CN212149312U - Unmanned aerial vehicle load quick detach interface arrangement - Google Patents

Unmanned aerial vehicle load quick detach interface arrangement Download PDF

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Publication number
CN212149312U
CN212149312U CN202020432575.1U CN202020432575U CN212149312U CN 212149312 U CN212149312 U CN 212149312U CN 202020432575 U CN202020432575 U CN 202020432575U CN 212149312 U CN212149312 U CN 212149312U
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CN
China
Prior art keywords
base
connector
rod
aerial vehicle
unmanned aerial
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Expired - Fee Related
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CN202020432575.1U
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Chinese (zh)
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不公告发明人
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Shanghai Olawi Network Technology Co ltd
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Shanghai Olawi Network Technology Co ltd
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Priority to CN202020432575.1U priority Critical patent/CN212149312U/en
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Publication of CN212149312U publication Critical patent/CN212149312U/en
Expired - Fee Related legal-status Critical Current
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Abstract

The utility model discloses an unmanned aerial vehicle load quick detach interface arrangement, which comprises a base, the inside of base is equipped with the connector, the bottom rigid coupling of connector has vice interface, the inside bottom rigid coupling of base has main interface, main interface pegs graft with vice interface mutually, the connector is connected with the base through installation mechanism, the front surface center bottom of base is equipped with the rubber strip. This unmanned aerial vehicle load quick detach interface arrangement for the conventional art, has following advantage: through the cooperation between base, connector, vice interface, main interface and the installation mechanism, operating personnel only need insert the inside downward application of force of base with the connector and press, makes to support the pole and accomplish one-way joint with the inserted bar, can accomplish the installation of connector and base, operates comparatively simply and high-efficiently, need not to occupy the space in the base outside to the installation mechanism of connector, then more does benefit to the overall arrangement of unmanned aerial vehicle inner structure.

Description

Unmanned aerial vehicle load quick detach interface arrangement
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle load quick detach interface arrangement.
Background
The unmanned aerial vehicle system comprises aircraft platform system, information acquisition system and ground control system, and the task load subsystem indicates the device that has the specific task function that can accomplish detection, collection and record, help to accomplish the flight purpose, generally includes the device of all kinds of application scenes such as optoelectronic pod, shock attenuation cloud platform, camera, thermal infrared imager to and megaphone, gas detection appearance, jetter, searchlight. These devices only need to install and to satisfy simple work on the unmanned aerial vehicle, reach certain task effect, among the current solution, the flight stability of aircraft receives load module's influence, need manual operation to patrol the line operation, its efficiency can not satisfy the demand of patrolling and examining of a large amount of china far away, in order to improve the efficiency of patrolling and examining, the market will hang multiple load of patrolling and examining, threaded bolt connection's mode has been replaced to the mounting means at present stage, can promote installation efficiency, but its installation mechanism subassembly can occupy more base outside space, then can influence its unmanned aerial vehicle's inner structure overall arrangement, the practicality remains the promotion.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle load quick detach interface arrangement to the mounting means of the present stage that proposes in solving above-mentioned background art has replaced threaded bolt connection's mode, can promote installation effectiveness, but its installation mechanism subassembly can occupy more base outside space, can influence its unmanned aerial vehicle's inner structure overall arrangement then, and practicality remains the promotion problem.
In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle load quick-release interface device comprises a base, wherein a connector is arranged inside the base, an auxiliary insertion port is fixedly connected to the bottom end of the connector, a main insertion port is fixedly connected to the bottom end inside the base, the main insertion port is inserted into the auxiliary insertion port, the connector is connected with the base through an installation mechanism, a rubber strip is arranged at the bottom end of the center of the front surface of the base, and through holes are formed in the left side and the right side of the front surface of the rubber strip;
the mounting mechanism comprises an inserting rod, a cavity, a resisting rod, an extension spring, a gasket, a diamond block, a supporting rod, a transverse cylinder, a pull rope, a groove, a transverse rod, a pin shaft and a pressing plate;
the two inserting rods are fixedly connected to the left side and the right side of the lower surface of the connector respectively, one part of each inserting rod penetrates through the base, the two cavities are formed in the left side and the right side of the inner bottom of the base respectively, the abutting rods are inserted into the top ends of the right sides of the inner portions of the cavities, one part of each abutting rod penetrates through the base and is in one-way clamping connection with the outer walls of the inserting rods, the outer sides of the outer walls of the abutting rods are sleeved with extension springs, the inner side end portions of the extension springs are fixedly connected with the inner walls of the cavities, the outer side end portions of the extension springs are fixedly connected with gaskets, the right surfaces of the gaskets are fixedly connected with the left side end portions of the abutting rods, the centers of the inner portions of the cavities are provided with diamond-shaped blocks, supporting rods are fixedly connected to the centers of the front and back surfaces of the diamond-shaped blocks, the, the right side end of the pull rope is fixedly connected with the gasket, the two grooves are respectively formed in the bottom ends of the left side and the right side of the base, a cross rod is inserted into the inner side of each groove, a part of the cross rod penetrates through the base and is connected with the bottom end of the diamond block in a rotating mode, the cross rod is connected with the diamond block in a rotating mode through a pin shaft, and a pressing plate is fixedly connected to the outer side end of the cross rod.
Preferably, four corners of the outer side surface of the base are provided with threaded holes.
Preferably, the distance between the outer wall of the cross rod and the contact surface of the base is 3-8 mm.
Preferably, the left side and the right side of the inner wall of the base are both provided with connector pushing-out mechanisms;
the connector pushing-out mechanism comprises a sliding chute, a sliding block, a supporting plate, a hook spring, a supporting column, a special-shaped groove, a bent rod and a pin rod;
two the spout is seted up respectively in the inner wall left and right sides of base, the inside slip joint of spout has the slider, the inboard surface rigid coupling of slider has the layer board, the lower surface of layer board is laminated with the lower surface of connector mutually, the front side top of slider is equipped with the couple spring, the pillar has all been articulated at the upper and lower both ends of couple spring, the bottom the pillar is fixed continuous with the front surface top of slider, the top the pillar is fixed continuous with the inside top of spout, the profiled groove has been seted up to the front surface of slider, the inside slip joint in profiled groove has the knee, the bottom of knee rotates and is connected with the pin rod, the pin rod links to each other with the inner wall bottom stationary phase of spout.
Preferably, the sliding groove and the sliding block form a sliding limiting structure.
Preferably, a sealing cover is arranged at the top end of the base;
the sealing cover comprises a top cover, a rubber pad, a pore and a rubber ring;
the top cap is located the inside top of base, the outer wall bottom of top cap and the contact surface clearance fit of base, the lower surface rigid coupling of top cap has the rubber pad, a plurality of pores have been seted up to the front surface of rubber pad, the bottom of rubber pad links to each other with the last fixed surface of connector, the fixed rubber ring that has cup jointed in the outer wall top of top cap, the bottom of rubber ring offsets tightly with the upper surface of base.
Compared with the prior art, the beneficial effects of the utility model are that: this unmanned aerial vehicle load quick detach interface arrangement for the conventional art, has following advantage:
through the cooperation between base, connector, vice interface, main interface and the installation mechanism, operating personnel only need insert the inside downward application of force of base with the connector and press, makes to support pole and inserted bar and accomplish one-way joint, can accomplish the installation of connector and base, operates comparatively simply and high-efficiently, need not to occupy the space in the base outside to the installation mechanism of connector, then more do benefit to the overall arrangement of unmanned aerial vehicle inner structure, and practicality can promote.
Through base, connector, installation mechanism and connector support the cooperation between the mechanism, when needs take out the connector from the base inside and change or when maintaining, operating personnel all moves two clamp plates to the inboard, pushes down the connector and makes the knee move to the inboard in the inside in abnormal shape groove, and then the couple spring can kick-back, can be comparatively laborsaving convenient take out the connector from the inside of base, does benefit to operating personnel and operates.
Through base, connector, installation mechanism, connector support out the cooperation between mechanism and the closing cap, after supporting pole and inserted bar completion one-way joint, the rubber ring between top cap and the base can be in and support tight state, and then can make the base inner space be in relative sealed state, does benefit to the permanent use of each parts of base inside.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a front cross-sectional view of FIG. 1;
FIG. 3 is a schematic view of the connection structure of the base, the insert rod and the support rod of FIG. 1;
fig. 4 is a schematic view of a connection structure of the base, the slider and the connector of fig. 1.
In the figure: 1. the connector comprises a base, 2, a connector, 3, an auxiliary socket, 4, a main socket, 5, a mounting mechanism, 501, a plug rod, 502, a cavity, 503, a resisting rod, 504, a tension spring, 505, a gasket, 506, a diamond block, 507, a support rod, 508, a transverse cylinder, 509, a pull rope, 510, a groove, 511, a cross rod, 512, a pin shaft, 513, a pressing plate, 6, a connector resisting mechanism, 601, a sliding groove, 602, a sliding block, 603, a supporting plate, 604, a hook spring, 605, a supporting column, 606, a special-shaped groove, 607, a bent rod, 608, a pin rod, 7, a sealing cover, 701, a top cover, 702, a rubber pad, a pore, 704, a rubber ring, 8, a rubber strip, 9, a through hole, 10 and a threaded hole.
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. 1-4, the present invention provides a technical solution: the utility model provides an unmanned aerial vehicle load quick detach interface arrangement, including base 1, the inside of base 1 is equipped with connector 2, the bottom rigid coupling of connector 2 has vice interface 3, the inside bottom rigid coupling of base 1 has main interface 4, main interface 4 pegs graft with vice interface 3 mutually, connector 2 is connected with base 1 through installation mechanism 5, the front surface center bottom of base 1 is equipped with rubber strip 8, rubber strip 8 is fixed continuous with base 1, rubber strip 8 is made for the rubber material, certain toughness has, through-hole 9 has all been seted up to the front surface left and right sides of rubber strip 8, through-hole 9 is used for connecting wire to insert the inside of base and is connected with main interface 4 and vice interface 3, installation mechanism 5 includes inserted bar 501, cavity 502, support bar 503, extension spring 504, gasket 505, diamond-shaped block 506, branch 507, horizontal section of thick bamboo 508, stay cord 509, recess 510, horizontal pole 511, The connector comprises a pin shaft 512 and a pressing plate 513, two insert rods 501 are respectively fixedly connected to the left side and the right side of the lower surface of the connector 2, a part of the insert rod 501 penetrates through the base 1, the outer wall of the insert rod 501 is in clearance fit with the contact surface of the base 1, two cavities 502 are respectively arranged on the left side and the right side of the inner bottom end of the base 1, a resisting rod 503 is inserted into the top end of the right side of the inner part of the cavity 502, a part of the resisting rod 503 penetrates through the base 1 and is in one-way clamped connection with the outer wall of the insert rod 501, the outer side of the outer wall of the insert rod 501 is provided with an inclined groove so as to be in single-item clamped connection with the resisting rod 503, the outer side of the outer wall of the resisting rod 503 is sleeved with an extension spring 504, the coefficient of the extension spring 504 is 2-8N/CM, the inner side end of the extension spring 504 is fixedly connected with the inner wall of the, all the rigid coupling in front and back two sides center of diamond-shaped block 506 has branch 507, the other end of branch 507 rotates with the inner wall of cavity 502 and links to each other, the front surface top rigid coupling of diamond-shaped block 506 has horizontal section of thick bamboo 508, the right side rigid coupling of horizontal section of thick bamboo 508 has stay cord 509, tensile 509 has certain toughness, the right side tip of stay cord 509 and gasket 505 are fixed continuous, two recesses 510 are seted up respectively in the left and right sides two sides bottom of base 1, horizontal pole 511 has been inserted to the inside inboard of recess 510, a part of horizontal pole 511 runs through base 1 and links to each other with the bottom of diamond-shaped block 506 commentaries on classics, horizontal pole 511 rotates with diamond-shaped block 506 through round pin axle 512 and links to each other, the outside tip rigid coupling of horizontal pole 511 has clamp plate 513, threaded hole 10 has all been seted up to the outside surface four corners of base 1, be convenient for base 1 and unmanned aerial vehicle installation, the distance between horizontal pole.
The left side and the right side of the inner wall of the base 1 are respectively provided with a connector pushing-out mechanism 6, the connector pushing-out mechanism 6 comprises sliding chutes 601, sliding blocks 602, supporting plates 603, hook springs 604, supporting columns 605, special-shaped grooves 606, bent rods 607 and pin rods 608, the two sliding chutes 601 are respectively arranged on the left side and the right side of the inner wall of the base 1, the sliding blocks 602 are slidably clamped in the sliding chutes 601, the supporting plates 603 are fixedly connected on the inner side surfaces of the sliding blocks 602, the lower surfaces of the supporting plates 603 are attached to the lower surface of the connector 2, the hook springs 604 are arranged above the front sides of the sliding blocks 602, the coefficient of the hook springs 604 is 2-10N/CM, the hook springs 604 are in a stretching state, the supporting columns 605 are respectively hung at the upper end and the lower end of each hook spring 604, the supporting columns 605 at the bottom end are fixedly connected with the top end of the front surface of, the inside slip joint of profiled groove 606 has the knee 607, and the bottom of knee 607 rotates to be connected with pin 608, and pin 608 is fixed continuous with the inner wall bottom of spout 601, and spout 601 and slider 602 constitute the spacing structure that slides, and spout 601 can play limiting displacement to slider 602, and slider 602 can slide from top to bottom in the inside of spout 601, can ensure the stability when slider 602 slides from top to bottom.
The top of base 1 is equipped with closing cap 7, closing cap 7 includes top cap 701, rubber pad 702, pore 703 and rubber ring 704, top cap 701 is located the inside top of base 1, the outer wall bottom of top cap 701 and the contact surface clearance fit of base 1, the lower surface rigid coupling of top cap 701 has rubber pad 702, a plurality of pores 703 have been seted up to the front surface of rubber pad 702, pore 703 can increase the toughness of rubber pad 702, the bottom of rubber pad 702 links to each other with the last fixed surface of connector 2, the fixed cover in outer wall top of top cap 701 has rubber ring 704, the bottom of rubber ring 704 offsets tightly with the upper surface of base 1, rubber pad 702 and rubber ring 704 are the rubber material and make, certain toughness has.
When the rapid interface device for load disassembly of the unmanned aerial vehicle is used, an operator inserts the connector 2 into the base 1 to apply downward force and press, the main interface 4 and the auxiliary interface 3 are connected together in a clamping manner, the main interface 4 and the auxiliary interface 3 are internally provided with communication interfaces for realizing communication connection of a flight control system and a load, and the abutting rod 503 and the inserting rod 501 can be connected in a one-way clamping manner to complete the installation of the connector 2 and the base 1, the operation is simple and efficient, the installation mechanism 5 of the connector 2 does not need to occupy the space outside the base 1, meanwhile, the rubber ring 704 between the top cover 701 and the base 1 can be in an abutting state, so that the internal space of the base 2 can be in a relatively sealed state, the device is beneficial to the long-term use of all parts inside the base 1, when the connector 2 needs to be taken out from the base 1 for replacement or maintenance, the operator moves the two pressing plates 513 inwards, the diamond blocks 506 can rotate around the supporting rods 507, the pulling ropes 509 can apply force to the gasket 505, the gasket 505 and the abutting rods 503 are outward fixed, the abutting rods 503 are separated from the inserting rods 501, the connector 2 of the top cover 701 is pressed downwards to move downwards in the base 1 in a certain amount, the bent rods 607 move inwards in the special-shaped grooves 606, the hook springs 604 can rebound, the connector 2 can be conveniently taken out from the base 1 in a labor-saving mode, and operation of the operator is facilitated.
In the description of the present invention, it is to be understood that the terms "coaxial", "bottom", "one end", "top", "middle", "other end", "upper", "one side", "top", "inner", "front", "center", "both ends", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "disposed," "connected," "fixed," "screwed" and the like are to be construed broadly, e.g., as meaning fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; they may be directly connected or indirectly connected through an intermediate medium, and may be connected through the inside of two elements or in an interaction relationship between two elements, unless otherwise specifically defined, and the specific meaning of the above terms in the present invention will be understood by those skilled in the art according to specific situations.
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 load quick detach interface arrangement, includes base (1), its characterized in that: a connector (2) is arranged inside the base (1), an auxiliary inserting port (3) is fixedly connected to the bottom end of the connector (2), a main inserting port (4) is fixedly connected to the bottom end inside the base (1), the main inserting port (4) is inserted into the auxiliary inserting port (3), the connector (2) is connected with the base (1) through an installing mechanism (5), a rubber strip (8) is arranged at the bottom end of the center of the front surface of the base (1), and through holes (9) are formed in the left side and the right side of the front surface of the rubber strip (8);
the mounting mechanism (5) comprises an inserting rod (501), a cavity (502), a resisting rod (503), an extension spring (504), a gasket (505), a diamond block (506), a support rod (507), a transverse cylinder (508), a pull rope (509), a groove (510), a transverse rod (511), a pin shaft (512) and a pressing plate (513);
the two insertion rods (501) are fixedly connected to the left side and the right side of the lower surface of the connector (2) respectively, a part of the insertion rods (501) penetrates through the base (1), the two cavities (502) are arranged on the left side and the right side of the inner bottom end of the base (1) respectively, a resisting rod (503) is inserted into the top end of the right side of the inner portion of each cavity (502), a part of the resisting rod (503) penetrates through the base (1) and is in one-way clamped connection with the outer wall of the insertion rod (501), a tension spring (504) is sleeved on the outer side of the outer wall of each resisting rod (503), the end of the inner side of each tension spring (504) is fixedly connected with the inner wall of each cavity (502), a gasket (505) is fixedly connected with the end of the outer side of each tension spring (504), the right surface of each gasket (505) is fixedly connected with the end of the left side of each resisting rod (503), a diamond block (506) is arranged in the center of the inner, the other end of branch (507) rotates with the inner wall of cavity (502) and links to each other, the front surface top rigid coupling of diamond-shaped block (506) has horizontal section of thick bamboo (508), the right side rigid coupling of horizontal section of thick bamboo (508) has stay cord (509), the right side tip of stay cord (509) links to each other with gasket (505) is fixed, two recess (510) are seted up respectively in the left and right sides two sides bottom of base (1), horizontal pole (511) have been inserted to the inside inboard of recess (510), the bottom that base (1) and diamond-shaped block (506) were run through to partly of horizontal pole (511) is changeed and is linked to each other, horizontal pole (511) rotate with diamond-shaped block (506) through round pin axle (512) and link to each other, the outside tip rigid coupling of horizontal pole (511) has clamp.
2. The rapid interface device for unmanned aerial vehicle load release of claim 1, wherein: threaded holes (10) are formed in four corners of the outer side surface of the base (1).
3. The rapid interface device for unmanned aerial vehicle load release of claim 1, wherein: the distance between the outer wall of the cross rod (511) and the contact surface of the base (1) is 3-8 mm.
4. The rapid interface device for unmanned aerial vehicle load release of claim 1, wherein: the left side and the right side of the inner wall of the base (1) are respectively provided with a connector pushing-out mechanism (6);
the connector pushing-out mechanism (6) comprises a sliding groove (601), a sliding block (602), a supporting plate (603), a hook spring (604), a supporting column (605), a special-shaped groove (606), a bent rod (607) and a pin rod (608);
the two sliding chutes (601) are respectively arranged at the left side and the right side of the inner wall of the base (1), a sliding block (602) is clamped in the sliding groove (601) in a sliding manner, a supporting plate (603) is fixedly connected to the inner side surface of the sliding block (602), the lower surface of the supporting plate (603) is attached to the lower surface of the connector (2), a hook spring (604) is arranged above the front side of the sliding block (602), the upper end and the lower end of the hook spring (604) are respectively hung with a supporting column (605), the supporting column (605) at the bottom end is fixedly connected with the top end of the front surface of the sliding block (602), the supporting column (605) at the top end is fixedly connected with the top end inside the sliding groove (601), the front surface of the sliding block (602) is provided with a special-shaped groove (606), the inner part of the special-shaped groove (606) is clamped with a bent rod (607) in a sliding way, the bottom end of the bent rod (607) is rotatably connected with a pin rod (608), and the pin rod (608) is fixedly connected with the bottom end of the inner wall of the sliding groove (601).
5. The rapid interface device for unmanned aerial vehicle load according to claim 4, wherein: the sliding groove (601) and the sliding block (602) form a sliding limiting structure.
6. The rapid interface device for unmanned aerial vehicle load release of claim 1, wherein: a sealing cover (7) is arranged at the top end of the base (1);
the sealing cover (7) comprises a top cover (701), a rubber pad (702), a pore (703) and a rubber ring (704);
top cap (701) are located the inside top of base (1), the outer wall bottom of top cap (701) and the contact surface clearance fit of base (1), the lower surface rigid coupling of top cap (701) has rubber pad (702), a plurality of pores (703) have been seted up to the front surface of rubber pad (702), the bottom of rubber pad (702) links to each other with the last fixed surface of connector (2), the outer wall top of top cap (701) is fixed to be cup jointed rubber ring (704), the bottom of rubber ring (704) offsets tightly with the upper surface of base (1).
CN202020432575.1U 2020-03-30 2020-03-30 Unmanned aerial vehicle load quick detach interface arrangement Expired - Fee Related CN212149312U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202020432575.1U CN212149312U (en) 2020-03-30 2020-03-30 Unmanned aerial vehicle load quick detach interface arrangement

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202020432575.1U CN212149312U (en) 2020-03-30 2020-03-30 Unmanned aerial vehicle load quick detach interface arrangement

Publications (1)

Publication Number Publication Date
CN212149312U true CN212149312U (en) 2020-12-15

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Application Number Title Priority Date Filing Date
CN202020432575.1U Expired - Fee Related CN212149312U (en) 2020-03-30 2020-03-30 Unmanned aerial vehicle load quick detach interface arrangement

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117498083A (en) * 2024-01-03 2024-02-02 陕西四菱电子科技股份有限公司 Micro rectangular electric connector with guiding function

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117498083A (en) * 2024-01-03 2024-02-02 陕西四菱电子科技股份有限公司 Micro rectangular electric connector with guiding function
CN117498083B (en) * 2024-01-03 2024-03-12 陕西四菱电子科技股份有限公司 Micro rectangular electric connector with guiding function

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Granted publication date: 20201215

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