CN113911362B - Unmanned aerial vehicle system ammunition throwing device - Google Patents
Unmanned aerial vehicle system ammunition throwing device Download PDFInfo
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- CN113911362B CN113911362B CN202111407977.1A CN202111407977A CN113911362B CN 113911362 B CN113911362 B CN 113911362B CN 202111407977 A CN202111407977 A CN 202111407977A CN 113911362 B CN113911362 B CN 113911362B
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- aerial vehicle
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- 239000011521 glass Substances 0.000 claims description 6
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- 238000005859 coupling reaction Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 238000000151 deposition Methods 0.000 description 1
- 238000005474 detonation Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 238000004043 dyeing Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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- IMACFCSSMIZSPP-UHFFFAOYSA-N phenacyl chloride Chemical compound ClCC(=O)C1=CC=CC=C1 IMACFCSSMIZSPP-UHFFFAOYSA-N 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 239000003491 tear gas Substances 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/04—Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
- B64D1/06—Bomb releasing; Bomb doors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/15—UAVs specially adapted for particular uses or applications for conventional or electronic warfare
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention relates to an unmanned aerial vehicle standard ammunition throwing device, which comprises: the connecting device comprises a connecting bracket, two first hanging pieces are arranged on the connecting bracket, a limiting piece is arranged at the first end of each first hanging piece, a pressing piece is arranged at the second end of each first hanging piece, and each pressing piece is provided with a first working position and a second working position; the top surface of the cover body is provided with two second hanging pieces, and the two second hanging pieces are respectively hung with the two first hanging pieces; when the pressing piece is located at the first working position, the limiting piece abuts against the first end of the second hanging piece, the pressing piece abuts against the second end of the second hanging piece, and the cover body and the connecting support are located in a locking state; when the pressing piece is located at the second working position, the pressing piece does not abut against the second end of the second hanging piece, the second end of the first hanging piece is open, and the connecting bracket can slide in or slide out from the second end of the first hanging piece.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles and task loads thereof, in particular to an unmanned aerial vehicle standard ammunition throwing device.
Background
The common bolt of ammunition transmitter that current unmanned aerial vehicle used is on the connecting piece, and the connecting piece passes through the bolt fastening on unmanned aerial vehicle. However, the existing installation mode is complex, and the connection and the quick disassembly of the ammunition launcher for the unmanned aerial vehicle cannot be realized.
Disclosure of Invention
Based on this, the invention aims to provide an unmanned aerial vehicle system ammunition throwing device.
The utility model provides an unmanned aerial vehicle system ammunition throwing device, unmanned aerial vehicle system ammunition throwing device includes: the connecting device comprises a connecting bracket, wherein two first hanging pieces are arranged on the connecting bracket, a limiting piece is arranged at the first end of each first hanging piece, a pressing piece is arranged at the second end of each first hanging piece, and each pressing piece is provided with a first working position and a second working position; the top surface of the cover body is provided with two second hanging pieces, and the two second hanging pieces are hung and leaned against the two first hanging pieces respectively; when the pressing piece is located at the first working position, the limiting piece abuts against the first end of the second hanging piece, the pressing piece abuts against the second end of the second hanging piece, and the cover body and the connecting support are located in a locking state; when the pressing piece is located at the second working position, the pressing piece does not abut against the second end of the second hanging piece, the second end of the first hanging piece is open, and the connecting bracket can slide in or slide out from the second end of the first hanging piece.
Further, the first hanger has a first notch in which a portion of the second hanger is located when the first hanger and the second hanger are hung against each other, the portion of the second hanger and the first notch abutting against each other; the second hanger has a second notch in which a portion of the first hanger is positioned when the first hanger and the second hanger are hung against each other, the portion of the first hanger and the second notch abutting against each other.
Further, the first hanging member has a first extending member and a second extending member, the first extending member extends vertically and downwardly from the bottom surface of the connecting bracket, the second extending member extends horizontally and outwardly from the lower end of the first extending member, and the bottom surface of the connecting bracket, the first extending member and the second extending member together form one of the first recesses.
Further, the second hanging piece is provided with a third extending piece and a fourth extending piece, the third extending piece extends vertically and upwards from the top surface of the cover body, the fourth extending piece extends horizontally and inwards from the upper end of the third extending piece, and the top surface of the cover body, the third extending piece and the fourth extending piece together form the second notch; when the first and second hangers are engaged with each other, the end portion of the second extension is located in the second recess and the end portion of the fourth extension is located in the first recess.
Furthermore, the first hanging piece is of a long strip-shaped rail structure with a guiding function; the second hanging piece is of a strip-shaped rail structure with a guiding function.
Further, a second connecting hole is formed in the connecting support, and the second connecting hole is provided with an internal thread; the pressing piece is rotatably connected to the connecting support through a rotating shaft, a third connecting hole which can correspond to the second connecting hole is formed in the pressing piece, a bolt is arranged in the third connecting hole, and the bolt is in threaded connection with the second connecting hole; the bolt is also in threaded connection with the third connecting hole.
Furthermore, a second connecting hole is formed in the connecting support, and the second connecting hole is of a hemispherical groove structure; the pressing piece is rotatably connected to the connecting support through a rotating shaft, a third connecting hole which can correspond to the second connecting hole is formed in the pressing piece, a glass bead screw is connected to the third connecting hole in a threaded mode, and the glass bead screw is connected with the second connecting hole in a buckling mode.
Further, be provided with first connecting hole on the linking bridge install the anticreep screw in the first connecting hole, the one end of first connecting hole can with anticreep screw threaded connection, the other end cover of first connecting hole is established outside on the anticreep screw.
Further, unmanned aerial vehicle system ammunition throwing device still includes the box, the lid closes the opening part of box.
Furthermore, two side surfaces of the opening of the box body are respectively provided with a clamping piece and a clamping piece, and the clamping piece are arranged oppositely; the cover body is provided with a buckling part and a clamping hook part, the buckling part is connected with the clamping piece in a buckling mode, the clamping hook part is connected to the cover body in a rotating mode and provided with a hook part and a fourth connecting hole, the hook part and the fourth connecting hole are arranged on two sides of the rotating axis of the clamping hook part respectively, the hook part is connected with the clamping piece in a buckling mode, a locking piece is connected to the fourth connecting hole in a threaded mode, and a pressing surface is arranged on the moving track of the locking piece; after the locking piece abuts against the pressing surface, the locking piece is rotated, one end, far away from the hook part, of the hook part rotates along the direction of the locking piece far away from the pressing surface, and the hook part rotates towards the direction of the clamping piece, so that the hook part is connected with the clamping piece in a clamping mode; a guide hole is formed in the moving track of the locking piece, one end of the guide hole is opened to allow the locking piece to enter, and the other end of the guide hole is closed to form the abutting surface; the pressing surface is arranged on the cover body and is positioned at the top of the cover body; the guide hole is formed in the cover body and is located at the top of the cover body; the clamping piece is of a boss structure or a hook structure, and the buckling part is of a round shaft structure; the buckle piece is of a flanging structure or a buckle hole structure; a guide hole is formed in the moving track of the locking piece, one end of the guide hole is opened to allow the locking piece to enter, and the other end of the guide hole is closed to form the abutting surface; the aperture of the guide hole is larger than that of the fourth connecting hole; the unmanned aerial vehicle standard ammunition throwing device further comprises a controller, a first wiring terminal and a second wiring terminal, wherein the controller is used for controlling ammunition emission, the first wiring terminal is arranged on the connecting support and is in a floating end shape, the second wiring terminal is arranged at the top of the cover body and is a floating terminal, the controller is connected with one end of the first wiring terminal through an electric wire, and the other end of the first wiring terminal is connected with one end of the second wiring terminal in an inserting mode.
For a better understanding and practice, the present invention is described in detail below with reference to the accompanying drawings.
Drawings
Fig. 1 is an exploded schematic view of an unmanned aerial vehicle type ammunition throwing device according to an embodiment;
FIG. 2 is a schematic structural view of a connecting bracket according to an embodiment;
FIG. 3 is a bottom view of an exemplary attachment bracket;
FIG. 4 is a schematic view of an unlocked state of the connecting bracket according to the embodiment;
FIG. 5 is a schematic structural diagram of a cover according to an embodiment;
FIG. 6 is a schematic view of another perspective of the cover according to the embodiment;
FIG. 7 is a schematic view of the embodiment showing the connection bracket and the cover locked to each other;
FIG. 8 is a schematic structural diagram of a case according to an embodiment;
FIG. 9 is a schematic view illustrating a locked state of the case and the cover according to the embodiment;
reference numerals:
1. connecting a bracket; 11. a first connection hole; 11a, an anti-falling screw; 12. a first hanger; 12a, a first notch; 12b, a first extension; 12c, a second extension; 12d, a limiting piece; 13. a pressing member; 13a, a rotating shaft; 13b, a third connecting hole; 13c, bolts; 14. a second connection hole; 2. a box body; 21. a fastener; 22. a fastener; 3. a cover body; 31. a second pendant; 31a, a second recess; 31b, a third extension; 31c, a fourth extension; 32. a buckle part; 33. a hook section; 33a, a hook portion; 33b, a fourth connection hole; 33c, a locking member; 33d, a pressing surface; 33e, a guide hole; 4. a first connection terminal; 5. and a second connection terminal.
Detailed Description
An unmanned aerial vehicle system ammunition throwing device is shown in figures 1 to 9 and comprises a connecting bracket 1 and an ammunition box. Wherein, linking bridge 1 can be used to install on the mobile device, for example unmanned aerial vehicle, unmanned ship, unmanned car etc. in this embodiment, this linking bridge 1 is used for installing in unmanned aerial vehicle's bottom to linking bridge 1 is located between unmanned aerial vehicle's the landing leg. The ammunition box is used for installing on linking bridge 1, and the inner chamber of ammunition box is used for depositing the ammunition, and this ammunition can be tear-gas shells, detonation bomb, smog bullet, pain ball bullet, dyeing bomb, flash bomb, dazzling bomb etc..
Referring to fig. 1 to 9, in order to connect the connection bracket 1 with the mobile device, at least four first connection holes 11 are provided at the top of the connection bracket 1, an inner wall of a lower end of the first connection hole 11 has an internal thread, and an inner wall of an upper end of the first connection hole 11 does not have an internal thread. An anti-drop screw 11a is installed in each first connection hole 11, and the anti-drop screw 11a is a screw having an external thread at a screw end and no external thread at the rest of the screw. When the connecting bracket 1 is connected with the mobile device, the anti-falling screw 11a is in threaded connection with the mobile device after sequentially passing through the internal thread part and the non-internal thread part of the first connecting hole 11. When the connection bracket 1 is separated from the mobile device, the end surface of the internal thread of the first connection hole 11 abuts against the end surface of the external thread of the anti-drop screw 11a, the anti-drop screw 11a is limited on the connection bracket 1, and the anti-drop screw 11a can move up and down in the first connection hole 11.
Referring to fig. 1 to 9, in order to connect the linking bracket 1 to the cartridge case, two first hanging members 12 are provided on the bottom surface of the linking bracket 1, and the first hanging members 12 have first recesses 12 a. The ammunition box comprises a box body 2 and a cover body 3, wherein the inner cavity of the box body 2 is used for storing ammunition, and the cover body 3 is detachably arranged on the box body 2. Two second hanging pieces 31 are arranged on the top surface of the cover body 3, the two second hanging pieces 31 are respectively hung with the two first hanging pieces 12, and the second hanging pieces 31 are provided with second notches 31 a. When the first hanging member 12 and the second hanging member 31 are hung on each other, a portion of the first hanging member 12 is located in the second recess 31a, a portion of the second hanging member 31 is located in the first recess 12a, and the portion of the first hanging member 12 abuts against the wall surface of the second recess 31a to provide an upward supporting force to the lid body 3.
Specifically, the first hanging member 12 has a first extending member 12b and a second extending member 12c, the first extending member 12b extends vertically downward from the bottom surface of the connecting bracket 1, the second extending member 12c extends horizontally outward from the lower end of the first extending member 12b, and the bottom surface of the connecting bracket 1, the first extending member 12b and the second extending member 12c together form one of the first recesses 12 a. The second hanging member 31 has a third extending member 31b and a fourth extending member 31c, the third extending member 31b extends vertically upward from the top surface of the lid 3, the fourth extending member 31c extends horizontally inward from the upper end of the third extending member 31b, and the top surface of the lid 3, the third extending member 31b and the fourth extending member 31c together form one of the second recesses 31 a. When the first hanger 12 and the second hanger 31 are hung on each other, the end portion of the second extension piece 12c is located in the second recess 31a, the end portion of the fourth extension piece 31c is located in the first recess 12a, and the top surface of the second extension piece 12c and the bottom surface of the fourth extension piece 31c are butted on each other.
In addition to this, in order to hang the cartridge case on the attachment bracket 1, it is also possible that the first suspension member 12 has a first recess 12a, the second suspension member 31 does not have a second recess 31a, and a portion of the second suspension member 31 is located in the first recess 12 a. It is also possible that the first hanger 12 does not have the first recess 12a, the second hanger 31 has the second recess 31a, and a portion of the first hanger 12 is located in the second recess 31 a.
Further, in order to facilitate the assembly of the connecting bracket 1 and the cover 3, one of the first hanging member 12 and the second hanging member 31 is an elongated rail structure with a guiding function, and in this embodiment, the first hanging member 12 and the second hanging member 31 are both elongated rail structures with a guiding function. Through this design, can increase the area of contact between linking bridge 1 and lid 3 effectively to increase the lifting surface area.
Further, in order to ensure the locking of the cover 3 and the connecting bracket 1, a limiting member 12d is disposed at a first end of the first hanging member 12, and a pressing member 13 is disposed at a second end of the first hanging member 12, wherein the pressing member 13 has a first working position and a second working position. When the cover 3 and the connecting bracket 1 are in a locked state, the limiting member 12d abuts against the first end of the second hanging member 31, the pressing member 13 is in the first working position, the pressing member 13 abuts against the second end of the second hanging member 31, and the second end of the first hanging member 12 is a closed end. When the cover 3 and the connecting bracket 1 are in the unlocked state, the pressing part 13 is in the second working position, the pressing part 13 does not abut against the second end of the second hanging member 31, and the second end of the first hanging member 12 is an open end, so that the connecting bracket 1 can slide out from the open end of the first hanging member 12.
In this embodiment, a second connecting hole 14 is provided on the connecting bracket 1, and the second connecting hole 14 is a threaded straight hole; one end of the pressing piece 13 is rotatably connected to the connecting bracket 1 through a rotating shaft 13a, a third connecting hole 13b which can correspond to the second connecting hole 14 is formed in the pressing piece 13, and the third connecting hole 13b can be a hole with an internal thread or a through hole without an internal thread. When the pressing member 13 is located at the first working position, the bolt 13c passes through the third connecting hole 13b and then is connected with the second connecting hole 14, so that the pressing member 13 is fixed at the first working position. When the pressing member 13 needs to be switched to the second working position, the bolt 13c is separated from the second connecting hole 14, and the pressing member 13 rotates around the rotating shaft 13a from the first working position to the second working position.
In another embodiment, a second connecting hole 14 is arranged on the connecting bracket 1, and the second connecting hole 14 is of a hemispherical groove structure; one end of the pressing piece 13 is rotatably connected to the connecting bracket 1 through a rotating shaft 13a, a third connecting hole 13b which can correspond to the second connecting hole 14 is formed in the pressing piece 13, a glass bead screw is connected to the third connecting hole 13b in a threaded manner, and the glass bead screw is connected with the second connecting hole 14 in a buckling manner.
In addition, the pressing member 13 may be rotatably connected to the connecting bracket 1, or may be slidably connected to the connecting bracket 1, and then the pressing member 13 is switched between the first working position and the second working position by the cooperation of the second connecting hole 14 of the connecting bracket 1, the third connecting hole 13b of the pressing member 13, and the bolt 13 c. In addition, the locking mechanism for locking the pressing member 13 in the first working position may be any of the existing locking mechanisms, and is not limited herein.
Referring to fig. 1 to 9, in order to connect the box body 2 and the cover body 3, a clamping piece 21 is arranged on a first side surface of an opening of the box body 2, the clamping piece 21 is of a boss structure, and the boss structure extends from the first side surface of the box body 2 to a direction away from the box body 2; besides, the latch 21 may have a hook-like structure. Correspondingly, a buckling part 32 is arranged on the first side surface of the cover body 3, the buckling part 32 and the card 21 are mutually buckled and connected, in this embodiment, the buckling part 32 is a circular shaft structure, and a peripheral wall surface of the circular shaft structure is abutted against a bottom surface of the card 21.
Next, a fastening member 22 is disposed on the second side surface of the opening of the box body 2, the second side surface of the box body 2 is disposed opposite to the first side surface of the box body 2, the fastening member 22 may be a flanging structure or a fastening hole structure, and in this embodiment, the fastening member 22 is a fastening hole. Accordingly, a hook portion 33 is rotatably connected to the second side surface of the cover 3, the hook portion 33 is in snap-fit connection with the snap member 22, in the present embodiment, the hook portion 33a of the hook portion 33 is snapped into the snap hole, and the hook portion 33a of the hook portion 33 abuts against the inner wall surface of the snap hole. The hook portion 33 is provided with a fourth connection hole 33b, the fourth connection hole 33b has an internal thread, and the hook portion 33a and the fourth connection hole 33b are located on both sides of the rotation axis of the hook portion 33 on the lid body 3. A locker 33c is threadedly coupled to the fourth coupling hole 33b, and the locker 33c has an external thread to be threadedly coupled to the fourth coupling hole 33 b. The top of the cover 3 is provided with a pressing surface 33d, the pressing surface 33d is disposed on the moving track of the locking member 33c, and the pressing surface 33d is located between the fastening portion 32 and the hook portion 33.
In the process of locking the cover 3 and the box body 2, firstly, the buckling part 32 and the clamping part 21 are buckled with each other, and meanwhile, the cover 3 is covered at the opening of the box body 2; then, the locking member 33c is rotated to urge the locking member 33c to move toward the abutting surface 33 d; after the end surface of the locking member 33c abuts against the abutting surface 33d, the locking member 33c continues to rotate, and because the locking member 33c only rotates and does not move, under the effect of threaded connection between the locking member 33c and the fourth connecting hole 33b, the rotation of the locking member 33c can drive one end of the hook portion 33a of the hook portion 33 to rotate towards the direction away from the abutting surface 33d, that is, the rotation of the locking member 33c can drive the hook portion 33a of the hook portion 33 to rotate towards the buckling member 22, so that the cover 3 and the box body 2 are firmly locked together.
Further, a guide hole 33e is provided at the top of the lid body 3, the guide hole 33e is provided on the moving locus of the lock member 33c, the closed end face of the guide hole 33e constitutes the above-mentioned abutting face 33d, and the diameter of the guide hole 33e is larger than that of the fourth attaching hole 33 b. The guide hole 33e guides the movement of the locking member 33c, and the position where the locking member 33c abuts against the abutting surface 33d can be determined, which contributes to the improvement of the locking force.
Referring to fig. 1 to 9, the unmanned aerial vehicle type ammunition discharging device further includes a controller (not shown), a first connection terminal 4, and a second connection terminal 5. Wherein the controller is operable to be mounted on a mobile device, the controller being operable to control firing of the ammunition. The first wiring terminal 4 is disposed on the connecting bracket 1, and in this embodiment, the first wiring terminal 4 is an existing floating terminal, and the design can avoid the occurrence of loose wiring caused by vibration of the mobile device. The second connection terminal 5 is provided on the top of the cover 3, and in this embodiment, the second connection terminal 5 is also an existing floating terminal. And the controller is connected with one end of the first wiring terminal 4 through an electric wire, and the other end of the first wiring terminal 4 is inserted into one end of the second wiring terminal 5.
The above-mentioned embodiments only express several embodiments of the present invention, and the description thereof is more specific and detailed, but not construed as limiting the scope of the invention. It should be noted that, for a person skilled in the art, several variations and modifications can be made without departing from the inventive concept, which falls within the scope of the present invention.
Claims (8)
1. The utility model provides an unmanned aerial vehicle system ammunition throwing device which characterized in that, unmanned aerial vehicle system ammunition throwing device includes:
the connecting device comprises a connecting bracket (1), wherein two first hanging pieces (12) are arranged on the connecting bracket (1), a limiting piece (12d) is arranged at the first end of each first hanging piece (12), a pressing piece (13) is arranged at the second end of each first hanging piece (12), and each pressing piece (13) is provided with a first working position and a second working position;
the top surface of the cover body (3) is provided with two second hanging pieces (31), and the two second hanging pieces (31) are respectively hung with the two first hanging pieces (12);
when the pressing piece (13) is located at a first working position, the limiting piece (12d) abuts against a first end of the second hanging piece (31), the pressing piece (13) abuts against a second end of the second hanging piece (31), and the cover body (3) and the connecting support (1) are located in a locking state;
when the press piece (13) is in the second working position, the press piece (13) does not abut against the second end of the second hanging piece (31), the second end of the first hanging piece (12) is open, and the connecting bracket (1) can slide in or slide out from the second end of the first hanging piece (12);
the unmanned aerial vehicle standard ammunition throwing device also comprises a box body (2), and the cover body (3) covers the opening of the box body (2);
two side surfaces of the opening of the box body (2) are respectively provided with a clamping piece (21) and a clamping piece (22), and the clamping piece (21) and the clamping piece (22) are arranged oppositely; a buckling part (32) and a clamping hook part (33) are arranged on the cover body (3), the buckling part (32) is connected with the clamping piece (21) in a buckling mode, the clamping hook part (33) is connected to the cover body (3) in a rotating mode, the clamping hook part (33) is provided with a hook part (33a) and a fourth connecting hole (33b), the hook part (33a) and the fourth connecting hole (33b) are respectively arranged on two sides of the rotating axis of the clamping hook part (33), the hook part (33a) is connected with the clamping piece (22) in a buckling mode, a locking piece (33c) is connected to the fourth connecting hole (33b) in a threaded mode, and a pressing surface (33d) is arranged on the moving track of the locking piece (33 c); after the locking piece (33c) abuts against the abutting surface (33d), rotating the locking piece (33c), wherein one end, away from the hook part (33a), of the clamping hook part (33) rotates along the direction of the locking piece (33c) away from the abutting surface (33d), and the hook part (33a) rotates towards the direction of the clamping piece (22) so that the hook part (33a) is connected with the clamping piece (22) in a clamping manner;
a guide hole (33e) is formed in the moving track of the locking piece (33c), one end of the guide hole (33e) is opened to allow the locking piece (33c) to enter, and the other end of the guide hole (33e) is closed to form the abutting surface (33 d);
the pressing surface (33d) is arranged on the cover body (3), and the pressing surface (33d) is positioned at the top of the cover body (3); the guide hole (33e) is arranged on the cover body (3), and the guide hole (33e) is positioned at the top of the cover body (3);
the clamping piece (21) is of a boss structure or a hook structure, and the buckling part (32) is of a round shaft structure;
the buckling piece (22) is of a flanging structure or a buckling hole structure;
the aperture of the guide hole (33e) is larger than that of the fourth connecting hole (33 b);
the unmanned aerial vehicle standard ammunition throwing device further comprises a controller, a first wiring terminal (4) and a second wiring terminal (5), wherein the controller is used for controlling ammunition emission, the first wiring terminal (4) is arranged on the connecting support (1), the first wiring terminal (4) is in a floating end shape, the second wiring terminal (5) is arranged at the top of the cover body (3), the second wiring terminal (5) is a floating terminal, the controller is connected with one end of the first wiring terminal (4) through an electric wire, and the other end of the first wiring terminal (4) is connected with one end of the second wiring terminal (5) in an inserting mode.
2. The unmanned aerial vehicle system ammunition launching device of claim 1, characterized in that:
the first hanger (12) has a first notch (12a), when the first hanger (12) and the second hanger (31) are hung on each other, a part of the second hanger (31) is positioned in the first notch (12a), and a part of the second hanger (31) is butted with the first notch (12 a);
the second hanger (31) has a second notch (31a) in which a portion of the first hanger (12) is located when the first hanger (12) and the second hanger (31) are hung on each other, and the portion of the first hanger (12) and the second notch (31a) are hung on each other.
3. The unmanned aerial vehicle system ammunition launching device of claim 2, characterized in that: the first hanging piece (12) is provided with a first extending piece (12b) and a second extending piece (12c), the first extending piece (12b) extends vertically downwards from the bottom surface of the connecting bracket (1), the second extending piece (12c) extends horizontally outwards from the lower end of the first extending piece (12b), and the bottom surface of the connecting bracket (1), the first extending piece (12b) and the second extending piece (12c) form the first notch (12a) together.
4. The unmanned aerial vehicle system ammunition launching device of claim 3, characterized in that:
the second hanging piece (31) is provided with a third extending piece (31b) and a fourth extending piece (31c), the third extending piece (31b) extends vertically upwards from the top surface of the cover body (3), the fourth extending piece (31c) extends horizontally inwards from the upper end of the third extending piece (31b), and the top surface of the cover body (3), the third extending piece (31b) and the fourth extending piece (31c) form a second notch (31a) together;
when the first and second hanging members (12, 31) are hung on each other, the end portion of the second extension member (12c) is located in the second recess (31a), and the end portion of the fourth extension member (31c) is located in the first recess (12 a).
5. The unmanned aerial vehicle system ammunition launching device of claim 1, characterized in that:
the first hanging piece (12) is of a strip-shaped rail structure with a guiding function;
the second hanging piece (31) is of a strip-shaped rail structure with a guiding function.
6. The unmanned aerial vehicle system ammunition launching device of claim 1, characterized in that: a second connecting hole (14) is formed in the connecting support (1), and the second connecting hole (14) is provided with an internal thread; the pressing piece (13) is rotatably connected to the connecting support (1) through a rotating shaft (13a), a third connecting hole (13b) which can correspond to the second connecting hole (14) is formed in the pressing piece (13), a bolt (13c) is arranged in the third connecting hole (13b), and the bolt (13c) is in threaded connection with the second connecting hole (14);
the bolt (13c) is also threadedly connected with the third connecting hole (13 b).
7. The unmanned aerial vehicle system ammunition launching device of claim 1, characterized in that: a second connecting hole (14) is formed in the connecting support (1), and the second connecting hole (14) is of a hemispherical groove structure; the pressing piece (13) is rotatably connected to the connecting support (1) through a rotating shaft (13a), a third connecting hole (13b) which can correspond to the second connecting hole (14) is formed in the pressing piece (13), a glass bead screw is connected to the third connecting hole (13b) in an internal thread mode, and the glass bead screw is connected with the second connecting hole (14) in a buckling mode.
8. The unmanned aerial vehicle system ammunition launching device of claim 1, characterized in that: be provided with first connecting hole (11) on linking bridge (1) install anticreep screw (11a) in first connecting hole (11), the one end of first connecting hole (11) can with anticreep screw (11a) threaded connection, the other end cover of first connecting hole (11) is established outside on anticreep screw (11 a).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105270646A (en) * | 2015-11-16 | 2016-01-27 | 湖南云顶智能科技有限公司 | Holder device of unmanned airplane |
| CN107021224A (en) * | 2017-04-28 | 2017-08-08 | 深圳市轻准科技有限公司 | Hang down and throw howitzer unmanned plane |
| CN206645037U (en) * | 2017-02-05 | 2017-11-17 | 深圳一电航空技术有限公司 | Head Quick-disassembling mechanism and unmanned plane |
| CN107985618A (en) * | 2017-11-20 | 2018-05-04 | 南京拓威航空科技有限公司 | A kind of quick-disassembly structure, holder and unmanned vehicle |
| CN110053776A (en) * | 2019-05-15 | 2019-07-26 | 浙江临航智能科技有限公司 | A kind of unmanned plane service ammunition delivery device |
| CN111824438A (en) * | 2020-07-07 | 2020-10-27 | 哈瓦国际航空技术（深圳）有限公司 | Quick detach device and unmanned aerial vehicle |
| CN112239031A (en) * | 2019-07-19 | 2021-01-19 | 南通中集特种运输设备制造有限公司 | Top cover and container comprising same |
-
2021
- 2021-11-19 CN CN202111407977.1A patent/CN113911362B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105270646A (en) * | 2015-11-16 | 2016-01-27 | 湖南云顶智能科技有限公司 | Holder device of unmanned airplane |
| CN206645037U (en) * | 2017-02-05 | 2017-11-17 | 深圳一电航空技术有限公司 | Head Quick-disassembling mechanism and unmanned plane |
| CN107021224A (en) * | 2017-04-28 | 2017-08-08 | 深圳市轻准科技有限公司 | Hang down and throw howitzer unmanned plane |
| CN107985618A (en) * | 2017-11-20 | 2018-05-04 | 南京拓威航空科技有限公司 | A kind of quick-disassembly structure, holder and unmanned vehicle |
| CN110053776A (en) * | 2019-05-15 | 2019-07-26 | 浙江临航智能科技有限公司 | A kind of unmanned plane service ammunition delivery device |
| CN112239031A (en) * | 2019-07-19 | 2021-01-19 | 南通中集特种运输设备制造有限公司 | Top cover and container comprising same |
| CN111824438A (en) * | 2020-07-07 | 2020-10-27 | 哈瓦国际航空技术（深圳）有限公司 | Quick detach device and unmanned aerial vehicle |
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|---|---|
| CN113911362A (en) | 2022-01-11 |
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