CN211786773U - Unmanned aerial vehicle hovers positioner of flight training - Google Patents

Unmanned aerial vehicle hovers positioner of flight training Download PDF

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Publication number
CN211786773U
CN211786773U CN202020903010.7U CN202020903010U CN211786773U CN 211786773 U CN211786773 U CN 211786773U CN 202020903010 U CN202020903010 U CN 202020903010U CN 211786773 U CN211786773 U CN 211786773U
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CN
China
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fixedly connected
wall
unmanned aerial
aerial vehicle
gear
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Expired - Fee Related
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CN202020903010.7U
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Chinese (zh)
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冯鲁红
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Individual
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Individual
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Abstract

The utility model discloses an unmanned aerial vehicle hovers positioner of flight training, the utility model relates to an unmanned aerial vehicle technique flight technical field. Top and bottom roll connection in the protective glass wall have the both ends of hob, the internal connection of hob has micro motor's outer wall, the both ends of the transparent transmission band of outer wall fixedly connected with of hob, the internal connection of transparent transmission band has the cotton outer wall of absorption, the one end of the inside roll connection gear of rotation shell, the other end fixedly connected with of gear rotates the one end of outrigger, the bottom swing joint of gear has the one end of piece, the one end of one side fixedly connected with button of piece, the inside of the first spring one end of outside fixedly connected with of button, the micro motor inside starting the hob lets the outer rainwater of the cotton clearance protective glass of absorption on the transparent transmission band, start and rotate the outrigger, it drives gear revolve to make and rotate the outrigger, the gear is letting the locator body raise the angle upwards, make the transmission coordinate that the locator body can be clear.

Description

Unmanned aerial vehicle hovers positioner of flight training
Technical Field
The utility model relates to an unmanned aerial vehicle skill technical field that flies specifically is an unmanned aerial vehicle hovers positioner of flight training.
Background
Unmanned aircraft, commonly known as: unmanned planes, unmanned aerial vehicles, unmanned combat airplanes, and bee-type machines; the airplane is a wide-range remote control aircraft which does not need a driver to board and pilot, and generally refers to an unmanned reconnaissance airplane in the military, an unmanned plane and an airplane without a cockpit, but is provided with an autopilot, a program control device and other equipment. Personnel on the ground, a naval vessel or a mother aircraft remote control station track, position, remote control, remote measurement and digital transmission through equipment such as a radar, and when the unmanned aerial vehicle is hovered and trained, a ground positioner is often needed to suspend a position coordinate for the unmanned aerial vehicle, so that the position is positioned.
Unmanned aerial vehicle positioning device who uses at present, when rainy use, most unmanned aerial vehicle positioning device can't give unmanned aerial vehicle with coordinate signal transmission in rainy ground because of not having waterproof function to lead to unmanned aerial vehicle positioning device, the rainwater leads to unmanned aerial vehicle positioning device inner line short circuit even, or unmanned aerial vehicle positioning device decides can't nimble use under the unstable condition of relief, for this reason, technical personnel in the field have provided the positioner of unmanned aerial vehicle flight training that hovers.
SUMMERY OF THE UTILITY MODEL
Not enough to prior art, the utility model provides an unmanned aerial vehicle hovers positioner of flight training has solved unmanned aerial vehicle positioning device and can't give unmanned aerial vehicle or unmanned aerial vehicle positioning device and decide the problem that can't use in a flexible way under the unstable condition of relief for coordinate signal transmission in the rain ground.
In order to achieve the above purpose, the utility model discloses a following technical scheme realizes: the utility model provides an unmanned aerial vehicle hovers positioner of flight training, includes the locator body, the outside fixedly connected with protection machanism's of locator body one end, the inside of connection structure is rotated to the both sides swing joint of locator body, protection machanism includes protective housing, one side of protective housing one end fixedly connected with safety goggles, top and bottom roll connection in the safety goggles wall have the both ends of roller bar, the inside fixedly connected with micro motor's of roller bar outer wall, micro motor's output shaft fixedly connected with safety goggles's inner wall, the both ends of the transparent transmission band of outer wall fixedly connected with of roller bar, the inside fixedly connected with of transparent transmission band adsorbs cotton outer wall, there is protective housing's the other end outside of locator body through bolt threaded connection, and the junction is equipped with the sealing washer.
The rotating connection structure comprises a rotating shell, one end of an internal rolling connection gear of the rotating shell is connected with one end of a rotating outer frame, the other end of the gear is fixedly connected with one end of a blocking block, one end of a button is fixedly connected with one side of the blocking block, the inside of one end of a first spring of the external fixedly connected with of the button is connected with one end of a rotating outer frame, the inner wall of the rotating shell is fixedly connected with the other end of the first spring, the other end of the button penetrates through the outer wall of the rotating shell, one end of a connecting rod is fixedly connected with the bottom of the rotating shell, the inner wall of one end of a second spring of the connecting rod penetrates through one side of the rotating platform, and the inner wall of the rotating platform is fixedly connected with.
Preferably, the inside both sides roll connection of locator body has the inner wall that rotates the shell, the bottom fixedly connected with that rotates the shell inner wall rotates the outside of platform, the bottom roll connection of platform has the top of supporting link, the bottom fixedly connected with of supporting link fixes the top of foot rest.
Preferably, one side of the protective shell is provided with a rotary connecting block, the inside of the rotary connecting block is fixedly connected with the outside of the positioner body, one side of the rotary connecting block is provided with a handle, and the inside of the handle is fixedly connected with the outside of the positioner body.
Preferably, the inside of the rotating shell at the other side of the rotating platform is fixedly connected with the outside of the bearing.
Preferably, the axle center of gear is coaxial with the axle center of bearing, the outside of connecting the rotation connecting block is all laminated to the inside of gear and the inside of bearing.
Preferably, the inner distance of the rotary connecting structure is matched with the width of the positioner body.
Advantageous effects
The utility model provides an unmanned aerial vehicle hovers positioner of flight training. Compared with the prior art, the method has the following beneficial effects:
1. a positioning device for hovering flight training of an unmanned aerial vehicle comprises a protective shell, one end of the protective shell is fixedly connected with one side of a protective mirror, the top and the bottom in the wall of the protective mirror are connected with two ends of a rolling rod in a rolling manner, the inner part of the rolling rod is fixedly connected with the outer wall of a micro motor, an output shaft of the micro motor is fixedly connected with the inner wall of the protective mirror, the outer wall of the rolling rod is fixedly connected with two ends of a transparent transmission belt, the inner part of the transparent transmission belt is fixedly connected with an outer wall for absorbing cotton, the outer part of a positioner body is connected with the other end of the protective shell through bolt threads, and, when the locator body is used in rainy days, one end of the protective shell is connected with the outer wall of the locator body through a bolt, the micro motor inside the starting rolling rod enables the absorption cotton on the transparent transmission band to clean rainwater outside the protective glasses, so that the locator body can clearly transmit coordinates.
2. A positioning device for unmanned aerial vehicle hovering flight training comprises a rotating shell, wherein the rotating shell is connected with one end of a gear in a rolling mode through a rotating connecting structure, the other end of the gear is fixedly connected with one end of a rotating outer frame, the bottom of the gear is movably connected with one end of a block, one side of the block is fixedly connected with one end of a button, the outside of the button is fixedly connected with the inside of one end of a first spring, the other end of the first spring is fixedly connected with the inner wall of the rotating shell, the other end of the button penetrates through the outer wall of the rotating shell, the bottom of the rotating shell is fixedly connected with one end of a connecting rod, the other end of the connecting rod penetrates through one side of a rotating platform and is fixedly connected with the inner wall of one end of a second spring, the other end of the second spring is fixedly connected with the inner wall of a rotating platform, the rotating, rotate the outrigger in the start, make to rotate the outrigger and drive gear revolve, the gear is letting the locator body raise the angle upwards, lets the locator body give unmanned aerial vehicle position location coordinate.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a front view of the protection mechanism of the present invention;
FIG. 3 is a front view of the inside of the rotary connection structure of the present invention;
fig. 4 is a right side view of the inside of the rotary connection structure of the present invention.
In the figure: 1. a locator body; 2. a protection mechanism; 21. a protective housing; 22. protective glasses; 23. rolling a rod; 24. a micro motor; 25. a transparent transfer belt; 26. adsorbing cotton; 27. rotating the connecting block; 28. a grip; 3. a rotating connection structure; 31. rotating the housing; 32. rotating the outer frame; 33. a gear; 34. blocking; 35. a first spring; 36. a connecting rod; 37. a second spring; 38. a bearing; 39. a button; 4. rotating the platform; 5. a support link; 6. and (4) fixing the foot rest.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 2, the present invention provides a technical solution: a positioning device for unmanned aerial vehicle hovering flight training comprises a positioner body 1, one end of a protective mechanism 2 is fixedly connected to the outside of the positioner body 1, two sides of the positioner body 1 are movably connected with the inside of a rotating connection structure 3, the protective mechanism 2 comprises a protective shell 21, one end of the protective shell 21 is fixedly connected with one side of a protective mirror 22, the top and the bottom of the inside of the protective mirror 22 wall are connected with two ends of a rolling rod 23 in a rolling manner, the inside of the rolling rod 23 is fixedly connected with the outer wall of a micro motor 24, an output shaft of the micro motor 24 is fixedly connected with the inner wall of the protective mirror 22, the outer wall of the rolling rod 23 is fixedly connected with two ends of a transparent transmission belt 25, the inside of the transparent transmission belt 25 is fixedly connected with the outer wall of an adsorption cotton 26, the outside of the positioner body 1 is connected with the other end of the protective shell 21 through bolt threads, the inside fixedly connected with locator body 1 of rotation connecting block 27 is outside, and one side of rotating connecting block 27 is equipped with handle 28, and the inside fixedly connected with locator body 1's of handle 28 outside.
Referring to fig. 3-4, the rotating connection structure 3 includes a rotating housing 31, an inner portion of the rotating housing 31 is connected to one end of a gear 33 in a rolling manner, the other end of the gear 33 is fixedly connected to one end of a rotating outer frame 32, the bottom of the gear 33 is movably connected to one end of a stopping block 34, one side of the stopping block 34 is fixedly connected to one end of a button 39, an outer portion of the button 39 is fixedly connected to an inner portion of one end of a first spring 35, the other end of the first spring 35 is fixedly connected to an inner wall of the rotating housing 31, the other end of the button 39 penetrates through an outer wall of the rotating housing 31, the bottom of the rotating housing 31 is fixedly connected to one end of a connecting rod 36, the other end of the connecting rod 36 penetrates through an inner wall of one end of a second spring 37, the other end of the second spring 37 is fixedly connected to an inner wall of the.
Referring to fig. 1, the positioner body 1 has inner walls of a rotating housing 31 connected to the inner sides thereof in a rolling manner, the bottom of the inner wall of the rotating housing 31 is fixedly connected to the outside of a rotating platform 4, the bottom of the rotating platform 4 is connected to the top of a supporting link 5 in a rolling manner, and the bottom of the supporting link 5 is fixedly connected to the top of a fixed foot rest 6.
The axle center of the gear 33 is coaxial with the axle center of the bearing 38, the inside of the gear 33 and the inside of the bearing 38 are both attached to the outside of the rotary connecting block 27, and the inner distance of the rotary connecting structure 3 is matched with the width of the positioner body 1.
When the positioning device is used, firstly, the support connecting rod 5 and the fixed foot stool 6 are fixedly connected with the bottom of the rotating platform 4 and are supported with the ground, the positioner body 1 is started, the rotating shell 31 on one side of the rotating platform 4 is pulled outwards, when the positioner body 1 can be put down at the inner side of the rotating connecting structure 3, the rotating connecting blocks 27 on two sides of the positioner body 1 are put into the gear 33 and the shaft core of the bearing 38 in the rotating shell 31 on two sides of the rotating platform 4, the rotating shell 31 on one side of the rotating platform 4 is loosened, the inner part of the rotating shell 31 is more attached to the outer part of the positioner body 1 under the action of the elastic force of the second spring 37, the rotating outer frame 32 is started to drive the gear 33 to rotate, the gear 33 is lifted upwards by the angle of the positioner body 1, the positioner body 1 positions and coordinates the position of the unmanned aerial vehicle, and after the position is fixed, one end of the resistance block 34 fixes the gear 33 in the gear 33, if when the locator body 1 is turned down, the button 39 is pressed to separate one end of the blocking block 34 from the gear 33, the locator body 1 is turned down by the rotating outer frame 32 when being started, or the locator body 1 is used under the condition that the terrain is unstable, the locator body 1 can be taken out from the inside of the rotating connecting structure 3, the handles 28 on two sides of the locator body 1 are held by hands, the angle of the locator body 1 is manually adjusted, when the locator body 1 is used in rainy days, one end of the protective shell 21 is connected with the outer wall of the locator body 1 through a bolt, the micro motor 24 in the rolling rod 23 is started to enable the adsorption cotton 26 on the transparent transmission belt 25 to clean rainwater outside the protective mirror 22, and the locator body 1 can clearly transmit coordinates.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims (6)

1. The utility model provides an unmanned aerial vehicle hover flight training's positioner, includes locator body (1), its characterized in that: the outside fixedly connected with protection machanism (2)'s of locator body (1) one end, the inside of both sides swing joint rotation connection structure (3) of locator body (1), protection machanism (2) includes protecting sheathing (21), one side of protecting sheathing (21) one end fixedly connected with protecting mirror (22), top and bottom roll connection in protecting mirror (22) wall has the both ends of roller bar (23), the inside fixedly connected with micro motor's (24) outer wall of roller bar (23), the output shaft fixedly connected with protecting mirror's (22) inner wall of micro motor (24), the outer wall fixedly connected with transparent transmission band's (25) both ends of roller bar (23), the inside fixedly connected with of transparent transmission band (25) adsorbs the outer wall of cotton (26), the outside of locator body (1) has the other end of protecting sheathing (21) through bolt threaded connection, and the joint is provided with a sealing ring;
the rotary connecting structure (3) comprises a rotary shell (31), one end of a gear (33) is connected with the inner rolling of the rotary shell (31), the other end of the gear (33) is fixedly connected with one end of a rotary outer frame (32), one end of a blocking block (34) is movably connected with the bottom of the gear (33), one end of a button (39) is fixedly connected with one side of the blocking block (34), the inner part of one end of a first spring (35) is fixedly connected with the outer part of the button (39), the other end of the first spring (35) is fixedly connected with the inner wall of the rotary shell (31), the other end of the button (39) penetrates through the outer wall of the rotary shell (31), one end of a connecting rod (36) is fixedly connected with the bottom of the rotary shell (31), the other end of the connecting rod (36) penetrates through the inner wall of one end of a second spring (37) fixedly connected with one side of the rotary platform (4), the other end of the second spring (37) is fixedly connected with the inner wall of the rotating platform (4).
2. The positioning device for unmanned aerial vehicle hovering flight training according to claim 1, wherein: the interior both sides roll connection of locator body (1) has the inner wall that rotates shell (31), the outside of the bottom fixedly connected with rotation platform (4) of rotation shell (31) inner wall, the bottom roll connection of rotation platform (4) has the top of supporting rod (5), the top of the fixed foot rest of bottom fixedly connected with (6) of supporting rod (5).
3. The positioning device for unmanned aerial vehicle hovering flight training according to claim 1, wherein: one side of protective housing (21) is equipped with rotates connecting block (27), the outside of the inside fixedly connected with locator body (1) of rotating connecting block (27), one side of rotating connecting block (27) is equipped with handle (28), the outside of the inside fixedly connected with locator body (1) of handle (28).
4. The positioning device for unmanned aerial vehicle hovering flight training according to claim 2, wherein: the inside of the rotating shell (31) at the other side of the rotating platform (4) is fixedly connected with the outside of a bearing (38).
5. The positioning device for unmanned aerial vehicle hovering flight training according to claim 4, wherein: the axis of the gear (33) is coaxial with the axis of the bearing (38), and the inside of the gear (33) and the inside of the bearing (38) are both attached to the outside of the rotary connecting block (27).
6. The positioning device for unmanned aerial vehicle hovering flight training according to claim 1, wherein: the inner side distance of the rotary connecting structure (3) is matched with the width of the positioner body (1).
CN202020903010.7U 2020-05-25 2020-05-25 Unmanned aerial vehicle hovers positioner of flight training Expired - Fee Related CN211786773U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202020903010.7U CN211786773U (en) 2020-05-25 2020-05-25 Unmanned aerial vehicle hovers positioner of flight training

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202020903010.7U CN211786773U (en) 2020-05-25 2020-05-25 Unmanned aerial vehicle hovers positioner of flight training

Publications (1)

Publication Number Publication Date
CN211786773U true CN211786773U (en) 2020-10-27

Family

ID=72956104

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202020903010.7U Expired - Fee Related CN211786773U (en) 2020-05-25 2020-05-25 Unmanned aerial vehicle hovers positioner of flight training

Country Status (1)

Country Link
CN (1) CN211786773U (en)

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CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20201027

Termination date: 20210525

CF01 Termination of patent right due to non-payment of annual fee