CN105083552A - Saucer-shaped aircraft - Google Patents
Saucer-shaped aircraft Download PDFInfo
- Publication number
- CN105083552A CN105083552A CN201410219581.8A CN201410219581A CN105083552A CN 105083552 A CN105083552 A CN 105083552A CN 201410219581 A CN201410219581 A CN 201410219581A CN 105083552 A CN105083552 A CN 105083552A
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- China
- Prior art keywords
- impeller
- cover
- shaped
- disc
- engine
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Abstract
The invention provides a saucer-shaped aircraft in order to solve the technical problems that an existing saucer-shaped aircraft is insufficient in balance adjustment and power supply. The saucer-shaped aircraft comprises a saucer-shaped cover, a work bin and an engine. The saucer-shaped cover and the work bin are connected together through a connecting plate. The engine is installed in the work bin. A fan wheel is installed on a main shaft of the engine. A balance mechanism is arranged in the middle of the fan wheel and installed on the main shaft of the engine. The top of the saucer-shaped cover is provided with a saucer-shaped cover air port corresponding to the middle of the fan wheel. The engine drives the fan wheel to rotate so that wind power can be provided; the wind power is blown out around the saucer-shaped cover and provides power for the aircraft; and the balance mechanism located in the middle of the fan wheel can adjust balance of the aircraft in the flying process.
Description
Technical field
The present invention relates to a kind of flight instruments, be specifically related to a kind of disc-shaped flying craft.
Background technology
Helicopter can be divided into four classes substantially: one is air-flotation type, comprise dirigible, fire balloon, hydrogen balloon or nitrogen ball etc., two is propcopters, comprise one or more groups screw propeller, also the furnished osprey opportunity of combat of U.S. army is comprised, three is the fixing Ji opportunities of combat that can vertically hoist, as " sparrow hawk " formula opportunity of combat of France.Four is the flying saucers in hearsay.About flying saucer, may also be referred to as disc-shaped flying craft, someone has made patent application, but existing disc-shaped flying craft, Shortcomings in the balance regulated in flight course and power.
Summary of the invention
The technical problem to be solved in the present invention is existing disc-shaped flying craft, balance adjustment, supply of power Shortcomings, for solving the problem, provides a kind of disc-shaped flying craft.
The object of the invention is to realize in the following manner:
A kind of disc-shaped flying craft, it comprises dish cover, working bin and driving engine, and dish cover is linked together by connecting panel and working bin, and driving engine is arranged in working bin; Described engine spindle installs impeller; In the middle part of described impeller, arrange equalizing gear, equalizing gear is arranged on engine spindle; The dish cover air port corresponding with in the middle part of impeller is offered at described dish cover top.
Described connecting panel is uniformly distributed in one week of working bin.
Described impeller comprises impeller base, flabellum and impeller cover, and flabellum is evenly distributed between impeller base and impeller cover, and impeller cover top offers the impeller air port corresponding with dish cover air port.
At described dish cover air port place, between dish cover and engine spindle, stirrup I is set; At described impeller air port place, between impeller cover and engine spindle, be provided with stirrup II.
Described stirrup I and stirrup II are all arranged on engine spindle by bearing.
Described equalizing gear comprises pipe link, is arranged on bob-weight and the arc at pipe link two ends, and pipe link is arranged on engine spindle by bearing.
A circle air regulating board is set inside described dish-shaped shroud rim, is also provided with a circle air door along described dish-shaped shroud rim.
Relative to prior art, driven by engine impeller of the present invention rotates, and provide wind-force, wind-force blows out along dish-shaped cover surrounding, and for aircraft provides power, the equalizing gear be arranged in the middle part of impeller can regulate the balance of aircraft flight process.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention.
Fig. 2 is the structural representation of dish cover.
Fig. 3 is the structural representation of impeller.
Fig. 4 is exterior contour figure of the present invention.
Detailed description of the invention
As shown in Figure 1, a kind of disc-shaped flying craft, it comprises dish cover 1, working bin 2 and driving engine 3, and dish cover 1 is linked together by connecting panel 4 and working bin 2, and connecting panel is uniformly distributed in one week of working bin; Driving engine 3 is arranged in working bin 2; Engine spindle 6 is installed impeller 5, as shown in Figure 3, impeller 5 comprises impeller base 9, flabellum 10 and impeller cover 11, flabellum 10 is evenly distributed between impeller base 9 and impeller cover 11, cover 1 top at dish and offer the dish cover air port 7 corresponding with in the middle part of impeller, impeller cover 11 top offers the impeller air port 8 corresponding with dish cover air port 7.
In the middle part of impeller, arrange equalizing gear, equalizing gear comprises pipe link 15, is arranged on bob-weight 16 and the arc 17 at pipe link 15 two ends, and pipe link 15 is arranged on engine spindle 6 by bearing 14; At dish cover air port place, between dish cover 1 and engine spindle 6, stirrup I 12 is set; At impeller air port place, between impeller cover 11 and engine spindle 6, be provided with stirrup II 13.Stirrup I 12 and stirrup II 13 are all arranged on engine spindle 6 by bearing 14.As shown in Figure 2 and Figure 4, a circle air regulating board 18 is set inside dish cover 1 edge, is also provided with a circle air door 19 along dish-shaped shroud rim.
Actuating unit (impeller) and equalizing gear are installed on the main shaft of driving engine by the present invention, compact conformation, when taking off, driven by engine impeller rotates, and makes air constantly to dish-shaped cover surrounding flowing, blows out downwards along air regulating board, thus produce a thrust upwards, for disc-shaped flying craft provides power upwards, the middle part at impeller place can produce negative pressure, and air is constantly entered from dish cover air port; Equalizing gear adopts bob-weight and arc plate structure, when aircraft run-off the straight, bob-weight can move to inclined side, at this moment arc can block opposite side flows to dish-shaped shroud rim air from impeller, thus reduce opposite side thrust upwards, automatically can adjust the inclination of aircraft, ensure the balance in aircraft flight process.
Arrange a circle air door in dish-shaped shroud rim, when opening an air door, aircraft can fly to relative direction; Open the air door of line direction before aircraft, can aircraft down be made; Open the air door about line direction before aircraft, aircraft can be made to adjust heading; Open multiple air door, aircraft landing can be realized.Air door can make aircraft carry out parallel flight, turn to, stops and land.
Inside dish-shaped shroud rim, arrange air regulating board, when aircraft is in vacant state, in impeller, flabellum rotates towards a direction, and due to antagonistic force, aircraft then can rotate to direction in opposite directions, in order to overcome this problem, arranges air regulating board, and the device that socks in rotates.
Claims (7)
1. a disc-shaped flying craft, is characterized in that: it comprises dish cover, working bin and driving engine, and dish cover is linked together by connecting panel and working bin, and driving engine is arranged in working bin; Described engine spindle installs impeller; In the middle part of described impeller, arrange equalizing gear, equalizing gear is arranged on engine spindle; The dish cover air port corresponding with in the middle part of impeller is offered at described dish cover top.
2. disc-shaped flying craft according to claim 1, is characterized in that: described connecting panel is uniformly distributed in one week of working bin.
3. disc-shaped flying craft according to claim 1, it is characterized in that: described impeller comprises impeller base, flabellum and impeller cover, flabellum is evenly distributed between impeller base and impeller cover, and impeller cover top offers the impeller air port corresponding with dish cover air port.
4. disc-shaped flying craft according to claim 3, is characterized in that: at described dish cover air port place, arrange stirrup I between dish cover and engine spindle; At described impeller air port place, between impeller cover and engine spindle, be provided with stirrup II.
5. disc-shaped flying craft according to claim 4, is characterized in that: described stirrup I and stirrup II are all arranged on engine spindle by bearing.
6. disc-shaped flying craft according to claim 1, is characterized in that: described equalizing gear comprises pipe link, is arranged on bob-weight and the arc at pipe link two ends, and pipe link is arranged on engine spindle by bearing.
7. disc-shaped flying craft according to claim 1, is characterized in that: inside described dish-shaped shroud rim, arrange a circle air regulating board, be also provided with a circle air door along described dish-shaped shroud rim.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410219581.8A CN105083552B (en) | 2014-05-23 | 2014-05-23 | Saucer-shaped aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410219581.8A CN105083552B (en) | 2014-05-23 | 2014-05-23 | Saucer-shaped aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105083552A true CN105083552A (en) | 2015-11-25 |
| CN105083552B CN105083552B (en) | 2017-05-17 |
Family
ID=54565073
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410219581.8A Expired - Fee Related CN105083552B (en) | 2014-05-23 | 2014-05-23 | Saucer-shaped aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105083552B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112319799A (en) * | 2020-11-03 | 2021-02-05 | 谭成刚 | Wingless aircraft |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2006069361A (en) * | 2004-09-01 | 2006-03-16 | Mitsubishi Heavy Ind Ltd | Flying body with attitude controller |
| CN200967029Y (en) * | 2006-11-21 | 2007-10-31 | 李宝贵 | Flying saucer sprayer |
| CN201284014Y (en) * | 2008-08-25 | 2009-08-05 | 王人庆 | Discs type helicopters |
| CN201457738U (en) * | 2009-04-16 | 2010-05-12 | 赵忠祥 | Dishing aircraft |
| CN102020020A (en) * | 2010-12-08 | 2011-04-20 | 张奎 | Aerospace flying saucer aircraft |
-
2014
- 2014-05-23 CN CN201410219581.8A patent/CN105083552B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2006069361A (en) * | 2004-09-01 | 2006-03-16 | Mitsubishi Heavy Ind Ltd | Flying body with attitude controller |
| CN200967029Y (en) * | 2006-11-21 | 2007-10-31 | 李宝贵 | Flying saucer sprayer |
| CN201284014Y (en) * | 2008-08-25 | 2009-08-05 | 王人庆 | Discs type helicopters |
| CN201457738U (en) * | 2009-04-16 | 2010-05-12 | 赵忠祥 | Dishing aircraft |
| CN102020020A (en) * | 2010-12-08 | 2011-04-20 | 张奎 | Aerospace flying saucer aircraft |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112319799A (en) * | 2020-11-03 | 2021-02-05 | 谭成刚 | Wingless aircraft |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105083552B (en) | 2017-05-17 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170517 Termination date: 20180523 |