine output shaft is connected with the star-wheel of overriding clutch through key; The outer ring of overriding clutch is connected with magnetic gearing wheel through key, passes through magnetic drive between magnetic gearing wheel and the rotating disc.
4. common people's aircraft according to claim 1 is characterized in that having circular vortex generator at the fixing lower surface of lifting body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011200270568U CN202320779U (en) | 2011-01-17 | 2011-01-17 | Common people airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011200270568U CN202320779U (en) | 2011-01-17 | 2011-01-17 | Common people airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202320779U true CN202320779U (en) | 2012-07-11 |
Family
ID=46432769
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011200270568U Expired - Fee Related CN202320779U (en) | 2011-01-17 | 2011-01-17 | Common people airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202320779U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103693188A (en) * | 2014-01-03 | 2014-04-02 | 南京航空航天大学 | Wing folding and unfolding mechanism of unmanned aerial vehicle |
| CN104627363A (en) * | 2013-11-13 | 2015-05-20 | 银川上河图新技术研发有限公司 | Device for greatly increasing load of helicopter under same power |
| CN107054640A (en) * | 2014-10-22 | 2017-08-18 | 李志强 | A kind of lift unit with the disk wing and the aircraft using the device |
-
2011
- 2011-01-17 CN CN2011200270568U patent/CN202320779U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104627363A (en) * | 2013-11-13 | 2015-05-20 | 银川上河图新技术研发有限公司 | Device for greatly increasing load of helicopter under same power |
| CN103693188A (en) * | 2014-01-03 | 2014-04-02 | 南京航空航天大学 | Wing folding and unfolding mechanism of unmanned aerial vehicle |
| CN107054640A (en) * | 2014-10-22 | 2017-08-18 | 李志强 | A kind of lift unit with the disk wing and the aircraft using the device |
| CN107054640B (en) * | 2014-10-22 | 2019-07-16 | 宝嘉智能科技(南通)有限公司 | A kind of lift unit with the disk wing and the aircraft using the device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120711 Termination date: 20150117 |
|
| EXPY | Termination of patent right or utility model |