CN111204461A - Unmanned aerial vehicle and artillery mounting rack thereof - Google Patents
Unmanned aerial vehicle and artillery mounting rack thereof Download PDFInfo
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- CN111204461A CN111204461A CN202010179511.XA CN202010179511A CN111204461A CN 111204461 A CN111204461 A CN 111204461A CN 202010179511 A CN202010179511 A CN 202010179511A CN 111204461 A CN111204461 A CN 111204461A
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- 230000003014 reinforcing effect Effects 0.000 claims abstract description 25
- 238000003780 insertion Methods 0.000 claims description 6
- 230000037431 insertion Effects 0.000 claims description 6
- 230000000712 assembly Effects 0.000 claims 1
- 238000000429 assembly Methods 0.000 claims 1
- 230000002787 reinforcement Effects 0.000 abstract description 2
- 238000009434 installation Methods 0.000 description 6
- 230000005540 biological transmission Effects 0.000 description 3
- 230000006978 adaptation Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 206010040007 Sense of oppression Diseases 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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- 230000000750 progressive effect Effects 0.000 description 1
- 239000013585 weight reducing agent Substances 0.000 description 1
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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
- B64D7/00—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft
- B64D7/08—Arrangements of rocket launchers or releasing means
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Abstract
The invention discloses an artillery mounting rack of an unmanned aerial vehicle, which comprises an artillery barrel clamp, an artillery barrel clamp cover and a weapon hanging rack connector; the gun barrel is clamped and fixed on the tube weapon frame; the pipe weapon frame is fixedly connected with a landing gear reinforcing pipe of the unmanned aerial vehicle; the gun barrel clamping cover is used for clamping and matching with the gun barrel and clamping and fixing the gun barrel; the gun barrel clamping cover is fixedly connected with the gun barrel clamp through a fixing piece; weapon stores pylon connector and control weapon frame fixed connection, and weapon stores pylon connector is used for fixing at unmanned aerial vehicle's fuselage side. In this unmanned aerial vehicle's artillery mounting bracket, weapon stores pylon connector is used for fixing in unmanned aerial vehicle's fuselage side to this artillery mounting bracket's control weapon frame and unmanned aerial vehicle's undercarriage reinforcement pipe fixed connection, this artillery mounting bracket has two position connections with unmanned aerial vehicle promptly, ensures that the barrel is reliably installed. The invention also discloses an unmanned aerial vehicle, which applies the artillery mounting frame to ensure the reliable assembly of the gun barrel.
Description
Technical Field
The invention relates to the technical field of aircrafts, in particular to a gun mounting rack of an unmanned aerial vehicle and the unmanned aerial vehicle.
Background
The gun barrel on the unmanned aerial vehicle is directly installed below the body of the unmanned aerial vehicle and is installed in parallel. However, the gun barrel is only connected with the base below the machine body through the mounting frame, the connecting positions are few, and the mounting reliability is poor. Therefore, how to reliably assemble the gun barrel on the unmanned aerial vehicle is a problem to be solved by the technical personnel in the field.
Disclosure of Invention
In view of the above, the invention provides an artillery mounting rack of an unmanned aerial vehicle, wherein a weapon hanger connector of the artillery mounting rack is used for being fixed on the side surface of a body of the unmanned aerial vehicle, and a tube weapon frame of the artillery mounting rack is fixedly connected with a landing gear reinforcing tube of the unmanned aerial vehicle, namely the artillery mounting rack is respectively connected with two positions of the unmanned aerial vehicle, so that reliable installation is ensured. The invention further provides an unmanned aerial vehicle, and the gun mounting frame is applied to guarantee reliable installation of the gun barrel.
In order to achieve the purpose, the invention provides the following technical scheme:
an unmanned aerial vehicle's gun mounting bracket includes:
the gun barrel clamp is fixed on the tube weapon frame; the pipe weapon frame is fixedly connected with the landing gear reinforcing pipe of the unmanned aerial vehicle;
the gun barrel clamping cover is used for clamping and fixing the gun barrel in a clamping fit manner with the gun barrel; the gun barrel clamping cover is fixedly connected with the gun barrel clamp through a fixing piece;
a weapon rack connector, the weapon rack connector with tube weapon rack fixed connection, just the weapon rack connector is used for fixing unmanned aerial vehicle's fuselage side.
Preferably, in the artillery mounting frame, the lower end of the tube weapon frame is connected with a fixed connector, and the fixed connector is fixedly connected with the undercarriage reinforcing tube through a connecting column.
Preferably, in the artillery mounting frame, two ends of the connecting column are respectively in plug-in fit with the fixed connector and the undercarriage reinforcing pipe; the outer diameter of the connecting column is equal to the inner diameter of the insertion hole of the fixed connector and the inner diameter of the insertion hole of the landing gear reinforcing pipe.
Preferably, in the artillery mounting frame, two ends of the connecting column are respectively and fixedly connected with the fixed connector and the undercarriage reinforcing pipe through fixing pieces.
Preferably, in the gun mounting rack, the gun barrel clamp and the gun barrel clamp cover are fixed to each other to form two sets of clamping components.
Preferably, in the artillery mounting frame, the artillery tube clamp is of a block structure with a preset height, one end of the artillery tube clamp in the height direction is fixedly connected with the tube weapon frame, and the other end of the artillery tube clamp in the height direction is provided with an arc-shaped notch for fitting the artillery tube; the gun barrel clamping cover is arc-shaped and is used for being attached to the outer wall of the gun barrel.
Preferably, in the above-mentioned artillery mounting bracket, the weapon stores pylon connector pass through the mounting with control weapon frame fixed connection, the weapon stores pylon connector is used for fixing through the mounting unmanned aerial vehicle's fuselage side.
The utility model provides an unmanned aerial vehicle, includes the artillery mounting bracket, the artillery mounting bracket be any one in the above-mentioned technical scheme artillery mounting bracket.
Preferably, among the above-mentioned unmanned aerial vehicle, be fixed with the mounting panel on unmanned aerial vehicle's the fuselage, weapon stores pylon connector is fixed in through the mounting panel.
Preferably, among the above-mentioned unmanned aerial vehicle, unmanned aerial vehicle is the unmanned helicopter of two rotor wings in alternately.
The invention provides an unmanned aerial vehicle artillery mounting frame which comprises an artillery barrel clamp, an artillery barrel clamp cover and a weapon hanging frame connector; the gun barrel is clamped and fixed on the tube weapon frame; the pipe weapon frame is fixedly connected with a landing gear reinforcing pipe of the unmanned aerial vehicle; the gun barrel clamping cover is used for clamping and matching with the gun barrel and clamping and fixing the gun barrel; the gun barrel clamping cover is fixedly connected with the gun barrel clamp through a fixing piece; weapon stores pylon connector and control weapon frame fixed connection, and weapon stores pylon connector is used for fixing at unmanned aerial vehicle's fuselage side.
In the artillery mounting frame of the unmanned aerial vehicle, the weapon hanger connector is used for being fixed on the side face of the unmanned aerial vehicle body, and the pipe weapon frame of the artillery mounting frame is fixedly connected with the undercarriage reinforcing pipe of the unmanned aerial vehicle, namely the artillery mounting frame is connected with the unmanned aerial vehicle at two positions, so that the gun pipes are guaranteed to be reliably mounted.
The invention further provides an unmanned aerial vehicle, and the gun mounting frame is applied to guarantee reliable assembly of the gun barrel.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.
Fig. 1 is a schematic perspective view of a gun mounting rack of an unmanned aerial vehicle according to an embodiment of the present invention;
fig. 2 is a schematic side view of a gun mounting rack of the unmanned aerial vehicle according to the embodiment of the present invention;
wherein, in fig. 1-2:
a gun barrel 1; a gun barrel clamp 2; a tube control weapon frame 3; a gun barrel clamping cover 4; a fixed connector 5; a connecting column 6; a weapon rack connector 7; landing gear reinforcing tube 8.
Detailed Description
The embodiment of the invention discloses an artillery mounting rack of an unmanned aerial vehicle, wherein a weapon rack connector of the artillery mounting rack is fixed on the side surface of a machine body of the unmanned aerial vehicle, and a pipe weapon rack of the artillery mounting rack is fixedly connected with an undercarriage reinforcing pipe of the unmanned aerial vehicle, namely the artillery mounting rack is respectively connected with two positions of the unmanned aerial vehicle, so that reliable mounting is ensured. The embodiment of the invention also discloses an unmanned aerial vehicle, which applies the artillery mounting frame to ensure that a gun barrel is reliably mounted.
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-2, an embodiment of the present invention provides an unmanned aerial vehicle artillery mounting rack, including an artillery barrel clamp 2, an artillery barrel clamp cover 4, and a weapon hanger connector 7; the cannon pipe clamp 2 is fixed on the cannon pipe rack 3; the pipe weapon frame 3 is fixedly connected with an undercarriage reinforcing pipe 8 of the unmanned aerial vehicle; the gun barrel clamping cover 4 is used for matching with the gun barrel clamp 2 and clamping and fixing the gun barrel 1; the gun barrel clamp cover 4 is fixedly connected with the gun barrel clamp 2 through a fixing piece; weapon stores pylon connector 7 and control weapon frame 3 fixed connection, and weapon stores pylon connector 7 is used for fixing at unmanned aerial vehicle's fuselage side.
In the artillery mounting frame of the unmanned aerial vehicle, the weapon hanger connector 7 is used for being fixed on the side face of the unmanned aerial vehicle body, and the tube weapon frame 3 of the artillery mounting frame is fixedly connected with the undercarriage reinforcing tube 8 of the unmanned aerial vehicle, namely the artillery mounting frame is connected with the unmanned aerial vehicle at two positions, so that compared with the installation mode of the gun tube 1 in the prior art, the reliable installation of the gun tube 1 can be ensured.
In addition, the gun barrel among the prior art is installed in unmanned aerial vehicle fuselage bottom, can produce the flare when owing to the gun barrel transmission, so the gun barrel dress will keep away from engine and oil circuit in the unmanned aerial vehicle below, lead to the gun barrel to keep away from unmanned aerial vehicle's base in the below, it has certain distance to cause the mounting bracket to have from the base, such condition makes whole gun barrel mounting bracket comparatively heavy, influence unmanned aerial vehicle's flight performance, and the gun mounting bracket that this embodiment provided is installed in the side of fuselage, keep away from engine and the oil circuit of unmanned aerial vehicle bottom, the structure is simpler, light in weight, do benefit to the wholeness ability that improves unmanned aerial vehicle.
In the above artillery mounting rack, the lower end of the tube weapon frame 3 is connected with the fixed connector 5, and the fixed connector 5 is fixedly connected with the undercarriage reinforcing tube 8 through the connecting column 6. Two ends of the connecting column 6 are respectively matched with the fixed connector 5 and the landing gear reinforcing pipe 8 in a plugging manner; the outer diameter of the connecting column 6 is equal to the inner diameter of an insertion hole matched with the connecting column 6 in the fixed connector 5, and the inner diameter of an insertion hole matched with the connecting column 6 in the undercarriage reinforcing pipe 8. The both ends of spliced pole 6 are respectively through mounting and fixed connector 5 and undercarriage reinforcing tube 8 fixed connection, and above-mentioned mounting is the screw to the screw passes through aviation locknut fastening.
The gun barrel clamp 2 is of a block structure with a preset height, and one end of the gun barrel clamp 2 in the height direction is fixedly connected with the pipe weapon frame 3 through a screw; the other end of the gun barrel clamp 2 along the height direction is provided with an arc-shaped notch, and the arc-shaped notch is used for being attached to the gun barrel 1; the gun barrel clamping cover 4 is arc-shaped and is used for being attached to the outer wall of the gun barrel 1. Be equipped with on the barrel clamp 2 with the screw complex screw hole of connecting barrel clamp 2 and pipe control weapon frame 3, this screw hole sets up along the great position of direction of height size on barrel clamp 2, and the length of the screw of being convenient for sets up to longer to great recoil when 1 transmission of adaptation barrel avoids the screw to influence the installation of barrel 1 again.
Weapon stores pylon connector 7 passes through mounting and control weapon frame 3 fixed connection, and weapon stores pylon connector 7 is used for fixing at unmanned aerial vehicle's fuselage side through the mounting.
In as the embodiment provides, barrel clamp 2 links together through the screw hole of upper end and control weapon frame 3, and control weapon frame 3 is together fixed with weapon stores pylon connector 7 through upper end screw hole, and control weapon frame 3 is together fixed with fixed connector 5 through lower extreme screw hole, and fixed connector 5 is connected to together through spliced pole 6 and undercarriage reinforcement pipe 8, and weapon stores pylon connector 7 lug connection is to the side of organism, and direct mode through rigid connection is connected to unmanned aerial vehicle like this. The arc size of barrel card 2 and barrel card lid 4 and barrel 1 adaptation ensure that barrel 1 tightly fixes on unmanned aerial vehicle.
In the gun mounting bracket provided by the embodiment, each fixing piece is a screw, and each screw is fastened through an aviation locknut. The two parts connected by the screw are respectively provided with a threaded hole matched with the screw, specifically, the upper end of the cannon barrel clamp 2 is provided with a threaded hole, and the tubular weapon frame 3 is provided with a threaded hole with the same size as the cannon barrel clamp 2; the upper end of one side of the tube weapon frame 3 is provided with three screw holes with the same size, and one end of the weapon hanging frame connector 7 is also provided with screw holes with the same size and number; the lower extreme of 3 one ends of pipe control weapon frame is equipped with two equidimension screw holes, and fixed connector 5 one end also is equipped with the screw hole of equidimension and quantity. The radius of the outer ring of the fixed connector 5 is exactly equal to the radius of the inner ring at the lower end of the tube weapon frame 3, and the fixed connector can be directly inserted into the tube weapon frame 3 and is fastened and connected through screws and aviation locknuts; threaded holes with the same size are formed in the two ends of the connecting column 6. The gun barrel clamp 2 and the gun barrel clamp cover 4 are fixedly connected with an aviation nut through screws; the cannon tube clamp 2 is fixedly connected with the cannon tube rack 3 through screws; the pipe weapon frame 3 and the weapon hanger connector 7 are fixed with an aviation locknut through screws; the pipe control weapon frame 3 and the fixed connector 5 are fixed with the aviation locknut through screws; the fixed connector 5 and the connecting column 6 are fixed with the aviation locknut through screws; the connecting column 6 and the landing gear reinforcing pipe 8 are fixed with an aviation locknut through screws; through the setting, the occupied space and the weight of the gun mounting rack are effectively reduced, and the overall performance of the unmanned aerial vehicle is further improved.
The weapon pylon connector 7 and the landing gear reinforcing tube 8 have a spatial difference, which depends on the width of the helicopter body.
The gun barrel 1, the gun barrel clamp 2, the tube weapon frame 3, the gun barrel clamp cover 4, the fixed connector 5, the connecting column 6, the weapon hanger connector 7 and the falling rack reinforcing tube 8 are respectively parts made of rigid materials.
In the unmanned helicopter artillery mounting frame provided by the embodiment of the invention, different parts are respectively and rigidly connected, so that the mounting firmness of the artillery tube 1 can be ensured, the influence on the initial mounting position of the artillery tube 1 due to flight vibration and artillery recoil is avoided, and the reduction of the launching accuracy of the artillery tube 1 is prevented; simultaneously, this artillery mounting bracket just directly is fixed to unmanned aerial vehicle with gun barrel 1 tightly through seven rigid material on, and occupation space is less, has simplified the structure, and weight reduction has improved unmanned aerial vehicle's wholeness ability.
The embodiment of the invention also provides an unmanned aerial vehicle which comprises the artillery mounting frame, wherein the artillery mounting frame is the artillery mounting frame provided by the embodiment. Specifically, the hanger connector 7 is fixed on the left side of the unmanned aerial vehicle. A mounting plate is fixed on the body of the unmanned aerial vehicle, and a weapon hanger connector 7 is fixed on the mounting plate through a fixing piece; the mounting plate has a threaded hole of the same size as the threaded hole of the weapon rack connector 7. The mounting panel links to each other through the bolt with weapon stores pylon connector 7 is preferred, improves weapon stores pylon connector 7 and unmanned aerial vehicle's stability of being connected.
The unmanned aerial vehicle is an unmanned helicopter, in particular to a crossed double-rotor unmanned helicopter.
The unmanned aerial vehicle that this embodiment provided has used the artillery mounting bracket that above-mentioned embodiment provided, ensures that barrel 1 installs reliably. Certainly, the unmanned aerial vehicle that this embodiment provided still has the other effects of the artillery mounting bracket that above-mentioned embodiment provided, and no longer repeated here.
The embodiments in the present description are described in a progressive manner, each embodiment focuses on differences from other embodiments, and the same and similar parts among the embodiments are referred to each other.
The previous description of the disclosed embodiments is provided to enable any person skilled in the art to make or use the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other embodiments without departing from the spirit or scope of the invention. Thus, the present invention is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
Claims (10)
1. The utility model provides an unmanned aerial vehicle's gun mounting bracket which characterized in that includes:
the gun barrel clamp is fixed on the tube weapon frame; the pipe weapon frame is fixedly connected with the landing gear reinforcing pipe of the unmanned aerial vehicle;
the gun barrel clamping cover is used for clamping and fixing the gun barrel in a clamping fit manner with the gun barrel; the gun barrel clamping cover is fixedly connected with the gun barrel clamp through a fixing piece;
a weapon rack connector, the weapon rack connector with tube weapon rack fixed connection, just the weapon rack connector is used for fixing unmanned aerial vehicle's fuselage side.
2. The artillery mounting bracket of claim 1, wherein a fixed connector is connected to the lower end of the tube weapon frame and is fixedly connected to the undercarriage reinforcing tube through a connecting column.
3. The artillery mount according to claim 2, wherein two ends of the connecting column are respectively in plug-fit engagement with the fixed connector and the landing gear reinforcing tube; the outer diameter of the connecting column is equal to the inner diameter of the insertion hole of the fixed connector and the inner diameter of the insertion hole of the landing gear reinforcing pipe.
4. The artillery mount according to claim 3, wherein two ends of the connecting column are fixedly connected with the fixed connector and the landing gear reinforcing tube through fixing pieces respectively.
5. The artillery mount of claim 1, wherein the barrel clamp and the barrel clamp cover are secured to one another to form two sets of clamp assemblies.
6. The artillery mounting rack according to claim 1 or 5, wherein the artillery barrel clamp is of a block-shaped structure with a preset height, one end of the artillery barrel clamp in the height direction is fixedly connected with the tube weapon frame, and the other end of the artillery barrel clamp in the height direction is provided with an arc-shaped notch for fitting the artillery barrel; the gun barrel clamping cover is arc-shaped and is used for being attached to the outer wall of the gun barrel.
7. The artillery mount of claim 1, wherein the weapon rack connector is fixedly connected with the tube weapon rack by a fastener, and the weapon rack connector is used for being fixed on the side of the unmanned aerial vehicle body by a fastener.
8. An unmanned aerial vehicle comprising a gun mount, wherein the gun mount is as claimed in any one of claims 1 to 7.
9. The unmanned aerial vehicle of claim 8, wherein a mounting plate is fixed to the body of the unmanned aerial vehicle, and the weapon pylon connector is fixed to the mounting plate by a fixing member.
10. The drone of claim 8, wherein the drone is a cross-twin rotor drone.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010179511.XA CN111204461A (en) | 2020-03-13 | 2020-03-13 | Unmanned aerial vehicle and artillery mounting rack thereof |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010179511.XA CN111204461A (en) | 2020-03-13 | 2020-03-13 | Unmanned aerial vehicle and artillery mounting rack thereof |
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| CN111204461A true CN111204461A (en) | 2020-05-29 |
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| CN202010179511.XA Pending CN111204461A (en) | 2020-03-13 | 2020-03-13 | Unmanned aerial vehicle and artillery mounting rack thereof |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114030626A (en) * | 2021-11-30 | 2022-02-11 | 北京航星机器制造有限公司 | Hanging rack not prone to fracture, unmanned aerial vehicle and method for hanging articles on unmanned aerial vehicle |
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| CN107875540A (en) * | 2017-11-29 | 2018-04-06 | 天长航空技术有限公司 | It is a kind of to patrol the integral unmanned plane that disappears |
| CN109665104A (en) * | 2018-12-18 | 2019-04-23 | 哈瓦国际航空技术（深圳）有限公司 | A kind of ejecting gun and unmanned plane |
| CN110271669A (en) * | 2019-06-18 | 2019-09-24 | 深圳高度创新技术有限公司 | Fire control and disaster rescue unmanned plane |
| CN211766324U (en) * | 2020-03-13 | 2020-10-27 | 北京清航紫荆装备科技有限公司 | Unmanned aerial vehicle and artillery mounting rack thereof |
-
2020
- 2020-03-13 CN CN202010179511.XA patent/CN111204461A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107875540A (en) * | 2017-11-29 | 2018-04-06 | 天长航空技术有限公司 | It is a kind of to patrol the integral unmanned plane that disappears |
| CN109665104A (en) * | 2018-12-18 | 2019-04-23 | 哈瓦国际航空技术（深圳）有限公司 | A kind of ejecting gun and unmanned plane |
| CN110271669A (en) * | 2019-06-18 | 2019-09-24 | 深圳高度创新技术有限公司 | Fire control and disaster rescue unmanned plane |
| CN211766324U (en) * | 2020-03-13 | 2020-10-27 | 北京清航紫荆装备科技有限公司 | Unmanned aerial vehicle and artillery mounting rack thereof |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114030626A (en) * | 2021-11-30 | 2022-02-11 | 北京航星机器制造有限公司 | Hanging rack not prone to fracture, unmanned aerial vehicle and method for hanging articles on unmanned aerial vehicle |
| CN114030626B (en) * | 2021-11-30 | 2024-04-05 | 北京航星机器制造有限公司 | Difficult-to-break hanging frame, unmanned aerial vehicle and method for hanging articles on unmanned aerial vehicle |
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