CN215285252U - Many rotor unmanned aerial vehicle horn quick assembly disassembly device - Google Patents
Many rotor unmanned aerial vehicle horn quick assembly disassembly device Download PDFInfo
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- CN215285252U CN215285252U CN202023278216.4U CN202023278216U CN215285252U CN 215285252 U CN215285252 U CN 215285252U CN 202023278216 U CN202023278216 U CN 202023278216U CN 215285252 U CN215285252 U CN 215285252U
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- pipe clamp
- fixing plate
- aerial vehicle
- unmanned aerial
- horn
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Abstract
The utility model discloses a many rotor unmanned aerial vehicle horn quick assembly disassembly device, include from last pipe clamp of connecting extremely down in order, the lower pipe clamp, the gasket, the lower pipe clamp comprises 2 group's chucking structures, the chucking structure includes an upper fixed plate, the bottom plate, an upper fixed plate, the bottom plate is the vertical rectangular plate of placing, the complete open-ended semi-circular passageway in bottom has been seted up to an upper fixed plate's bottom, the complete open-ended semi-circular passageway in top has been seted up at a bottom fixed plate's top, an upper fixed plate is connected with the bottom plate and is made an upper fixed plate's semi-circular passageway and the complete circular passageway of semi-circular passageway combination formation of bottom plate, two sets of chucking structures are parallel to each other and are located the both sides of gasket respectively, the circular passageway of two sets of chucking structures is coaxial and isometric. The utility model provides a connection structure between traditional unmanned aerial vehicle horn and the fuselage among the prior art complicated, the quick assembly disassembly horn of being not convenient for, long, the big problem of working strength of dismouting duration.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle horn dismouting device, concretely relates to many rotor unmanned aerial vehicle horn quick assembly disassembly device.
Background
The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. The machine has no cockpit, but is provided with an automatic pilot, a program control device and other equipment. The aircraft can take off like a common airplane under the radio remote control or launch and lift off by a boosting rocket, and can also be thrown into the air by a mother aircraft for flying. During recovery, the aircraft can land automatically in the same way as the common aircraft landing process, and can also be recovered by a parachute or a barrier net for remote control. Can be repeatedly used for many times. The method is widely used for aerial photography, communication, electronic interference and the like.
Traditional unmanned aerial vehicle wants to dismantle the back and carry out fuselage, horn inspection or vanning and place, will carry out complicated dismantlement operation, and the connection structure between horn and the fuselage is complicated, and quick assembly disassembly horn of not being convenient for, the dismouting is long consuming time, and working strength is big.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the technical problem that connection structure between traditional unmanned aerial vehicle horn and the fuselage is complicated, the quick assembly disassembly horn of being not convenient for, the dismouting is long consuming time, and working strength is big, and aim at provides a many rotor unmanned aerial vehicle horn quick assembly disassembly device, solves above-mentioned problem.
The utility model discloses a following technical scheme realizes:
a multi-rotor unmanned aerial vehicle arm quick dismounting device comprises an upper pipe clamp, a lower pipe clamp and a gasket which are sequentially connected from top to bottom, wherein the lower pipe clamp is positioned below the upper pipe clamp, the gasket is positioned below the lower pipe clamp, a through hole for the unmanned aerial vehicle arm to pass through is formed in the upper pipe clamp, the through hole in the upper pipe clamp is coaxial and internally tangent with the unmanned aerial vehicle arm, the lower pipe clamp comprises 2 groups of clamping structures, each clamping structure comprises an upper fixing plate and a lower fixing plate, the upper fixing plate and the lower fixing plate are rectangular plates which are vertically arranged, a semicircular channel with a completely opened bottom is formed in the bottom of the upper fixing plate, a semicircular channel with a completely opened top is formed in the top of the lower fixing plate, the upper fixing plate and the lower fixing plate are connected, so that the semicircular channel of the upper fixing plate and the semicircular channel of the lower fixing plate are combined to form a complete circular channel, and the two groups of clamping structures are parallel to each other and are respectively positioned on two sides of the gasket, the circular channels of the two groups of clamping structures are coaxial and have the same diameter, the machine body sequentially penetrates through the circular channels of the two groups of clamping structures along the axial direction of the machine body, the central shaft of the circular channel of the clamping structure and the central shaft of the upper pipe clamp through hole are translated to be intersected along the vertical direction, and the central shaft of the circular channel of the clamping structure and the central shaft of the upper pipe clamp through hole are intersected to form an included angle of 90 degrees;
the lower fixing plate is vertically connected with the gasket, the upper fixing plate is detachably connected with the lower fixing plate, and the upper fixing plate is vertically connected with the bottom surface of the upper pipe clamp.
The utility model discloses based on traditional unmanned aerial vehicle, increased the connection structure that can quick assembly disassembly between unmanned aerial vehicle horn and fuselage, saved other connection structure's use, the utility model relates to a many rotor unmanned aerial vehicle horn quick assembly disassembly device is the connection structure between horn and fuselage, the utility model relates to a connection structure simple structure, the dismouting is efficient, has solved the connection structure between traditional unmanned aerial vehicle horn and the fuselage among the prior art complicacy, is not convenient for quick assembly disassembly horn, and the dismouting is long consuming time, problem that working strength is big; the utility model discloses be connected fixedly with simple structure's connection structure to horn and fuselage, reduced other connection structure's use amount, under the condition that can fix horn and fuselage, the utility model discloses the dismouting degree of difficulty of unmanned aerial vehicle horn and fuselage has been reduced.
The utility model discloses well upper pipe clamp is used for the centre gripping horn, and the horn is the tubular structure, and the horn is inscribe with the top tube clip, and the outer wall of horn and the inner wall in close contact with of top tube clip through-hole utilize the friction between wall and the wall can fix the horn, and the bottom tube clip is used for fixed fuselage, the utility model discloses form the circular passageway that matches with the fuselage shape between an upper fixed plate and the bottom plate, an upper fixed plate and bottom plate mutually support press from both sides the fuselage tightly between the two, and an upper fixed plate is connected fixedly with the bottom plate and just can realize being connected of horn and fuselage, and during the dismouting, separation an upper fixed plate with down fixed roof can, do not need complicated operation, the utility model relates to a connection structure dismouting is fast.
Go up the U template that the pipe clamp was placed for the level, the through-hole that the confession unmanned aerial vehicle horn of seting up on the pipe clamp is the U type passageway of last pipe clamp, the arcwall face and the laminating of unmanned aerial vehicle horn outer wall of U type passageway, install vertical round pin axle of placing between the last plate of going up the pipe clamp and the lower slab of last pipe clamp, the round pin axle passes the last plate of going up the pipe clamp and the lower slab of last pipe clamp along vertical direction in proper order, the round pin axle can be dismantled through the pinhole with the last plate of last pipe clamp and the lower slab of last pipe clamp and be connected, the unmanned aerial vehicle horn that inserts in the pipe clamp U type passageway is located between round pin axle and the U type passageway arcwall face, round pin axle and unmanned aerial vehicle horn in close contact with.
The utility model discloses the placing means of well U template and the mounting means adaptation of horn, the U type passageway of U template are used for fixed horn, and the round pin axle is used for consolidating the horn, and the arcwall face of round pin axle and U template mutually supports and presss from both sides the horn tightly inside U type passageway, and is fixed firm, and the dismouting of round pin axle is prior art, the utility model discloses do not change the structure of round pin axle and mounting means, directly utilized current round pin axle construction to realize the reinforcement to the horn. The open end of U-shaped board is many, can follow a plurality of open end dismouting horn, the operation of being convenient for.
The upper fixing plate and the lower fixing plate are fixedly connected through bolts. The upper fixing plate and the lower fixing plate need to be repeatedly disassembled and assembled, the bolt is less in abrasion in the repeated disassembling and assembling process compared with a screw, the service life is long, the bolt is easy to obtain on the market, and the disassembling and assembling are convenient.
The lower fixing plate is fixedly connected with the gasket through screws. The upper fixing plate and the gasket do not need to be repeatedly disassembled and assembled, and the screw is firmer compared with the bolt fixing property, but is easily deformed to be incapable of being used after being repeatedly disassembled and assembled.
The upper fixing plate is fixedly connected with the upper pipe clamp through screws.
The top of round pin axle is installed the nut of level and is placed, and the nut is connected with the round pin axle is perpendicular. The nut is fixedly connected with the pin shaft, provides a force application point convenient for operation of operators for the pin shaft, and is convenient to disassemble and assemble.
Compared with the prior art, the utility model, following advantage and beneficial effect have:
1. the utility model relates to a many rotor unmanned aerial vehicle horn quick assembly disassembly device has increased the connection structure that can quick assembly disassembly between unmanned aerial vehicle horn and fuselage, has saved the use of other connection structures, and the dismouting is efficient, and it is complicated to have solved the connection structure between traditional unmanned aerial vehicle horn and the fuselage among the prior art, is not convenient for quick assembly disassembly horn, and the dismouting is long consuming time;
2. the utility model relates to a many rotor unmanned aerial vehicle horn quick assembly disassembly device has further limited the structure of top tube clamp, can consolidate the horn, and fixed firm to the horn, the horn is difficult to drop from the top tube clamp;
3. the utility model relates to a many rotor unmanned aerial vehicle horn quick assembly disassembly device simple structure, connecting piece between each associative structure are bolt or screw, and are with low costs, and the dismouting is simple.
Drawings
The accompanying drawings, which are included to provide a further understanding of the embodiments of the invention and are incorporated in and constitute a part of this application, illustrate embodiment(s) of the invention and together with the description serve to explain the principles of the invention. In the drawings:
FIG. 1 is a schematic structural view of the present invention;
fig. 2 is a schematic view of the present invention.
Reference numbers and corresponding part names in the drawings:
1-upper pipe clamp, 2-lower pipe clamp, 3-gasket, 4-pin shaft, 5-unmanned aerial vehicle arm, 6-nut, 21-upper fixing plate and 22-lower fixing plate.
Detailed Description
To make the objects, technical solutions and advantages of the present invention more apparent, the present invention is further described in detail below with reference to the following examples and drawings, and the exemplary embodiments and descriptions thereof of the present invention are only used for explaining the present invention, and are not intended as limitations of the present invention.
Example 1
As shown in figures 1 and 2, the utility model relates to a multi-rotor unmanned aerial vehicle horn quick dismounting device, which comprises an upper pipe clamp 1, a lower pipe clamp 2 and a gasket 3 which are connected from top to bottom in sequence, wherein the lower pipe clamp 2 is positioned below the upper pipe clamp 1, the gasket 3 is positioned below the lower pipe clamp 2, the upper pipe clamp 1 is provided with a through hole for the unmanned aerial vehicle horn 5 to pass through, the through hole on the upper pipe clamp 1 is coaxial and internally tangent with the unmanned aerial vehicle horn, the lower pipe clamp 2 is composed of 2 groups of clamping structures, the clamping structure comprises an upper fixing plate 21 and a lower fixing plate 22, the upper fixing plate 21 and the lower fixing plate 22 are rectangular plates which are vertically arranged, the bottom of the upper fixing plate 21 is provided with a semicircular channel with a completely opened bottom, the top of the lower fixing plate 22 is provided with a semicircular channel with a completely opened top, the upper fixing plate 21 is connected with the lower fixing plate 22 so that the semicircular channel of the upper fixing plate 21 and the semicircular channel of the lower fixing plate 22 are combined to form a complete circular channel, the two groups of clamping structures are parallel to each other and are respectively positioned at two sides of the gasket 3, the circular channels of the two groups of clamping structures are coaxial and have the same diameter, the machine body sequentially penetrates through the circular channels of the two groups of clamping structures along the axial direction of the machine body, the central shaft of the circular channel of the clamping structure and the central shaft of the through hole of the upper pipe clamp 1 are horizontally moved to be intersected along the vertical direction, and the central shaft of the circular channel of the clamping structure and the central shaft of the through hole of the upper pipe clamp 1 are intersected to form an included angle of 90 degrees;
the lower fixing plate 22 is vertically connected with the gasket 3, the upper fixing plate 21 is detachably connected with the lower fixing plate 22, and the upper fixing plate 21 is vertically connected with the bottom surface of the upper pipe clamp 1.
The upper fixing plate 21 and the lower fixing plate 22 are fixed by bolts. The lower fixing plate 22 is fixed to the spacer 3 by screws. The upper fixing plate 21 is fixed to the upper pipe clamp 1 by screws.
The utility model discloses well upper pipe clamp is used for the centre gripping horn, and the horn is the tubular structure, and the horn is inscribe with the top tube clip, and the outer wall of horn and the inner wall in close contact with of top tube clip through-hole utilize the friction between wall and the wall can fix the horn, and the bottom tube clip is used for fixed fuselage, the utility model discloses form the circular passageway that matches with the fuselage shape between an upper fixed plate and the bottom plate, an upper fixed plate and bottom plate mutually support press from both sides the fuselage tightly between the two, and an upper fixed plate is connected fixedly with the bottom plate and just can realize being connected of horn and fuselage, and during the dismouting, separation an upper fixed plate with down fixed roof can, do not need complicated operation, the utility model relates to a connection structure dismouting is fast.
The utility model discloses be not suitable for all unmanned aerial vehicle models, suitable unmanned aerial vehicle horn, fuselage respectively with the utility model discloses an go up pipe clamp, low pipe clamp shape adaptation.
Example 2
Based on embodiment 1, go up the U template that pipe clamp 1 was placed for the level, the through-hole that supplies the unmanned aerial vehicle horn to pass of seting up on last pipe clamp 1 is the U type passageway of last pipe clamp 1, the arcwall face and the 5 outer wall laminating of unmanned aerial vehicle horn of U type passageway, install vertical round pin axle 4 of placing between the last plate of going up pipe clamp 1 and the lower slab of last pipe clamp 1, round pin axle 4 passes the last plate of last pipe clamp 1 and the lower slab of last pipe clamp 1 along vertical direction in proper order, round pin axle 4 can be dismantled through the pinhole with the last plate of last pipe clamp 1 and be connected, the unmanned aerial vehicle horn that inserts in the 1U type passageway of last pipe clamp is located between round pin axle 4 and the U type passageway arcwall face, round pin axle 4 and 5 in close contact with of unmanned aerial vehicle horn. The top of round pin axle 4 is installed the nut 6 of horizontal placement, and nut 6 is connected with round pin axle 4 is perpendicular.
The U type passageway of U template is used for fixed horn, and the round pin axle is used for consolidating the horn, and the round pin axle is mutually supported with the arcwall face of U template and is pressed from both sides the horn tightly inside U type passageway, and is fixed firm, and the dismouting of round pin axle is prior art, the utility model discloses do not change the structure of round pin axle and mounting means, directly utilized current round pin axle construction to realize the reinforcement to the horn.
The above-mentioned embodiments, further detailed description of the objects, technical solutions and advantages of the present invention, it should be understood that the above description is only the embodiments of the present invention, and is not intended to limit the scope of the present invention, and any modifications, equivalent substitutions, improvements, etc. made within the spirit and principle of the present invention should be included in the scope of the present invention.
Claims (6)
1. A multi-rotor unmanned aerial vehicle horn quick dismounting device is characterized by comprising an upper pipe clamp (1), a lower pipe clamp (2) and a gasket (3) which are sequentially connected from top to bottom, wherein the lower pipe clamp (2) is positioned below the upper pipe clamp (1), the gasket (3) is positioned below the lower pipe clamp (2), a through hole for an unmanned aerial vehicle horn (5) to pass through is formed in the upper pipe clamp (1), the through hole in the upper pipe clamp (1) is coaxial and internally tangent with the unmanned aerial vehicle horn, the lower pipe clamp (2) is composed of 2 groups of clamping structures, each clamping structure comprises an upper fixing plate (21) and a lower fixing plate (22), the upper fixing plate (21) and the lower fixing plate (22) are rectangular plates which are vertically placed, a semicircular channel with a completely opened bottom is formed in the bottom of the upper fixing plate (21), and a semicircular channel with a completely opened top is formed in the top of the lower fixing plate (22), the upper fixing plate (21) is connected with the lower fixing plate (22) so that a semicircular channel of the upper fixing plate (21) and a semicircular channel of the lower fixing plate (22) are combined to form a complete circular channel, the two groups of clamping structures are parallel to each other and are respectively positioned at two sides of the gasket (3), the circular channels of the two groups of clamping structures are coaxial and have the same diameter, the machine body sequentially penetrates through the circular channels of the two groups of clamping structures along the axial direction of the machine body, the central shaft of the circular channel of the clamping structure and the central shaft of the through hole of the upper pipe clamp (1) are horizontally moved to be intersected along the vertical direction, and the central shaft of the circular channel of the clamping structure and the central shaft of the through hole of the upper pipe clamp (1) are intersected to form an included angle of 90 degrees;
the lower fixing plate (22) is vertically connected with the gasket (3), the upper fixing plate (21) is detachably connected with the lower fixing plate (22), and the upper fixing plate (21) is vertically connected with the bottom surface of the upper pipe clamp (1).
2. The device for rapidly dismounting the horn of the multi-rotor unmanned aerial vehicle according to claim 1, wherein the upper pipe clamp (1) is a horizontally arranged U-shaped plate, a through hole formed in the upper pipe clamp (1) and used for the unmanned aerial vehicle horn to pass through is a U-shaped channel of the upper pipe clamp (1), an arc-shaped surface of the U-shaped channel is attached to the outer wall of the unmanned aerial vehicle horn (5), a vertically arranged pin shaft (4) is installed between an upper plate block of the upper pipe clamp (1) and a lower plate block of the upper pipe clamp (1), the pin shaft (4) sequentially passes through the upper plate block of the upper pipe clamp (1) and the lower plate block of the upper pipe clamp (1) along the vertical direction, the pin shaft (4) is detachably connected with the upper plate block of the upper pipe clamp (1) and the lower plate block of the upper pipe clamp (1) through a pin hole, the unmanned aerial vehicle horn inserted into the U-shaped channel of the upper pipe clamp (1) is located between the pin shaft (4) and the arc-shaped channel, and the pin shaft (4) is in close contact with the unmanned aerial vehicle horn (5).
3. The device for quickly dismounting and mounting the horn of a multi-rotor unmanned aerial vehicle according to claim 1, wherein the upper fixing plate (21) and the lower fixing plate (22) are fixed by bolts.
4. The device for quickly dismounting and mounting the horn of a multi-rotor unmanned aerial vehicle according to claim 1, wherein the lower fixing plate (22) is fixed to the gasket (3) through screw connection.
5. The device for quickly dismounting and mounting the horn of the multi-rotor unmanned aerial vehicle according to claim 1, wherein the upper fixing plate (21) is fixedly connected with the upper pipe clamp (1) through screws.
6. The device for quickly dismounting and mounting the horn of the multi-rotor unmanned aerial vehicle according to claim 2, wherein a horizontally placed nut (6) is mounted on the top of the pin (4), and the nut (6) is vertically connected with the pin (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023278216.4U CN215285252U (en) | 2020-12-29 | 2020-12-29 | Many rotor unmanned aerial vehicle horn quick assembly disassembly device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023278216.4U CN215285252U (en) | 2020-12-29 | 2020-12-29 | Many rotor unmanned aerial vehicle horn quick assembly disassembly device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215285252U true CN215285252U (en) | 2021-12-24 |
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ID=79529236
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202023278216.4U Active CN215285252U (en) | 2020-12-29 | 2020-12-29 | Many rotor unmanned aerial vehicle horn quick assembly disassembly device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215285252U (en) |
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2020
- 2020-12-29 CN CN202023278216.4U patent/CN215285252U/en active Active
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