CN2558583Y - Circular wing light aviation passenger plane - Google Patents
Circular wing light aviation passenger plane Download PDFInfo
- Publication number
- CN2558583Y CN2558583Y CN 02247068 CN02247068U CN2558583Y CN 2558583 Y CN2558583 Y CN 2558583Y CN 02247068 CN02247068 CN 02247068 CN 02247068 U CN02247068 U CN 02247068U CN 2558583 Y CN2558583 Y CN 2558583Y
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- China
- Prior art keywords
- fuselage
- wing
- passenger plane
- lifting
- type light
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Abstract
The utility model relates to a light airliner with round wing, which is a novel aircraft by employing vertical design scheme and having a disc-shaped wing. The utility model comprises a body, wings, a landing gear, a lifting dynamic system and a right and left wing propulsion dynamic system. The body takes the shape of oval; the lifting dynamic system and the right and left wing propulsion dynamic system are installed on the disc-shaped wing, so as to control aircraft rising and advancing. The utility model integrates the functions of helicopter and transporter, has the advantages of stable centre of gravity, being easy to control and safe operation.
Description
Affiliated technical field
Circular wing type light aircraft passenger plane described in the utility model is a kind of the have steadily of centre of gravity of disc wing structure, course of new aircraft that is easy to control.
Background technology
The aircraft of widespread usage mainly is conventional transport and helicopter at present, mostly imitates the principle research of birds flight in design and makes, and is streamlined structure, is made up of head, fuselage, wing, tail, alighting gear.But transport plane adopts the method for transverse design, makes aircraft produce very big inertia awing, has stronger impulsive force, takes off, need lay very long flight runway when landing, and when meeting accident accident, causes crank, shortcoming such as wayward easily; Helicopter utilizes screw propeller that active flight is provided, and stability is better during vertical flight, but wayward when horizontal flight, and field of application is narrower, civilian aircraft that neither be desirable.In order to overcome the existing in prior technology problem, it is very necessary developing a kind of later-model circular wing type light aircraft passenger plane.
Summary of the invention
In view of above-mentioned existing in prior technology problem is invented the course of new aircraft that provides a kind of steadily of centre of gravity, is easy to control, operate driving safety.
Circular wing type light aircraft passenger plane described in the utility model, its structure are to be made up of fuselage, wing, alighting gear, lifting power system, left and right propulsion system; Fuselage is an oval structures, and the top is a driving compartment, and the below is a transport pod, is connected by staircase between driving compartment and the transport pod; Transport pod links to each other with the hold of fuselage bottom, and actuating units such as storage battery are installed by portion within it; Driving compartment links to each other with the overhead bin at fuselage top, in overhead bin inside the suspension umbrella of slinging is housed, and the overhead bin top is provided with the overhead bin door; Wing is a disc-shaped structure, and the center that is fixedly mounted on body shell is portion on the upper side, between driving compartment and transport pod; The lifting power system is made up of two sustainer, main engines and four lifting worm gears; The left and right propulsion system is made up of two electronic worm gears; In the body of disc wing, the both sides, front and back of fuselage respectively symmetry a sustainer, main engine and two lifting worm gears are installed; On the disc wing, the left and right sides of fuselage respectively symmetry an electronic propelling worm gear is installed; Alighting gear is installed in the below of fuselage; Lifting power system described in the utility model has been installed netted outer cover on the lifting worm gear; Fuselage described in the utility model, the bottom in its outside is provided with overlooks mirror; The upper surface of disc wing described in the utility model is provided with solar energy absorption plant; Each lifting worm gear described in the utility model, its below has been installed to aircraft rises auxiliary power is provided, and slows down the air of the leaf structure of descending speed during decline and transfers the stream device.
Circular wing type light aircraft passenger plane described in the utility model has adopted vertical design-calculated method in design, has changed traditional thoughtcast and design concept, and the fuselage of oval structures and the wing of disc-shaped structure make aircraft have stable center of gravity.Be provided with lifting power system and left and right propulsion system on the aircraft, adopted Worm gear mechanism, the air-flow that produces by mechanical power is regulated and control the operation of aircraft, makes the aircraft in the horizontal direction can both smooth flight with vertical direction, thereby has guaranteed the safety of driving and taking.
Description of drawings
The utility model has two accompanying drawings, wherein:
Fig. 1: circular wing type light aircraft passenger plane structural representation (front view)
Fig. 2: circular wing type light aircraft passenger plane structural representation (birds-eye view)
Fig. 3: circular wing type light aircraft passenger plane structural representation (left view)
Fig. 4: circular wing type light aircraft passenger plane structural representation (back view)
Among the figure: 1, fuselage 2, wing 3, electronic propelling worm gear 4, lifting worm gear 5, sustainer, main engine 6, overlook mirror 7, alighting gear 8, driving compartment 9, transport pod 10, hold 11, overhead bin 12, hatch door 13, air and transfer the stream device
The specific embodiment
The specific embodiment of circular wing type light aircraft passenger plane described in the utility model is as shown in the figure: its structure is made up of fuselage 1, wing 2, alighting gear 7, lifting power system, left and right propulsion system; Fuselage 1 is an oval structures, and the top is a driving compartment 8, and the below is a transport pod 9, is connected by staircase between driving compartment 8 and the transport pod 9; Transport pod 9 links to each other with the hold 10 of fuselage bottom, at actuating units such as hold 10 inner installation storage batterys; Driving compartment 8 links to each other with the overhead bin 11 at fuselage top, in overhead bin 11 inside the suspension umbrella of slinging is housed, and overhead bin 11 tops are provided with the overhead bin door; Wing 2 is a disc-shaped structure, and the center that is fixedly mounted on fuselage 1 housing is portion on the upper side, between driving compartment 8 and transport pod 9; The lifting power system is made up of two sustainer, main engines 5 and four lifting worm gears 4; The left and right propulsion system is made up of two electronic worm gears 3; In the body of disc wing 2, the both sides, front and back of fuselage 1 respectively symmetry a sustainer, main engine 5 and two lifting worm gears 4 are installed; On disc wing 2, the left and right sides of fuselage 1 respectively symmetry an electronic propelling worm gear 3 is installed; Alighting gear 7 is installed in the below of fuselage 1; Lifting worm gear 4 is provided with netted outer cover; The bottom in fuselage 1 outside is provided with overlooks mirror 6; Below each lifting worm gear 4, installed to aircraft rises auxiliary power is provided, slow down the air of the leaf structure of descending speed during decline and transfer stream device 13.Fuel Tank is installed in the body of disc wing 2.When taking off, synchronous rotation by former and later two sustainer, main engines of fuselage, the lifting worm gear of sustainer, main engine both sides before and after driving respectively, produce backspin and advance air-flow, make the aircraft vertical uplift, after the arrival flying height, start the left and right propulsion system, adjust direction, after determining the position, start the electronic propelling worm gear of both wings and rotate synchronously, make the aircraft horizontal flight, after arriving the destination, the rotating speed of sustainer, main engine slows down the lifting air-flow before and after reducing, and closes the left and right propulsion system, make vertical, the stable landing of aircraft, thereby finish the air transport process.In the process of aircraft operation, when dangerous situation takes place, can open the hatch door of overhead bin 11, utilize the suspension umbrella of slinging that aircraft is slowly descended.
Claims (5)
1, a kind of circular wing type light aircraft passenger plane; It is characterized in that being formed by fuselage (1), wing (2), alighting gear (7), lifting power system, left and right propulsion system; Fuselage (1) is an oval structures, and the top is driving compartment (8), and the below is transport pod (9), is connected by staircase between driving compartment (8) and the transport pod (9); Transport pod (9) links to each other with the hold (10) of fuselage bottom, at actuating units such as the inner installation of hold (10) storage batterys; Driving compartment (8) links to each other with the overhead bin (11) at fuselage top, in overhead bin (11) inside the suspension umbrella of slinging is housed, and overhead bin (11) top is provided with the overhead bin door; Wing (2) is a disc-shaped structure, and the center that is fixedly mounted on fuselage (1) housing is portion on the upper side, is positioned between driving compartment (8) and the transport pod (9); The lifting power system is made up of two sustainer, main engines (5) and four lifting worm gears (4); The left and right propulsion system is made up of two electronic worm gears (3); In the body of disc wing (2), the both sides, front and back of fuselage (1) respectively symmetry a sustainer, main engine (5) and two lifting worm gears (4) are installed; The symmetrical respectively electronic propelling worm gear (3) of installing in the left and right sides last at disc wing (2), fuselage (1); Alighting gear (7) is installed in the below of fuselage (1).
2, circular wing type light aircraft passenger plane according to claim 1; It is characterized in that on lifting worm gear (4), netted outer cover being installed.
3, circular wing type light aircraft passenger plane according to claim 1; The bottom that it is characterized in that fuselage (1) outside is provided with overlooks mirror (6).
4, circular wing type light aircraft passenger plane according to claim 1; The upper surface that it is characterized in that disc wing (2) is provided with solar energy absorption plant.
5, circular wing type light aircraft passenger plane according to claim 1; The below that it is characterized in that each lifting worm gear (4) has been installed to aircraft rises auxiliary power is provided, and slows down the air of the leaf structure of descending speed during decline and transfers stream device (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 02247068 CN2558583Y (en) | 2002-08-02 | 2002-08-02 | Circular wing light aviation passenger plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 02247068 CN2558583Y (en) | 2002-08-02 | 2002-08-02 | Circular wing light aviation passenger plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2558583Y true CN2558583Y (en) | 2003-07-02 |
Family
ID=33718109
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 02247068 Expired - Fee Related CN2558583Y (en) | 2002-08-02 | 2002-08-02 | Circular wing light aviation passenger plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2558583Y (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102530248A (en) * | 2011-12-12 | 2012-07-04 | 周景荣 | Design method for multifunctional helicopter |
| CN105366053A (en) * | 2015-11-19 | 2016-03-02 | 唐若权 | Disk shaped vehicle |
| WO2022040948A1 (en) * | 2020-08-26 | 2022-03-03 | 叶殊钨 | Multirotor manned aerial vehicle |
-
2002
- 2002-08-02 CN CN 02247068 patent/CN2558583Y/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102530248A (en) * | 2011-12-12 | 2012-07-04 | 周景荣 | Design method for multifunctional helicopter |
| CN105366053A (en) * | 2015-11-19 | 2016-03-02 | 唐若权 | Disk shaped vehicle |
| WO2022040948A1 (en) * | 2020-08-26 | 2022-03-03 | 叶殊钨 | Multirotor manned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |