CN219447313U - Clip for remote control aircraft convenient to installation - Google Patents

Clip for remote control aircraft convenient to installation Download PDF

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Publication number
CN219447313U
CN219447313U CN202320576966.4U CN202320576966U CN219447313U CN 219447313 U CN219447313 U CN 219447313U CN 202320576966 U CN202320576966 U CN 202320576966U CN 219447313 U CN219447313 U CN 219447313U
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CN
China
Prior art keywords
clip
remote control
fixedly connected
control aircraft
transverse plate
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CN202320576966.4U
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Chinese (zh)
Inventor
赵增旭
张力
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Xiamen Hna General Aviation Technology Co ltd
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Xiamen Hna General Aviation Technology Co ltd
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Priority to CN202320576966.4U priority Critical patent/CN219447313U/en
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    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction

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Abstract

The utility model discloses a clip for a remote control aircraft, which is convenient to install and belongs to the field of unmanned aerial vehicle equipment.

Description

Clip for remote control aircraft convenient to installation
Technical Field
The utility model relates to the field of unmanned aerial vehicle equipment, in particular to a clip for a remote control aircraft, which is convenient to install.
Background
The clip aircraft adopts the clip to directly clamp and fix the operation generally, then drives fixed article through chip control aircraft and fly the operation, and current aircraft clip for building blocks toy is when installing, at first needs to carry out corresponding adjustment with the clip to make the clip can fix the operation with fixed mounting's structure respectively when carrying out the installation operation, but can't carry out different clamping dynamics adjustment operation according to the different circumstances of user's installation when carrying out the installation operation.
Disclosure of Invention
The utility model aims to provide a clip for a remote control aircraft, which is convenient to install, so as to solve the problem that the adjustment of the clamping force cannot be carried out according to different situations of installation of a user when the installation operation is carried out.
In order to achieve the above purpose, the present utility model provides the following technical solutions:
the utility model provides a clip for remote control aircraft convenient to installation, is including connecting the diaphragm, it runs through to have seted up in the middle part of connecting the diaphragm outer wall and changes the hole, it is connected with the clip to change the downthehole rotation, it is provided with and connects perpendicular piece to connect the diaphragm outside, connect the inboard fixed connection of diaphragm in the bottom of installation piece, the installation piece is inside to be the cavity setting, be provided with the motor in the installation piece, connect building blocks part junction through connecting the diaphragm, make the clip can carry out different clamp according to the demand of difference and get dynamics regulation under the regulation effect of clip and connection perpendicular piece to realize flight operation under the effect of motor and wing.
As a further scheme of the utility model: the connecting transverse plate is characterized in that a sliding groove is formed in the middle of the upper end of the outer side of the connecting transverse plate, a plurality of limiting holes are uniformly formed in the middle of the bottom end of the sliding groove, sliding adjustment and limiting installation operation of the sliding block are realized through the sliding groove, and the limiting holes provide limiting and fixing effects when the connecting vertical block slides.
As still further aspects of the utility model: the connecting vertical block is characterized in that the bottom end of the connecting vertical block is fixedly connected with a sliding block, the sliding block slides in a sliding groove, a plurality of inserting openings are uniformly formed in the outer side of the connecting vertical block, inserting holes are formed in the middle of the upper end of the connecting vertical block, corresponding to the matched limiting holes, inserting rods are inserted into the inserting holes, the inserting limiting connection with the clips is realized through the inserting openings, the inserting rods are inserted into the corresponding matched limiting holes under the action of the inserting rods and the inserting holes, and the limiting adjustment and fixing effects of the connecting vertical block are completed.
As still further aspects of the utility model: install the piece upper end symmetry and offered the installation room, two the equal fixedly connected with of installation room inner wall is first spring, two equal fixedly connected with in stopper inner wall middle part in first spring outer wall top, two the stopper is all inserted and is established to be connected in corresponding matched socket, two the socket symmetry is offered in spacing lid both sides, realizes carrying out spacing fixed operation to installation piece internally mounted's battery and motor through spacing lid, realizes when spacing lid carries out the installation operation under the effect of stopper elastic potential energy, the butt is in the stopper upper end for the stopper slides in the installation room, thereby accomplishes the spacing operation of stopper to the socket, when dismantling, only need inwards press the stopper to make the stopper release and the socket insert establish the connection, can dismantle fast.
As still further aspects of the utility model: the installation piece inner wall middle part fixedly connected with second spring, second spring upper end top fixed connection is in butt board bottom middle part, under the effect of second spring elastic potential energy, one of them can make better and the motor realization electric connection of battery, and its second can make battery and motor realize quick rising under the effect of second spring elastic potential energy when dismantling, conveniently take.
As still further aspects of the utility model: the battery has been placed to butt board upper end, battery upper end electric connection has the motor, motor top fixedly connected with wing provides electric power for the motor through the battery, realizes the rotation operation of motor to drive the wing and rotate, realize the flight function.
Compared with the prior art, the utility model has the beneficial effects that:
1. according to the utility model, the upper end of the part to be connected is abutted with the bottom end of the connecting transverse plate, then the clamp is clamped by the rotating hole clamp, the inserting opening is well clamped outside the clamp under the sliding limiting effect of the sliding block and the sliding groove, after the fixing effect is finished, the inserting hole is penetrated through by pressing the inserting rod, so that the clamp is further fixed, the installation is convenient, different clamping size adjustment operations can be carried out according to the requirement, and the stability of the device is effectively improved.
2. According to the utility model, the battery and the motor which are internally installed in the installation block are subjected to limiting and fixing operation through the limiting cover, when the limiting cover is subjected to installation operation under the action of elastic potential energy of the limiting block, the limiting cover is abutted against the upper end of the limiting block, so that the limiting block slides into the installation chamber, the limiting operation of the limiting block on the socket is completed, and when the socket needs to be disassembled, the limiting block is only required to be pressed inwards to release the inserting connection with the socket, so that the socket can be disassembled quickly.
Drawings
FIG. 1 is a schematic diagram of the structure of the present utility model;
FIG. 2 is a schematic view of the structure of the connecting cross plate assembly of the present utility model;
FIG. 3 is a schematic view of the construction of the mounting block assembly of the present utility model;
fig. 4 is an enlarged schematic view of the structure of fig. 3A according to the present utility model.
In the figure: 1. a connecting transverse plate; 110. a turning hole; 111. a chute; 112. a limiting hole; 120. a clip; 121. a slide block; 122. connecting the vertical blocks; 123. an inserting port; 124. a jack; 125. a rod; 2. a mounting block; 210. a mounting chamber; 211. a first spring; 212. a limiting block; 213. a second spring; 214. an abutting plate; 215. a battery; 216. a motor; 217. a limit cover; 218. a socket; 219. and (3) a wing.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to fig. 1-4, when the connection operation is performed, the upper end of the part to be connected is abutted against the bottom end of the connection transverse plate 1, then after the clamping operation is performed by the hole rotating clamp 120, the insertion opening 123 is well clamped outside the clamp 120 under the sliding limiting action of the sliding block 121 and the sliding chute 111, after the fixing action is completed, the insertion hole 124 is inserted into the corresponding matched limiting hole 112 by pressing the insertion rod 125, so that the clamping operation of the clamp 120 is further fixed, the installation is convenient, different clamping size adjustment operations can be performed as required, and the stability of the device is effectively improved.
In the second embodiment, referring to fig. 1 to 4, when the motor 216 is installed, the battery 215 and the motor 216 mounted inside the installation block 2 are limited and fixed by the limiting cover 217, and when the limiting cover 217 is installed under the action of elastic potential energy of the limiting block 212, the limiting cover 217 is abutted against the upper end of the limiting block 212, so that the limiting block 212 slides into the installation chamber 210, and the limiting operation of the limiting block 212 on the socket 218 is completed, and when the motor is required to be disassembled, the limiting block 212 is only required to be pressed inwards, so that the limiting block 212 is disconnected from the socket 218.
Referring to fig. 1 to 4, in the embodiment of the utility model, a clip for a remote control aircraft convenient to install comprises a connection transverse plate 1, a rotation hole 110 is formed in the middle of the outer wall of the connection transverse plate 1 in a penetrating manner, a clip 120 is connected in the rotation hole 110 in a rotating manner, a connection vertical block 122 is arranged on the outer side of the connection transverse plate 1, the inner side of the connection transverse plate 1 is fixedly connected to the bottom end of a mounting block 2, the inside of the mounting block 2 is hollow, a motor 216 is arranged in the mounting block 2, the connection position of building block parts is connected through the connection transverse plate 1, and the clip 120 can adjust different clamping forces according to different requirements under the adjusting action of the clip 120 and the connection vertical block 122, so that flying operation is realized under the actions of the motor 216 and a wing 219.
Wherein, the middle part of the outer side upper end of the connecting transverse plate 1 is provided with a chute 111, the middle part of the bottom end of the chute 111 is uniformly provided with a plurality of limiting holes 112, the sliding adjustment and the limiting installation operation of the sliding block 121 are realized by arranging the chute 111, and the limiting holes 112 are arranged to provide limiting and fixing functions when the connecting vertical block 122 slides.
Wherein, connect perpendicular piece 122 bottom fixedly connected with slider 121, slider 121 slides in spout 111, connects perpendicular piece 122 outside and evenly has seted up a plurality of mouths 123 of inserting, connects perpendicular piece 122 upper end middle part and corresponds and match spacing hole 112 department and offer jack 124, jack 124 inserts and establishes and be connected with inserted bar 125, realizes inserting limit connection with clip 120 through inserting mouthful 123, realizes under the effect of inserted bar 125 and jack 124 that inserted bar 125 inserts the limit and is in corresponding matched spacing hole 112, accomplishes the spacing regulation fixed action of connecting perpendicular piece 122.
Wherein, installation room 210 has been seted up to installation piece 2 upper end symmetry, the equal fixedly connected with first spring 211 of two installation room 210 inner walls, two equal fixedly connected with in stopper 212 inner wall middle parts in two first spring 211 outer wall tops, two stopper 212 are all inserted and are established in corresponding matched socket 218, two sockets 218 symmetry are seted up in spacing lid 217 both sides, realize carrying out spacing fixed operation to installation piece 2 internally mounted's battery 215 and motor 216 through spacing lid 217, realize when spacing lid 217 carries out the installation operation under the effect of stopper 212 elastic potential energy, the butt is in stopper 212 upper end, make stopper 212 slide in to installation room 210, thereby accomplish the spacing operation of stopper 212 to socket 218, when dismantling as required, only inwards press stopper 212 makes stopper 212 release the interpolation of inserting with socket 218 and establish the connection, can dismantle fast.
Wherein, installation piece 2 inner wall middle part fixedly connected with second spring 213, second spring 213 upper end top fixed connection is in butt board 214 bottom middle part, under the effect of second spring 213 elastic potential energy, one can make battery 215 better realize electric connection with motor 216, and two can make battery 215 and motor 216 realize quick rising under the effect of second spring 213 elastic potential energy when dismantling, conveniently take.
Wherein, battery 215 has been placed to butt plate 214 upper end, and battery 215 upper end electric connection has motor 216, and motor 216 top fixedly connected with wing 219 provides electric power for motor 216 through battery 215, realizes the rotation operation of motor 216 to drive wing 219 and rotate, realize the flight function.
The working principle of the utility model is as follows: after the upper end of a part to be connected is abutted with the bottom end of the connecting transverse plate 1, and then the rotating hole clamp 120 realizes clamping operation, the inserting opening 123 is well clamped outside the clamp 120 under the sliding limiting action of the sliding block 121 and the sliding groove 111, after the fixing action is finished, the inserting hole 124 is inserted into the corresponding matched limiting hole 112 by pressing the inserting rod 125, further fixing of the clamping operation of the clamp 120 is finished, limiting fixing operation of the battery 215 and the motor 216 mounted inside the mounting block 2 is realized through the limiting cover 217, when the limiting cover 217 is realized under the action of elastic potential energy of the limiting block 212 to perform mounting operation, the limiting cover 212 is abutted against the upper end of the limiting block 212, so that the limiting block 212 slides into the mounting chamber 210, and then the limiting operation of the inserting opening 218 by the limiting block 212 is finished, and then flying operation is performed through chip operation.
The present utility model is not limited to the above-mentioned embodiments, and any person skilled in the art, based on the technical solution of the present utility model and the inventive concept thereof, can be replaced or changed within the scope of the present utility model.

Claims (6)

1. Clip for remote control aircraft convenient to installation, including connecting diaphragm (1), its characterized in that: the connecting transverse plate (1) is characterized in that a rotating hole (110) is formed in the middle of the outer wall of the connecting transverse plate (1) in a penetrating mode, a clamp (120) is rotationally connected to the rotating hole (110), a connecting vertical block (122) is arranged on the outer side of the connecting transverse plate (1), the inner side of the connecting transverse plate (1) is fixedly connected to the bottom end of the mounting block (2), the inside of the mounting block (2) is provided with a hollow structure, and a motor (216) is arranged in the mounting block (2).
2. The clip for a remote control aircraft for easy installation according to claim 1, wherein: the middle part of the upper end of the outer side of the connecting transverse plate (1) is provided with a sliding groove (111), and the middle part of the bottom end of the sliding groove (111) is uniformly provided with a plurality of limiting holes (112).
3. The clip for a remote control aircraft for easy installation according to claim 1, wherein: the connecting vertical block (122) bottom fixedly connected with slider (121), slider (121) slip is in spout (111), a plurality of mouths (123) of inserting have evenly been seted up in connecting vertical block (122) outside, jack (124) have been seted up in connecting vertical block (122) upper end middle part correspondence matching spacing hole (112) department, jack (124) are inserted and are connected with inserted bar (125).
4. The clip for a remote control aircraft for easy installation according to claim 1, wherein: install piece (2) upper end symmetry and offered installation room (210), two installation room (210) inner wall is all fixedly connected with first spring (211), two equal fixedly connected with in stopper (212) inner wall middle part in first spring (211) outer wall top, two stopper (212) are all inserted and are established to be connected in corresponding matched socket (218), two socket (218) symmetry are offered in spacing lid (217) both sides.
5. The clip for a remote control aircraft for easy installation according to claim 1, wherein: the middle part of the inner wall of the mounting block (2) is fixedly connected with a second spring (213), and the top of the upper end of the second spring (213) is fixedly connected with the middle part of the bottom end of the abutting plate (214).
6. The clip for a remote control aircraft for easy installation according to claim 5, wherein: the battery (215) is placed at the upper end of the abutting plate (214), a motor (216) is electrically connected to the upper end of the battery (215), and a wing (219) is fixedly connected to the top end of the motor (216).
CN202320576966.4U 2023-03-22 2023-03-22 Clip for remote control aircraft convenient to installation Active CN219447313U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202320576966.4U CN219447313U (en) 2023-03-22 2023-03-22 Clip for remote control aircraft convenient to installation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202320576966.4U CN219447313U (en) 2023-03-22 2023-03-22 Clip for remote control aircraft convenient to installation

Publications (1)

Publication Number Publication Date
CN219447313U true CN219447313U (en) 2023-08-01

Family

ID=87387998

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202320576966.4U Active CN219447313U (en) 2023-03-22 2023-03-22 Clip for remote control aircraft convenient to installation

Country Status (1)

Country Link
CN (1) CN219447313U (en)

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