CN219134497U - Tilting propeller type vertical lifting aerial unmanned aerial vehicle - Google Patents
Tilting propeller type vertical lifting aerial unmanned aerial vehicle Download PDFInfo
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- CN219134497U CN219134497U CN202222473618.2U CN202222473618U CN219134497U CN 219134497 U CN219134497 U CN 219134497U CN 202222473618 U CN202222473618 U CN 202222473618U CN 219134497 U CN219134497 U CN 219134497U
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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Abstract
The utility model discloses a tilting propeller type vertical lifting aerial photographing unmanned aerial vehicle which comprises a frame, wings, a first propeller, a horizontal tail wing and a vertical tail wing, wherein the wings, the first propeller, the horizontal tail wing and the vertical tail wing are arranged on the left side and the right side of the frame; a propeller installation part extending forwards is arranged on a main wing close to the frame, the first propeller is movably installed at the front end of the propeller installation part and can form an included angle of 0 ︒ -90 degrees relative to the upward movement of the propeller installation part, so that the effect of vertically lifting or horizontally cruising the frame is realized; the horizontal tail comprises a main horizontal tail and an auxiliary horizontal tail, and plays a role of lifting and lowering the frame; the vertical tail fin is arranged on the inner side of the horizontal tail fin, so that the frame has static stability in the left-right yaw direction. The utility model has the advantages of simple integral structure, moderate price, good flying stability, flexibility, easy operation and strong loading capacity, and meets the demands of most consumers.
Description
Technical Field
The utility model relates to the technical field of aeromodelling, in particular to a tilting propeller type vertical lifting aerial photographing unmanned aerial vehicle.
Background
Model aircraft are model aircraft that are manufactured according to the appearance of aircraft, and model aircraft generally fall into two types, dynamic and static: static model is used for collection, display and the like, can not fly, and is a model which takes an airplane as an image and is reduced according to a certain proportion; and the dynamic state is that the model airplane can fly and can be controlled by a remote control mode.
The dynamic model aircraft can fly, mainly is a remote control model aircraft, and the flying direction and speed are controlled by a person through a remote controller. The aeroplane can fly, is increasingly crafted by model lovers, and can be used for shooting landscapes, animals and the like.
For a model airplane specially used for aerial photography, because the model airplane is provided with accessories such as a battery and a camera, certain requirements are met on the load of the model airplane, and in the prior art, the model airplane has defects in the aspect of the load, so that certain defects exist when the model airplane ascends, the voyage is short, and the speed is low; in addition, because the camera is required to track the shot object in a maneuvering way, and the shot object is required to be shot stably, or the shot object is required to be captured in a static/amplifying way in a hovering way, the mobility and stability of the model airplane in the prior art cannot meet the actual requirements.
In order to shoot high-quality aerial images, the model airplane with strong performance advantage is a target for all athletics lovers. At present, model airplanes with better performance in the market have the defects of high price, medium price and the like in the aspects of flight stability, maneuverability, loading capacity and the like, have no performance advantage and cannot meet the demands of most consumers.
Disclosure of Invention
Aiming at the defects in the prior art, the utility model provides the tilting propeller type vertical lifting aerial photographing unmanned aerial vehicle which has the advantages of simple structure, moderate price, good flying stability, flexibility, easy operation, strong loading capacity and strong performance.
In order to solve the technical problems, the technical scheme of the utility model is as follows: the utility model provides a tilting propeller type vertical lift unmanned aerial vehicle that takes photo by plane, includes the frame, installs in wing, first screw, horizontal fin and the vertical fin of frame left and right sides, and the second screw is installed to the rear end of frame, wherein:
the wing is arranged on the front side of the middle part of the frame and comprises a main wing and an auxiliary wing, the main wing is connected with the frame, the auxiliary wing is movably connected to the rear end of the main wing, and the auxiliary wing and the main wing are mutually matched to play roles of deflecting left and right and lifting the frame;
a propeller installation part extending forwards is arranged on a main wing close to the frame, the first propeller is movably installed at the front end of the propeller installation part and can form an included angle of 0 ︒ -90 degrees relative to the upward movement of the propeller installation part, so that the effect of vertically lifting or horizontally continuing the frame is realized;
the horizontal tail comprises a main horizontal tail and an auxiliary horizontal tail, the main horizontal tail is connected with the frame to play a role in stabilizing the frame in the horizontal direction, and the auxiliary horizontal tail is movably connected to the rear end of the main horizontal tail to lift and drop the frame;
the vertical tail fin is arranged on the inner side of the horizontal tail fin and comprises a vertical stable tail fin and a rudder, wherein the vertical stable tail fin is vertically and fixedly arranged on the stand, so that the stand has static stability in the left-right yaw direction, and the rudder is movably and vertically arranged at the rear end of the vertical stable tail fin so as to control the left-right deflection of the stand;
the second screw is vertically arranged at the front ends of the horizontal tail wing and the vertical tail wing and is used for assisting the first screw to enable the rack to vertically lift.
As a further illustration of the present utility model,
preferably, the periphery of the frame is provided with a fuselage, the fuselage is matched with the shape of the frame, and the main wing, the propeller installation part, the main horizontal tail wing, the vertical stabilizing tail wing and the second propeller are connected with the fuselage.
Preferably, the shape of the body is any one of a disc type, a circle type, a gyro type, a flying saucer type, a fan type, a spiral type or a light cluster type.
Preferably, the frame includes the first frame that parallel ground set up, second frame and the third frame that perpendicular to first frame left and right sides set up, first frame shape and fuselage assorted, the front end is equipped with a plurality of bar through-holes, and the rear end is equipped with a plurality of first circular through-holes, the second frame is fish-shaped fluid bodily form, through first connecting portion vertical mounting in the left and right sides both ends of first frame, the shape and the second frame assorted of third frame, and be less than the size of second frame, connect in the left and right sides both ends of second frame through the second connecting portion, the fuselage is connected in first frame, second frame and third frame.
The beneficial effects of the utility model are as follows:
the utility model comprises a frame, wings, a first propeller, a horizontal tail wing and a vertical tail wing which are arranged on the left side and the right side of the frame, wherein a second propeller is arranged at the rear end of the frame; the horizontal tail comprises a main horizontal tail and an auxiliary horizontal tail, the main horizontal tail is connected with the frame to play a role in stabilizing the frame in the horizontal direction, and the auxiliary horizontal tail is movably connected to the rear end of the main horizontal tail to lift and drop the frame; the vertical tail fin is arranged on the inner side of the horizontal tail fin and comprises a vertical stable tail fin and a rudder, wherein the vertical stable tail fin is vertically and fixedly arranged on the frame, so that the frame has static stability in the yaw direction, and the rudder is movably and vertically arranged at the rear end of the vertical stable tail fin so as to control the left and right deflection of the frame, and the components are mutually matched, so that the utility model has good stability in flying.
Secondly, the utility model is provided with the propeller installation part which extends forwards on the main wing close to the frame, the first propeller is movably installed at the front end of the propeller installation part and can form an included angle of 0 ︒ -90 degrees relative to the upward movement of the propeller installation part, the effect of the vertical lifting or horizontal endurance frame is realized, the second propeller is vertically installed at the front ends of the horizontal tail wing and the vertical tail wing and is used for assisting the first propeller to enable the frame to vertically lift, and the first propeller and the second propeller are mutually matched and rotated together, so that the loading capacity of the novel crane is greatly enhanced, and the stability of the lifting and descending of the frame is ensured.
The third frame comprises a first frame which is arranged in parallel with the ground, a second frame and a third frame which are arranged perpendicular to the left side and the right side of the first frame, the shape of the first frame is matched with that of the machine body, a plurality of strip-shaped through holes are formed in the front end of the first frame, a plurality of first round through holes are formed in the rear end of the first frame, the second frame is in a fish-shaped fluid shape and is vertically arranged at the left end and the right end of the first frame through a first connecting part, the shape of the third frame is matched with that of the second frame and is smaller than that of the second frame, the third frame is connected at the left end and the right end of the second frame through a second connecting part, the machine body is connected to the first frame, the second frame and the third frame, and the first frame, the second frame and the third frame are of an integrated structure, so that the flying stability is further improved.
Drawings
FIG. 1 is a schematic view of the overall structure of a first angle according to the present utility model.
Fig. 2 is a schematic view of the overall structure of the second angle of the present utility model.
FIG. 3 is a schematic view of a third angular exploded structure according to the present utility model.
Fig. 4 is an enlarged schematic view of the portion a in fig. 3.
In the figure: 1. a body; 2. a first propeller; 3. a second propeller; 4. a main wing; 5. an auxiliary wing; 6. a propeller mounting portion; 7. a main horizontal rear wing; 8. an auxiliary horizontal rear wing; 9. a vertically stable tail; 10. a rudder; 11. a first frame; 12. a second frame; 13. a third frame; 14. a bar-shaped through hole; 15. a first circular through hole; 16. a first connection portion; 17. a second connecting portion; 18. and a second circular through hole.
Detailed Description
The structural and operational principles of the present utility model will be described in further detail below with reference to the accompanying drawings.
The embodiments described by referring to the drawings are exemplary and intended for purposes of illustrating the present application and are not to be construed as limiting the present application. In the description of the present application, it should be understood that the terms "lower," "upper," "left," "right," "front," "rear," and the like indicate an orientation or a positional relationship based on that shown in the drawings, and are merely for convenience of description and simplification of the description, and do not indicate or imply that the apparatus or element in question must have a specific orientation, be configured and operated in a specific orientation, and therefore should not be construed as limiting the present application.
As shown in fig. 1 to 4, the utility model relates to a tilting propeller type vertical lifting aerial photographing unmanned aerial vehicle, which comprises a frame, wings, a first propeller 2, a horizontal tail wing and a vertical tail wing which are arranged at the left side and the right side of the frame, wherein a second propeller 3 is arranged at the rear end of the frame, wherein: the wing is arranged on the front side of the middle of the frame and comprises a main wing 4 and an auxiliary wing 5, the main wing 4 is connected with the frame, the main wing 4 is any one of rectangle, trapezoid, triangle, double triangle, arrow shape or edge shape, in the embodiment, the main wing 4 is rectangle, the auxiliary wing 5 is movably connected to the rear end of the main wing 4, and the auxiliary wing 5 and the main wing 4 are mutually matched to play roles of deflecting left and right and lifting the frame; a forward extending propeller installation part 6 is arranged on the main wing 4 close to the frame, the first propeller 2 is movably installed at the front end of the propeller installation part 6 and can form an included angle of 0 ︒ -90 degrees relative to the upward movement of the propeller installation part 6, so that the effect of vertically lifting or horizontally cruising the frame is realized; the horizontal tail comprises a main horizontal tail 7 and an auxiliary horizontal tail 8, the main horizontal tail 7 is connected with the frame to play a role in stabilizing the frame in the horizontal direction, and the auxiliary horizontal tail 8 is movably connected to the rear end of the main horizontal tail 7 to lift and lower the frame; the vertical tail fin is arranged on the inner side of the horizontal tail fin and comprises a vertical stable tail fin 9 and a rudder 10, the vertical stable tail fin 9 is vertically and fixedly arranged on the frame, so that the frame has static stability in the left-right yaw direction, and the rudder 10 is movably and vertically arranged at the rear end of the vertical stable tail fin 9 so as to control the left-right deflection of the frame; the second propeller 3 is vertically installed at the front ends of the horizontal tail wing and the vertical tail wing and is used for assisting the first propeller 2 to enable the frame to vertically lift.
As shown in fig. 1 to 3, a main body 1 is provided on the outer circumference of the frame, the main body 1 is matched with the shape of the frame, and the main wing 4, the propeller mounting part 6, the main horizontal tail 7, the vertical stabilizer 9 and the second propeller 3 are connected with the main body 1. Further, the shape of the body 1 is any one of a disc type, a circle type, a gyro type, a flying saucer type, a fan type, a spiral type or a light cluster type, and in this embodiment, the shape of the body 1 is a flying saucer type.
As shown in fig. 3 to 4, the rack includes a first rack 11 disposed parallel to the ground, a second rack 12 and a third rack 13 disposed perpendicular to the left and right sides of the first rack 11, the first rack 11 is shaped to match the machine body 1, a plurality of strip-shaped through holes 14 are disposed at the front end, a plurality of first circular through holes 15 are disposed at the rear end, the strip-shaped through holes 14 and the first circular through holes 15 play a role of heat dissipation inside the machine body 1, the second rack 12 is in a fish-shaped fluid shape, and is vertically mounted at the left and right ends of the first rack 11 through a first connection portion 16, the shape of the third rack 13 is matched with the second rack 12 and smaller than the size of the second rack 12, the machine body 1 is connected to the first rack 11, the second rack 12 and the third rack 13 through a second connection portion 17, and the first rack 11, the second rack 12 and the third rack 13 are in an integral structure.
The utility model overcomes the defects of insufficient lift, insufficient load, short range, low speed and the like of the existing model airplane. The first propeller 2 and the propeller installation part 6 form an included angle of 90 degrees during take-off, under the cooperation of the second propeller 3, take-off and landing are very stable, after the aircraft is lifted off, the first propeller 2 and the propeller installation part 6 are converted into an included angle of 0 degrees, the second propeller 3 stops rotating, lift force is provided by all wings, the first propeller 2 is only responsible for thrust force, so that the aircraft has the advantages of simple take-off and landing, enough load, course and speed, overcomes the defects in the aspect of the load of a model aircraft in the prior art, has certain defects during lifting, has short course and slow speed, and greatly improves the stability when hovering is needed.
In the foregoing, only the preferred embodiment of the present utility model is described, and any minor modifications, equivalent changes and modifications made to the above embodiments according to the technical solutions of the present utility model fall within the scope of the technical solutions of the present utility model.
Claims (4)
1. Tilting propeller type vertical lift unmanned aerial vehicle that takes photo by plane, its characterized in that: including the frame, install in wing, first screw, horizontal fin and the vertical fin of frame left and right sides, the second screw is installed to the rear end of frame, wherein:
the wing is arranged on the front side of the middle part of the frame and comprises a main wing and an auxiliary wing, the main wing is connected with the frame, the auxiliary wing is movably connected to the rear end of the main wing, and the auxiliary wing and the main wing are mutually matched to play roles of deflecting left and right and lifting the frame;
a propeller installation part extending forwards is arranged on a main wing close to the frame, the first propeller is movably installed at the front end of the propeller installation part and can form an included angle of 0 ︒ -90 degrees relative to the upward movement of the propeller installation part, so that the effect of vertically lifting or horizontally continuing the frame is realized;
the horizontal tail comprises a main horizontal tail and an auxiliary horizontal tail, the main horizontal tail is connected with the frame to play a role in stabilizing the frame in the horizontal direction, and the auxiliary horizontal tail is movably connected to the rear end of the main horizontal tail to lift and drop the frame;
the vertical tail fin is arranged on the inner side of the horizontal tail fin and comprises a vertical stable tail fin and a rudder, wherein the vertical stable tail fin is vertically and fixedly arranged on the stand, so that the stand has static stability in the left-right yaw direction, and the rudder is movably and vertically arranged at the rear end of the vertical stable tail fin so as to control the left-right deflection of the stand;
the second screw is vertically arranged at the front ends of the horizontal tail wing and the vertical tail wing and is used for assisting the first screw to enable the rack to vertically lift.
2. The tilting propeller type vertical lifting aerial photographing unmanned aerial vehicle according to claim 1, wherein: the periphery of the frame is provided with a machine body, the machine body is matched with the shape of the frame, and the main wing, the propeller installation part, the main horizontal tail wing, the vertical stabilizing tail wing and the second propeller are connected with the machine body.
3. The tilting propeller type vertical lift aerial photographing unmanned aerial vehicle according to claim 2, wherein: the shape of the machine body is any one of a disc type, a circle type, a gyro type, a flying saucer type, a fan type, a spiral type or a light cluster type.
4. A tilting propeller type vertical lift aerial photo unmanned aerial vehicle according to claim 3, wherein: the frame includes the first frame that parallel ground set up, second frame and the third frame that perpendicular to first frame left and right sides set up, first frame shape and fuselage assorted, the front end is equipped with a plurality of bar through-holes, and the rear end is equipped with a plurality of first circular through-holes, the second frame is fish-shaped fluid bodily form, installs in the left and right sides both ends of first frame through first connecting portion is vertical, the shape and the second frame assorted of third frame, and be less than the size of second frame, connect in the left and right sides both ends of second frame through second connecting portion, the fuselage is connected in first frame, second frame and third frame.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222473618.2U CN219134497U (en) | 2022-09-19 | 2022-09-19 | Tilting propeller type vertical lifting aerial unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222473618.2U CN219134497U (en) | 2022-09-19 | 2022-09-19 | Tilting propeller type vertical lifting aerial unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219134497U true CN219134497U (en) | 2023-06-06 |
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ID=86565376
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222473618.2U Active CN219134497U (en) | 2022-09-19 | 2022-09-19 | Tilting propeller type vertical lifting aerial unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219134497U (en) |
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2022
- 2022-09-19 CN CN202222473618.2U patent/CN219134497U/en active Active
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