CN201395246Y - Plane capable of flying by flapping wings - Google Patents
Plane capable of flying by flapping wings Download PDFInfo
- Publication number
- CN201395246Y CN201395246Y CN2009200134443U CN200920013444U CN201395246Y CN 201395246 Y CN201395246 Y CN 201395246Y CN 2009200134443 U CN2009200134443 U CN 2009200134443U CN 200920013444 U CN200920013444 U CN 200920013444U CN 201395246 Y CN201395246 Y CN 201395246Y
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- empennage
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Abstract
The utility model relates to a plane capable of flying by flapping wings, which is characterized by comprising a plane body, wings, a front wheel, a back wheel, a front axle, a first chain wheel, a chain, a second chain wheel, a power output device, a front axle supporting frame, a wing flapping driving rod, a gravity adjusting rod, a connecting bolt, a vertical fixing empennage, a horizontal fixing empennage, a vertical adjusting empennage and a horizontal adjusting empennage. The roots of the wings are articulated with the plane body, the front axle is connected with the plane body by the front axle supporting frame, the front wheel is fixedly arranged at the two ends of the front axle, the first chain wheel is fixedly arranged in the middle of the front axle, the second chain wheel is arranged on the output shaft of the power output device, the power output device is fixedly arranged at the lower part of the plane body, the chain is connected with the first chain wheel and the second chain wheel, and one end of the two wing flapping driving rods is articulated with the front wheel and the other end is articulated with the bottoms of the wings. The utility model can realize the wing-flapping flying and has the advantages of simple structure and low cost.
Description
Technical field
The utility model relates to the aircraft field, particularly a kind of aircraft of flying of agitating by wing.
Background technology
At present, the aircraft that can fly on the market, major part utilizes fixed-wing or screw propeller to realize flight, and it is dumb to fly.
The utility model content
The purpose of this utility model is in order to realize flapping flight flexibly, and the spy provides a kind of aircraft of flying of agitating by wing.
The utility model provides a kind of and has agitated the aircraft that flies by wing, and it is characterized in that: described aircraft of agitating to fly by wing comprises fuselage 1, wing 2, front-wheel 3, trailing wheel 4, front wheel spindle 5, first sprocket wheel 6, chain 7, the second sprocket wheels 8, power take-off implement 9, front wheel spindle bearing support 10, wing are agitated drive spindle 12, center of gravity adjusting lever 14, attaching screw 15, vertical fixing empennage 16, horizontal fixed empennage 17, vertical adjustment empennage 18, horizontal adjustment empennage 19;
Wherein: the root of two wings 2 and fuselage 1 are hinged, front wheel spindle 5 is connected with fuselage 1 by front wheel spindle bearing support 10, front-wheel 3 is fixedly mounted on the two ends of front wheel spindle 5, first sprocket wheel 6 is fixedly mounted on the centre of front wheel spindle 5, trailing wheel 4 is installed in below the fuselage afterbody, second sprocket wheel 8 is installed on the output shaft of power take-off implement 9, power take-off implement 9 is fixedly mounted on the bottom of fuselage 1, chain 7 connects first sprocket wheel 6 and second sprocket wheel 8, two wings agitate an end of drive spindle 12 and front-wheel 3 hinged, the bottom-hinged of the other end and two wings 2, vertical fixing empennage 16 and horizontal fixed empennage 17 are fixedly mounted on the afterbody of fuselage 1 respectively, vertical adjustment empennage 18 is hinged with the rear portion of vertical fixing empennage 16, and horizontal adjustment empennage 19 is hinged with the rear portion of horizontal fixed empennage 17.
Described aircraft of agitating to fly by wing comprises that also first setting device, 11, the first setting devices 11 are installed on the front wheel spindle bearing support 10, can regulate the length of wheel shaft bearing support 10.
Described aircraft of agitating to fly by wing comprises that also second setting device, 13, the second setting devices 13 are installed in wing and agitate can regulate the length that wing is agitated drive spindle 12 on the drive spindle 12.
The described wing 2 of the aircraft that flies of agitating by wing is double-layer structure, has through hole respectively, and through hole staggers and arrange, and lower floor is that flexible material is made.
Described power take-off implement 9 is a motor.
Described power take-off implement 9 also can be combustion engine.
Principle of work of the present utility model:
Power take-off implement 9 provides the motion output of rotating manner, drives front-wheel 3 by chain 7 and rotates, and agitates drive spindle 12 to drive wing 2 by wing and agitates, realize sporting flying.By adjusting the front and back position of center of gravity adjusting lever 14, can regulate the position at the center of gravity place of aircraft.
Advantage of the present utility model:
Described in the utility modelly agitate the aircraft that flies by wing, can realize flapping flight, simple in structure, cost is low.
Description of drawings
Below in conjunction with drawings and the embodiments the utility model is described in further detail:
Fig. 1 is the integral structure side schematic view of aircraft;
Fig. 2 is the integral structure forward direction scheme drawing of aircraft;
Fig. 3 is the upper strata scheme drawing of aircraft wing;
Fig. 4 is lower floor's scheme drawing of aircraft wing.
The specific embodiment
Present embodiment provides a kind of and has agitated the aircraft that flies by wing, and it is characterized in that: described aircraft of agitating to fly by wing comprises fuselage 1, wing 2, front-wheel 3, trailing wheel 4, front wheel spindle 5, first sprocket wheel 6, chain 7, the second sprocket wheels 8, power take-off implement 9, front wheel spindle bearing support 10, wing are agitated drive spindle 12, center of gravity adjusting lever 14, attaching screw 15, vertical fixing empennage 16, horizontal fixed empennage 17, vertical adjustment empennage 18, horizontal adjustment empennage 19;
Wherein: the root of two wings 2 and fuselage 1 are hinged, front wheel spindle 5 is connected with fuselage 1 by front wheel spindle bearing support 10, front-wheel 3 is fixedly mounted on the two ends of front wheel spindle 5, first sprocket wheel 6 is fixedly mounted on the centre of front wheel spindle 5, trailing wheel 4 is installed in below the fuselage afterbody, second sprocket wheel 8 is installed on the output shaft of power take-off implement 9, power take-off implement 9 is fixedly mounted on the bottom of fuselage 1, chain 7 connects first sprocket wheel 6 and second sprocket wheel 8, two wings agitate an end of drive spindle 12 and front-wheel 3 hinged, the bottom-hinged of the other end and two wings 2, vertical fixing empennage 16 and horizontal fixed empennage 17 are fixedly mounted on the afterbody of fuselage 1 respectively, vertical adjustment empennage 18 is hinged with the rear portion of vertical fixing empennage 16, and horizontal adjustment empennage 19 is hinged with the rear portion of horizontal fixed empennage 17.
Described aircraft of agitating to fly by wing comprises that also first setting device, 11, the first setting devices 11 are installed on the front wheel spindle bearing support 10, can regulate the length of wheel shaft bearing support 10.
Described aircraft of agitating to fly by wing comprises that also second setting device, 13, the second setting devices 13 are installed in wing and agitate can regulate the length that wing is agitated drive spindle 12 on the drive spindle 12.
The described wing 2 of the aircraft that flies of agitating by wing is double-layer structure, has through hole respectively, and through hole staggers and arrange, and lower floor is that flexible material is made.
Described power take-off implement 9 is a motor.
The principle of work of present embodiment:
Power take-off implement 9 provides the motion output of rotating manner, drives front-wheel 3 by chain 7 and rotates, and agitates drive spindle 12 to drive wing 2 by wing and agitates, realize sporting flying.By adjusting the front and back position of center of gravity adjusting lever 14, can regulate the position at the center of gravity place of aircraft.
Present embodiment provides a kind of and has agitated the aircraft that flies by wing, and it is characterized in that: described aircraft of agitating to fly by wing comprises fuselage 1, wing 2, front-wheel 3, trailing wheel 4, front wheel spindle 5, first sprocket wheel 6, chain 7, the second sprocket wheels 8, power take-off implement 9, front wheel spindle bearing support 10, wing are agitated drive spindle 12, center of gravity adjusting lever 14, attaching screw 15, vertical fixing empennage 16, horizontal fixed empennage 17, vertical adjustment empennage 18, horizontal adjustment empennage 19;
Wherein: the root of two wings 2 and fuselage 1 are hinged, front wheel spindle 5 is connected with fuselage 1 by front wheel spindle bearing support 10, front-wheel 3 is fixedly mounted on the two ends of front wheel spindle 5, first sprocket wheel 6 is fixedly mounted on the centre of front wheel spindle 5, trailing wheel 4 is installed in below the fuselage afterbody, second sprocket wheel 8 is installed on the output shaft of power take-off implement 9, power take-off implement 9 is fixedly mounted on the bottom of fuselage 1, chain 7 connects first sprocket wheel 6 and second sprocket wheel 8, two wings agitate an end of drive spindle 12 and front-wheel 3 hinged, the bottom-hinged of the other end and two wings 2, vertical fixing empennage 16 and horizontal fixed empennage 17 are fixedly mounted on the afterbody of fuselage 1 respectively, vertical adjustment empennage 18 is hinged with the rear portion of vertical fixing empennage 16, and horizontal adjustment empennage 19 is hinged with the rear portion of horizontal fixed empennage 17.
Described aircraft of agitating to fly by wing comprises that also first setting device, 11, the first setting devices 11 are installed on the front wheel spindle bearing support 10, can regulate the length of wheel shaft bearing support 10.
Described aircraft of agitating to fly by wing comprises that also second setting device, 13, the second setting devices 13 are installed in wing and agitate can regulate the length that wing is agitated drive spindle 12 on the drive spindle 12.
The described wing 2 of the aircraft that flies of agitating by wing is double-layer structure, has through hole respectively, and through hole staggers and arrange, and lower floor is that flexible material is made.
Described power take-off implement 9 is a combustion engine.
The principle of work of present embodiment:
Power take-off implement 9 provides the motion output of rotating manner, drives front-wheel 3 by chain 7 and rotates, and agitates drive spindle 12 to drive wing 2 by wing and agitates, realize sporting flying.By adjusting the front and back position of center of gravity adjusting lever 14, can regulate the position at the center of gravity place of aircraft.
Present embodiment provides a kind of and has agitated the aircraft that flies by wing, and it is characterized in that: described aircraft of agitating to fly by wing comprises fuselage 1, wing 2, front-wheel 3, trailing wheel 4, front wheel spindle 5, first sprocket wheel 6, chain 7, the second sprocket wheels 8, power take-off implement 9, front wheel spindle bearing support 10, wing are agitated drive spindle 12, center of gravity adjusting lever 14, attaching screw 15, vertical fixing empennage 16, horizontal fixed empennage 17, vertical adjustment empennage 18, horizontal adjustment empennage 19;
Wherein: the root of two wings 2 and fuselage 1 are hinged, front wheel spindle 5 is connected with fuselage 1 by front wheel spindle bearing support 10, front-wheel 3 is fixedly mounted on the two ends of front wheel spindle 5, first sprocket wheel 6 is fixedly mounted on the centre of front wheel spindle 5, trailing wheel 4 is installed in below the fuselage afterbody, second sprocket wheel 8 is installed on the output shaft of power take-off implement 9, power take-off implement 9 is fixedly mounted on the bottom of fuselage 1, chain 7 connects first sprocket wheel 6 and second sprocket wheel 8, two wings agitate an end of drive spindle 12 and front-wheel 3 hinged, the bottom-hinged of the other end and two wings 2, vertical fixing empennage 16 and horizontal fixed empennage 17 are fixedly mounted on the afterbody of fuselage 1 respectively, vertical adjustment empennage 18 is hinged with the rear portion of vertical fixing empennage 16, and horizontal adjustment empennage 19 is hinged with the rear portion of horizontal fixed empennage 17.
The described wing 2 of the aircraft that flies of agitating by wing is double-layer structure, has through hole respectively, and through hole staggers and arrange, and lower floor is that flexible material is made.
Described power take-off implement 9 is a motor.
The principle of work of present embodiment:
Power take-off implement 9 provides the motion output of rotating manner, drives front-wheel 3 by chain 7 and rotates, and agitates drive spindle 12 to drive wing 2 by wing and agitates, realize sporting flying.By adjusting the front and back position of center of gravity adjusting lever 14, can regulate the position at the center of gravity place of aircraft.
Claims (6)
1, a kind of aircraft of flying of agitating by wing, it is characterized in that: described aircraft of agitating to fly by wing comprises fuselage (1), wing (2), front-wheel (3), trailing wheel (4), front wheel spindle (5), first sprocket wheel (6), chain (7), second sprocket wheel (8), power take-off implement (9), front wheel spindle bearing support (10), wing is agitated drive spindle (12), center of gravity adjusting lever (14), attaching screw (15), vertical fixing empennage (16), horizontal fixed empennage (17), vertical adjustment empennage (18), horizontal adjustment empennage (19);
Wherein: the root of two wings (2) and fuselage (1) are hinged, front wheel spindle (5) is connected with fuselage (1) by front wheel spindle bearing support (10), front-wheel (3) is fixedly mounted on the two ends of front wheel spindle (5), first sprocket wheel (6) is fixedly mounted on the centre of front wheel spindle (5), trailing wheel (4) is installed in below the fuselage afterbody, second sprocket wheel (8) is installed on the output shaft of power take-off implement (9), power take-off implement (9) is fixedly mounted on the bottom of fuselage (1), chain (7) connects first sprocket wheel (6) and second sprocket wheel (8), two wings agitate an end of drive spindle (12) and front-wheel (3) hinged, the bottom-hinged of the other end and two wings (2), vertical fixing empennage (16) and horizontal fixed empennage (17) are fixedly mounted on the afterbody of fuselage (1) respectively, vertical adjustment empennage (18) is hinged with the rear portion of vertical fixing empennage (16), and horizontal adjustment empennage (19) is hinged with the rear portion of horizontal fixed empennage (17).
2, according to the described aircraft that flies of agitating by wing of claim 1, it is characterized in that: described aircraft of agitating to fly by wing also comprises first setting device (11), first setting device (11) is installed on the front wheel spindle bearing support (10), the length that can regulate wheel shaft bearing support (10).
3, according to claim 1 or the 2 described aircrafts that fly of agitating by wing, it is characterized in that: described aircraft of agitating to fly by wing also comprises second setting device (13), second setting device (13) is installed in wing and agitates can regulate the length that wing is agitated drive spindle (12) on the drive spindle (12).
4, agitate the aircraft that flies according to claim 1 is described by wing, it is characterized in that: described agitate the wing (2) of the aircraft that flies by wing be double-layer structure, has through hole respectively, and through hole staggers and arrange, and lower floor is that flexible material is made.
5, agitate the aircraft that flies according to claim 1 is described by wing, it is characterized in that: described power take-off implement (9) is a motor.
6, agitate the aircraft that flies according to claim 1 is described by wing, it is characterized in that: described power take-off implement (9) is a combustion engine.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009200134443U CN201395246Y (en) | 2009-05-06 | 2009-05-06 | Plane capable of flying by flapping wings |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009200134443U CN201395246Y (en) | 2009-05-06 | 2009-05-06 | Plane capable of flying by flapping wings |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201395246Y true CN201395246Y (en) | 2010-02-03 |
Family
ID=41617747
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009200134443U Expired - Fee Related CN201395246Y (en) | 2009-05-06 | 2009-05-06 | Plane capable of flying by flapping wings |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201395246Y (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104477384A (en) * | 2014-12-15 | 2015-04-01 | 佛山市神风航空科技有限公司 | Flat wing panel ornithopter |
-
2009
- 2009-05-06 CN CN2009200134443U patent/CN201395246Y/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104477384A (en) * | 2014-12-15 | 2015-04-01 | 佛山市神风航空科技有限公司 | Flat wing panel ornithopter |
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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: 20100203 Termination date: 20110506 |