CN218703842U

CN218703842U - A insert formula horn device soon for unmanned aerial vehicle

Info

Publication number: CN218703842U
Application number: CN202222963504.6U
Authority: CN
Inventors: 高明
Original assignee: Guandian Defense Technology Co ltd
Current assignee: Guandian Defense Technology Co ltd
Priority date: 2022-11-07
Filing date: 2022-11-07
Publication date: 2023-03-24
Anticipated expiration: 2032-11-07

Abstract

The utility model discloses a fast-inserting type horn device for an unmanned aerial vehicle, which aims to solve the technical problem that the rapid installation and disassembly treatment of the horn of the unmanned aerial vehicle is inconvenient in the prior art; the quick-insertion type horn device comprises an unmanned aerial vehicle main body; the outer side of the unmanned aerial vehicle main body is fixedly provided with a connector lug, the upper end of the connector lug is provided with a jack, the upper end of the connector lug is provided with a horn main body, the bottom end of the horn main body is fixedly provided with a metal connecting block, the outer side of the horn main body is provided with a positioning assembly, the outer side of the unmanned aerial vehicle main body is provided with a locking assembly, one end of the horn main body is fixedly provided with a motor, and the output end of the motor is provided with a spiral blade; this a formula horn device inserts soon for unmanned aerial vehicle only needs to fix a position the processing through positioning assembly's setting to the horn main part, fixes the position of horn main part through locking assembly's setting to realized the quick installation and the dismantlement processing to the unmanned aerial vehicle horn.

Description

A insert formula horn device soon for unmanned aerial vehicle

Technical Field

The utility model belongs to the technical field of the unmanned aerial vehicle horn, concretely relates to insert formula horn device soon for unmanned aerial vehicle.

Background

Nowadays, the use of unmanned aerial vehicles is more common in life, and compared with piloted aircraft, unmanned aerial vehicles are often better suited to tasks that are too "fool, dirty or dangerous", being unmanned aircraft operated by means of radio remote control devices and self-contained program control devices, whereas the unmanned aerial vehicle arm is one of the main accessories that make up the unmanned aerial vehicle.

At present, a patent of utility model No. cn202220701810.x discloses a quick-insertion type horn for an unmanned aerial vehicle, which comprises a large arm and a small arm, wherein the outer end of the small arm is connected with a motor mounting seat, the inner end of the small arm is movably inserted in the large arm, one end of the large arm is integrally connected with an insertion device, the insertion device is connected in the insertion seat, and the insertion seat is internally installed on the side wall of the unmanned aerial vehicle body; according to the quick-insertion type arm for the unmanned aerial vehicle, the locking plug is aligned with the jack to be inserted, the elastic spring bolt is clamped into the locking hole of the locking plug, the installation is simple and firm, and the problem of falling off cannot occur in the use process; when the movable arm is disassembled, the elastic spring bolt is manually pushed to be separated from the locking hole, so that the movable arm is very convenient to disassemble, the damaged arm can be conveniently replaced by the detachable arrangement, and the movable arm is convenient to carry when going out; the telescopic setting of forearm is in big arm, further reduces the storage space. What its adopted is that it sets up the convenience through detachable and changes the horn of damage, nevertheless should insert formula horn device soon in the use, and is comparatively loaded down with trivial details to the installation of unmanned aerial vehicle horn, is not convenient for install fast and dismantle the processing to the unmanned aerial vehicle horn.

Therefore, to the problem that the above-mentioned formula horn device of inserting soon that is used for unmanned aerial vehicle in daily use is not convenient for install fast after using, urgent need be solved to improve the device's practicality.

SUMMERY OF THE UTILITY MODEL

(1) Technical problem to be solved

Not enough to prior art, an object of the utility model is to provide a formula horn device inserts soon for unmanned aerial vehicle, this a formula horn device inserts soon for unmanned aerial vehicle aims at solving prior art and is not convenient for install the technical problem of handling fast and dismantlement to the unmanned aerial vehicle horn down.

(2) Technical scheme

In order to solve the technical problem, the utility model provides a quick-inserting type horn device for an unmanned aerial vehicle, which comprises an unmanned aerial vehicle main body; the utility model discloses an unmanned aerial vehicle, including unmanned aerial vehicle main part, connector lug, jack, bottom fixed mounting, locating component, locking component, the one end fixed mounting of horn main part has the motor, the output of motor is provided with the spiral leaf.

When using this technical scheme's a formula horn device of inserting soon for unmanned aerial vehicle, go into the bottom metal connecting block of horn main part along the jack card of connector lug upper end, fix a position the processing to the horn main part through setting up of locating component, fix the position of horn main part through setting up of locking component to realized installing fast and dismantling the processing to the unmanned aerial vehicle horn.

Further, locating component's inside is including the constant head tank, the constant head tank is seted up in the outside of unmanned aerial vehicle main part, the outside fixed mounting of horn main part has the locating piece, the locating piece with the constant head tank block is connected, is connected through the block of locating piece and constant head tank and carries out the location processing to the horn main part.

Further, locking Assembly's inside is including accomodating the groove, it sets up in to accomodate the groove the inboard of unmanned aerial vehicle main part, the inboard of accomodating the groove is provided with the inserted block, the inserted block with accomodate groove sliding connection, the pulling arm drives the inserted block and accomodates to the inside of accomodating the groove.

Furthermore, the inside of the locking assembly comprises a slot, the slot is arranged on the outer side of the machine arm main body and is connected with the insertion block in a clamping manner, and the position of the machine arm main body is fixed through the clamping connection of the insertion block and the slot.

Furthermore, locking Assembly's inside is including the spring, the spring set up in accomodate the inboard in groove, the one end of spring with the one end interconnect of inserted block loosens the arm-tie, makes the inserted block receive the elasticity of spring and resets.

Further, locking Assembly's inside is including the spout, the spout is seted up in the upper end of unmanned aerial vehicle main part, the upper end of inserted block is provided with the arm-tie, the arm-tie with spout sliding connection carries out spacing processing to the arm-tie through the sliding connection of arm-tie and spout.

(3) Advantageous effects

Compared with the prior art, the beneficial effects of the utility model reside in that: the utility model discloses a formula horn device inserts soon for unmanned aerial vehicle utilizes the pulling arm-tie to drive the inserted block and accomodates to the inside of accomodating the groove, sliding connection through arm-tie and spout carries out spacing processing to the arm-tie, the bottom metal connecting block with the horn main part is gone into along the jack card of connector lug upper end, and simultaneously, the locating piece is gone into along the constant head tank card, loosen the arm-tie, the elasticity that makes the inserted block receive the spring resets, block through inserted block and slot is connected the position of fixing the horn main part, thereby realized installing fast and dismantling the processing to the unmanned aerial vehicle horn.

Drawings

Fig. 1 is a schematic three-dimensional structure of an embodiment of the present invention;

FIG. 2 is a schematic structural view of a cross-section of an embodiment of the present invention;

fig. 3 is a schematic structural view of a partial section according to an embodiment of the present invention.

The symbols in the drawings are: 1. an unmanned aerial vehicle main body; 2. a connector lug; 3. a jack; 4. a horn body; 5. a metal connecting block; 6. a positioning assembly; 7. a locking assembly; 8. a motor; 9. helical leaves; 10. positioning a groove; 11. positioning blocks; 12. a receiving groove; 13. inserting a block; 14. a slot; 15. a spring; 16. a chute; 17. and (5) pulling the plate.

Detailed Description

In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the following description is made for the technical solution of the present invention in the embodiments to explain the present invention clearly and completely, obviously, the described embodiments are only a part of the embodiments of the present invention, but not all the embodiments.

Examples

This embodiment is a formula horn device inserts soon for unmanned aerial vehicle, and its spatial structure sketch map is as shown in fig. 1, and its section structure sketch map is as shown in fig. 2, and this formula horn device inserts soon includes unmanned aerial vehicle main part 1; the outside fixed mounting of unmanned aerial vehicle main part 1 has connector lug 2, jack 3 has been seted up to the upper end of connector lug 2, the upper end of connector lug 2 is provided with horn main part 4, the bottom fixed mounting of horn main part 4 has metal connecting block 5, the outside of horn main part 4 is provided with locating component 6, the outside of unmanned aerial vehicle main part 1 is provided with locking Assembly 7, the one end fixed mounting of horn main part 4 has motor 8, motor 8's output is provided with spiral leaf 9.

Wherein, locating component 6's inside is including constant head tank 10, the outside in unmanned aerial vehicle main part 1 is seted up to constant head tank 10, the outside fixed mounting of horn main part 4 has locating piece 11, locating piece 11 is connected with constant head tank 10 block, be connected through locating piece 11 and constant head tank 10 block and fix a position the processing to horn main part 4, locking component 7's inside is including accomodating groove 12, accomodate groove 12 and set up the inboard in unmanned aerial vehicle main part 1, the inboard of accomodating groove 12 is provided with inserted block 13, inserted block 13 with accomodate groove 12 sliding connection, the pulling arm-tie 17 drives inserted block 13 and accomodates to the inside of accomodating groove 12.

This embodiment is a formula horn device inserts soon for unmanned aerial vehicle, its local section structure schematic diagram is shown in fig. 3, locking Assembly 7's inside is including slot 14, slot 14 is seted up in the outside of horn main part 4, slot 14 is connected with inserted block 13 block, be connected the position to horn main part 4 through inserted block 13 and slot 14's block and fix, locking Assembly 7's inside is including spring 15, spring 15 sets up in the inboard of accomodating groove 12, spring 15's one end and the one end interconnect of inserted block 13, loosen arm-tie 17, make inserted block 13 receive the elasticity of spring 15 to reset.

Simultaneously, locking Assembly 7's inside is including spout 16, and spout 16 sets up in the upper end of unmanned aerial vehicle main part 1, and the upper end of inserted block 13 is provided with arm-tie 17, and arm-

tie

17 and 16 sliding connection of spout carry out spacing processing to arm-tie 17 through arm-

tie

17 and 16 sliding connection of spout.

Use during the formula horn device of inserting soon that is used for unmanned aerial vehicle of this technical scheme, pulling arm 17 drives inserted block 13 and accomodates the inside to accomodating groove 12, sliding connection through arm 17 and spout 16 carries out spacing processing to arm 17, the bottom metal connecting block 5 of horn main part 4 is gone into along the jack 3 card of 2 upper ends of connector lug, and simultaneously, locating piece 11 is gone into along constant head tank 10 card, loosen arm 17, make inserted block 13 receive the elasticity of spring 15 and reset, the position of being connected horn main part 4 is fixed through inserted block 13 and slot 14's block, thereby realized installing fast and dismantling the processing to the unmanned aerial vehicle horn.

Claims

1. A fast-inserting type horn device for an unmanned aerial vehicle comprises an unmanned aerial vehicle main body (1); its characterized in that, the outside fixed mounting of unmanned aerial vehicle main part (1) has connector lug (2), jack (3) have been seted up to the upper end of connector lug (2), the upper end of connector lug (2) is provided with horn main part (4), the bottom fixed mounting of horn main part (4) has metal connecting block (5), the outside of horn main part (4) is provided with locating component (6), the outside of unmanned aerial vehicle main part (1) is provided with locking Assembly (7), the one end fixed mounting of horn main part (4) has motor (8), the output of motor (8) is provided with spiral leaf (9).

2. The quick-insertion type horn device for the unmanned aerial vehicle according to claim 1, wherein the positioning assembly (6) comprises a positioning groove (10), the positioning groove (10) is arranged on the outer side of the unmanned aerial vehicle main body (1), a positioning block (11) is fixedly mounted on the outer side of the horn main body (4), and the positioning block (11) is connected with the positioning groove (10) in a clamping manner.

3. The quick-insertion type horn device for the unmanned aerial vehicle according to claim 1, wherein the locking assembly (7) comprises an accommodating groove (12), the accommodating groove (12) is formed in the inner side of the unmanned aerial vehicle main body (1), an inserting block (13) is arranged on the inner side of the accommodating groove (12), and the inserting block (13) is connected with the accommodating groove (12) in a sliding manner.

4. The fast-insertion type horn device for the unmanned aerial vehicle as claimed in claim 3, wherein the locking assembly (7) comprises a slot (14) inside, the slot (14) is arranged on the outer side of the horn body (4), and the slot (14) is connected with the insertion block (13) in a clamping manner.

5. The fast-plugging horn device for unmanned aerial vehicle of claim 4, wherein the inside of the locking assembly (7) comprises a spring (15), the spring (15) is disposed inside the accommodating groove (12), and one end of the spring (15) is connected with one end of the plug block (13).

6. The quick-insertion type horn device for the unmanned aerial vehicle according to claim 5, wherein the locking assembly (7) comprises a sliding groove (16), the sliding groove (16) is formed in the upper end of the unmanned aerial vehicle main body (1), a pulling plate (17) is arranged at the upper end of the insertion block (13), and the pulling plate (17) is in sliding connection with the sliding groove (16).