CN114379785A - Hasp structure, carry on platform and unmanned aerial vehicle - Google Patents
Hasp structure, carry on platform and unmanned aerial vehicle Download PDFInfo
- Publication number
- CN114379785A CN114379785A CN202111667479.0A CN202111667479A CN114379785A CN 114379785 A CN114379785 A CN 114379785A CN 202111667479 A CN202111667479 A CN 202111667479A CN 114379785 A CN114379785 A CN 114379785A
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- locking
- handle
- unmanned aerial
- aerial vehicle
- central shaft
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- 230000005540 biological transmission Effects 0.000 claims abstract description 29
- 230000005489 elastic deformation Effects 0.000 claims description 2
- 238000010276 construction Methods 0.000 claims 2
- 230000009286 beneficial effect Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000009434 installation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000005191 phase separation Methods 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
- B64D7/00—Arrangement of military equipment, e.g. armaments, armament accessories or military shielding, in aircraft; Adaptations of armament mountings for aircraft
- B64D7/02—Arrangement of military equipment, e.g. armaments, armament accessories or military shielding, in aircraft; Adaptations of armament mountings for aircraft the armaments being firearms
- B64D7/06—Arrangement of military equipment, e.g. armaments, armament accessories or military shielding, in aircraft; Adaptations of armament mountings for aircraft the armaments being firearms movably mounted
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
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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
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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 discloses a lock catch structure, a carrying platform and an unmanned aerial vehicle, which comprise a support, a lock catch piece and a rotary handle, wherein the support is used for assembling the carrying platform and is provided with a first lug and a second lug; the lock catch piece comprises a lock catch part and an elastic part, the lock catch part is rotatably connected with the first lug around the first central shaft and is used for hooking the unmanned aerial vehicle, one end of the elastic part is connected with the lock catch part, and the other end of the elastic part is a transmission end; the rotary handle comprises a rotating part, a transmission part and a handle part, the rotating part is rotatably connected with the second lug around the second central shaft, one end of the transmission part is connected with the rotating part, the other end of the transmission part is a driving end, the driving end and the transmission end are rotatably connected around the third central shaft, one end of the handle part is connected with the rotating part, the other end of the handle part is a handle end, and the first central shaft, the second central shaft and the third central shaft are arranged in parallel. The stable assembly of the carrying platform is ensured, and the convenience in disassembly of the carrying platform is also ensured.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to a lock catch structure, a carrying platform and an unmanned aerial vehicle.
Background
Along with the rapid development of modern military science and technology, unmanned weaponry frequently presents to modern battlefields, and the unmanned weaponry has become a development trend.
In the related art, the weaponry includes an unmanned aerial vehicle and a carrying seat, the carrying seat is carried at the bottom of the unmanned aerial vehicle and is used for carrying weapons, such as firearms or projectiles; wherein, be provided with the hasp structure on the carrying seat, the hasp structure includes support, hasp spare and torsional spring, and the hasp spare rotates with the support to be connected to and be used for with unmanned aerial vehicle's fuselage looks lock joint, torsional spring connects between support and hasp spare, be used for making the hasp spare keep with fuselage looks lock joint.
However, the unmanned aerial vehicle and the carrying seat adopt the above structure, if the torsion of the torsion spring is too large, the locking fastener is difficult to rotate, and the carrying seat is difficult to disassemble; if the torsion of torsional spring is too little, it is more convenient that the hasp piece rotates, nevertheless can't guarantee to carry the seat and can carry on unmanned aerial vehicle firmly.
Disclosure of Invention
The present invention is directed to solving at least one of the problems of the prior art. Therefore, the invention provides a lock catch structure which not only ensures the stable assembly of the carrying platform, but also ensures the convenient disassembly of the carrying platform.
The invention also provides a carrying platform with the lock catch structure.
The invention further provides an unmanned aerial vehicle with the carrying platform.
According to the hasp structure of this invention embodiment, include:
the support is used for assembling the carrying platform and is provided with a first lug and a second lug;
the locking part comprises a locking part and an elastic part, the locking part is rotatably connected with the first lug around a first central shaft and is used for hooking the unmanned aerial vehicle, one end of the elastic part is connected with the locking part, and the other end of the elastic part is a transmission end;
the rotary handle comprises a rotating part, a transmission part and a handle part, the rotating part is rotatably connected with the second lug around a second central shaft, one end of the transmission part is connected with the rotating part, the other end of the transmission part is a driving end, the driving end is rotatably connected with the transmission end around a third central shaft, one end of the handle part is connected with the rotating part, the other end of the handle part is a handle end, and the first central shaft, the second central shaft and the third central shaft are arranged in parallel;
the elastic part can be suitable for the rotation of the rotating handle to generate elastic deformation so as to enable the locking fastener to rotate around the first central shaft; the elastic part can be switched between an initial state and a deformation state, when the elastic part is in the initial state, the lock catch part is in a hooking state, and when the elastic part is in the deformation state, the lock catch part is in a disengaging state.
According to the lock catch structure provided by the embodiment of the invention, at least the following beneficial effects are achieved: through the setting of elastic part and hasp piece, the hasp piece is through the motion of restriction elastic part to the rotation of restriction hasp portion, and then guarantee that colluding of hasp portion holds the end and can stabilize and collude and hold in unmanned aerial vehicle, from this, carry on the platform and can carry on unmanned aerial vehicle's bottom steadily. Through the setting of hasp piece, thereby the staff utilizes the rotation of hasp piece to overcome the elasticity of elasticity portion to make hasp portion take place the rotation, and break away from unmanned aerial vehicle, from this, it is more convenient that mounting platform dismantles.
According to some embodiments of the invention, the distance between the handle end and the second central axis is greater than the distance between the drive end and the second central axis.
According to some embodiments of the invention, a distance between the driving end and the second central axis is greater than a distance between the driving end and the first central axis.
According to some embodiments of the present invention, one end of the locking portion is rotatably connected to the first protrusion, and the other end of the locking portion is a hooking end, and a distance between the hooking end and the first central axis is greater than a distance between the transmission end and the first central axis.
According to some embodiments of the present invention, one end of the locking portion is rotatably connected to the first lug, and the other end of the locking portion is a hooking end, and a distance between the handle end and the second central axis is greater than a distance between the hooking end and the first central axis. .
According to a second aspect of the present invention, a platform includes:
the lock catch structure is described above;
the lock catch structure is arranged on the carrying seat;
the frame subassembly, with carry on seat assembled connection for assemble gun, wherein, the frame subassembly along predetermineeing the adjustable setting in carry on the seat to make gun can follow self length direction and adjust.
The carrying platform provided by the embodiment of the invention at least has the following beneficial effects: when unmanned aerial vehicle assembles, gun carries on the skeleton subassembly, and the skeleton subassembly assembles on carrying the seat, carries the seat and carries the bottom in unmanned aerial vehicle, so to carry gun in unmanned aerial vehicle's below. Wherein, the skeleton subassembly can be adjusted along predetermineeing the direction, consequently, when the staff is at the test rifle accurate nature when using, the skeleton subassembly is adjusted on carrying the seat along predetermineeing the direction to make gun adjust along self length direction, and then make gun adjusted to suitable position, at this moment, the equilibrium of gun reaches the best, thereby make gun can aim at the target thing more stably, and carry out accurate shooting to the target thing.
According to some embodiments of the invention, the side wall of the skeleton assembly is provided with a plurality of first connecting parts at intervals along the preset direction, and the carrying seat is provided with a first assembling part which can be assembled and connected with any one of the first connecting parts.
According to some embodiments of the invention, the frame assembly comprises a body and a guide rail, the body is used for assembling the gun, the guide rail is fixedly connected with the outside of the body and is arranged along the preset direction, the guide rail is provided with the first connecting part, and the carrying seat is provided with a sliding groove matched with the guide rail; the carrying platform further comprises a locking mechanism, the locking mechanism comprises a locking piece, the locking piece is provided with a second assembling portion and a second connecting seat, the second assembling portion is in assembly connection with the first assembling portion, and the second connecting portion can be in assembly connection with any one of the first connecting portions.
According to some embodiments of the invention, the first assembling portion is a through groove opened in the carrying seat, the through groove is communicated with the sliding groove, and an inner port of the through groove is arranged towards the first connecting portion; the second assembling portion is matched with the first assembling portion in an embedded mode, and the second connecting portion is matched with the first connecting portion in an embedded mode.
According to the embodiment of the invention, the unmanned aerial vehicle comprises: a body; the carrying platform is carried at the bottom of the machine body.
The unmanned aerial vehicle provided by the embodiment of the invention at least has the following beneficial effects: when unmanned aerial vehicle assembles, gun carries on the skeleton subassembly, and the skeleton subassembly assembles on carrying the seat, carries the seat and carries the bottom in unmanned aerial vehicle, so to carry gun in unmanned aerial vehicle's below. Wherein, the skeleton subassembly can be adjusted along predetermineeing the direction, consequently, when the staff is at the test rifle accurate nature when using, the skeleton subassembly is adjusted on carrying the seat along predetermineeing the direction to make gun adjust along self length direction, and then make gun adjusted to suitable position, at this moment, the equilibrium of gun reaches the best, thereby make gun can aim at the target thing more stably, and carry out accurate shooting to the target thing.
Additional aspects and advantages of the invention will be set forth in part in the description which follows and, in part, will be obvious from the description, or may be learned by practice of the invention.
Drawings
The invention is further described with reference to the following figures and examples, in which:
FIG. 1 is a schematic view of a mounting platform and a firearm in accordance with an embodiment of the present invention;
fig. 2 is a schematic structural diagram of a latch structure according to an embodiment of the invention;
FIG. 3 is an exploded view of the latch structure according to the embodiment of the present invention;
FIG. 4 is an enlarged view of the area A of FIG. 1;
FIG. 5 is a schematic structural diagram of a skeletal assembly in accordance with an embodiment of the present invention;
FIG. 6 is an enlarged view of the area B in FIG. 5;
FIG. 7 is a schematic structural diagram of a locking member according to an embodiment of the invention.
Reference numerals:
100. a locking structure; 110. a base; 111. a first lug; 112. a second lug; 120. a fastener; 121. a locking part; 1211. a hooking end; 122. an elastic portion; 1221. a transmission end; 130. rotating the handle; 131. a rotating part; 132. a handle portion; 1321. a handle end; 133. a transmission section; 1331. a driving end; 140. a first rotating shaft; 150. a second rotating shaft; 160. a third rotating shaft; 200. a mounting platform; 210. a mounting seat; 211. a first fitting portion; 220. a skeletal assembly; 221. a sub-portion framework; 2211. a body; 2212. a guide rail; 2213. a first connection portion; 230. a locking mechanism; 231. a locking member; 2311. a second connecting portion; 2312. a second fitting portion; 232. a locking assembly; 2321. a guide bar; 2322. a limiting member; 2323. locking the handle; 300. a gun.
Detailed Description
Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the accompanying drawings are illustrative only for the purpose of explaining the present invention, and are not to be construed as limiting the present invention.
In the description of the present invention, it should be understood that the orientation or positional relationship referred to in the description of the orientation, such as the upper, lower, front, rear, left, right, etc., is based on the orientation or positional relationship shown in the drawings, and is only for convenience of description and simplification of description, and does not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention.
In the description of the present invention, the meaning of a plurality is one or more, the meaning of a plurality is two or more, and the above, below, exceeding, etc. are understood as excluding the present numbers, and the above, below, within, etc. are understood as including the present numbers. If the first and second are described for the purpose of distinguishing technical features, they are not to be understood as indicating or implying relative importance or implicitly indicating the number of technical features indicated or implicitly indicating the precedence of the technical features indicated.
In the description of the present invention, unless otherwise explicitly limited, terms such as arrangement, installation, connection and the like should be understood in a broad sense, and those skilled in the art can reasonably determine the specific meanings of the above terms in the present invention in combination with the specific contents of the technical solutions.
In the description of the present invention, reference to the description of the terms "one embodiment," "some embodiments," "an illustrative embodiment," "an example," "a specific example," or "some examples," etc., means that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the present invention. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
Disclosed is a latch structure 100 according to a first aspect of the present invention, referring to fig. 1 to 3, comprising a support, a latch member 120 and a rotating handle 130, wherein the support is used for assembling a carrying platform 200, and the support has a first lug 111 and a second lug 112; the locking part 120 comprises a locking part 121 and an elastic part 122, the locking part 121 is rotatably connected with the first lug 111 around a first central axis and is used for hooking the unmanned aerial vehicle, one end of the elastic part 122 is connected with the locking part 121, and the other end is a transmission end 1221; the rotating handle 130 comprises a rotating part 131, a transmission part 133 and a handle part 132, the rotating part 131 is rotatably connected with the second lug 112 around a second central axis, one end of the transmission part 133 is connected with the rotating part 131, the other end is a driving end 1331, the driving end 1331 is rotatably connected with a transmission end 1221 around a third central axis, one end of the handle part 132 is connected with the rotating part 131, the other end is a handle end 1321, and the first central axis and the second central axis are arranged in parallel with the third central axis; wherein, the elastic portion 122 can be adapted to elastically deform in the rotation of the rotating handle 130, so as to rotate the locking element 120 around the first central axis; the elastic portion 122 can be switched between an initial state and a deformed state, when the elastic portion 122 is in the initial state, the locking portion 121 is in a hooking state, and when the elastic portion 122 is in the deformed state, the locking portion 121 is in a disengaging state.
Specifically, the elastic portion 122 has two states, namely an initial state and a deformation state; when the elastic portion 122 is in the initial state, the locking portion 121 is in a hooking state, that is, the hooking end 1211 of the locking portion 121 hooks the bottom of the unmanned aerial vehicle, so that the mounting platform 200 is mounted on the bottom of the unmanned aerial vehicle. When the carrying platform 200 needs to be detached, the worker acts on the handle portion 132 through the handle end 1321, so that the handle portion 132 is rotated away from one side of the carrying platform 200, and the rotating portion 131 rotates around the first central shaft, so as to drive the transmission portion 133 to move towards the carrying platform 200. Since the driving end 1331 of the transmission part 133 is rotatably connected to the transmission end 1221 of the elastic part 122, the driving end 1331 overcomes the elastic force of the elastic part 122 to move close to the first central axis, at this time, the transmission end 1221 of the elastic part 122 moves close to the first central axis, and the elastic part 122 is transformed into a deformed state. The elastic part 122 acts on the locking part 121 in the deformation process, and the locking part 121 moves around the first central axis, so that the hooking end 1211 of the locking part 121 is separated from the unmanned aerial vehicle, and the detachment of the mounting platform 200 is completed.
From top to bottom, through the setting of elastic part 122 and hasp piece 120, hasp piece 120 is through the motion of restriction elastic part 122 to the rotation of restriction hasp portion 121, and then guarantee that colluding of hasp portion 121 holds end 1211 and can stabilize and collude and hold in unmanned aerial vehicle, from this, carry on platform 200 and can carry on the bottom in unmanned aerial vehicle steadily. Through the setting of hasp piece 120, thereby the staff utilizes the elasticity of the rotation of hasp piece 120 overcoming elasticity portion 122 to make hasp portion 121 take place the rotation, and break away from unmanned aerial vehicle, from this, it is more convenient that mounting platform 200 dismantles.
In some embodiments, the first lug 111 is provided with a first rotating shaft 140, and the end of the locking portion 121 is assembled to the first rotating shaft 140, such that the locking portion 121 is rotatably connected to the first lug 111 through the first rotating shaft 140, wherein the central axis of the first rotating shaft 140 is a first central axis; similarly, the second lug 112 is provided with a second rotating shaft 150, and the rotating part 131 is assembled on the second rotating shaft 150, so that the rotating part 131 is rotatably connected with the second lug 112 through the second rotating shaft 150, wherein the central axis of the second rotating shaft 150 is a second central axis; the driving end 1331 and the transmission end 1221 are rotatably provided with a third rotating shaft 160, so that the driving end 1331 and the transmission end 1221 are rotatably connected, wherein the central axis of the third rotating shaft 160 is a third central axis.
In some embodiments, the spacing between the grip end 1321 and the second central axis is X1, i.e., the spacing between the grip end 1321 and the second axis of rotation 150. The distance between the driving end 1331 and the second central axis is X2, i.e., the distance between the driving end 1331 and the second rotating shaft 150. Wherein, X1 is greater than X2, and according to lever principle, the staff only need apply less power to handle end 1321 to make drive end 1331 produce great power and act on elastic component 122, thereby make elastic component 122 convert deformation state into from initial state, and then make hasp portion 121 and unmanned aerial vehicle break away from, from top to bottom, it is more convenient to carry on platform 200 and dismantle.
In some embodiments, the spacing between the drive end 1221 and the first central axis is Y1, i.e., the spacing between the drive end 1221 and the first rotating shaft 140. One end of the locking portion 121 is rotatably connected to the first protrusion 111 through the first rotating shaft 140, and the other end is a hooking end 1211, and a distance between the hooking end 1211 and the first central axis is Y2, i.e. a distance between the hooking end 1211 and the first rotating shaft 140. Wherein, Y1 is less than Y2, so, transmission end 1221 only need move less arc length, collude and hold end 1211 and can move great arc length to can break away from with the unmanned aerial vehicle, from top to bottom visible, elasticity portion 122 takes place less deformation so that hasp portion 121 takes place enough big rotation, thereby makes colluding of hasp portion 121 hold end 1211 and unmanned aerial vehicle phase separation, and it is more convenient that mounting platform 200 dismantles.
Further, X2 is greater than Y1, so that the rotating handle 130 only needs to rotate in a small arc, the locking portion 121 can rotate by a large angle through the elastic portion 122, the hooking end 1211 of the locking portion 121 can be separated from the drone, and the mounting platform 200 is convenient to detach.
Further, X1 is larger than Y2, so that, according to the lever principle, the worker only needs to exert a small force on the grip end 1321 of the rotating grip 130 to be able to disengage the hooking end 1211 from the robot; however, if the worker directly acts on the hooking end 1211, a large force is required to overcome the elastic portion 122, so that the hooking end 1211 is separated from the drone, thereby proving that the hooking end 1211 is stably hooked with the drone. To sum up, hasp structure 100 had both guaranteed that hasp structure 100 can collude firmly and hold in unmanned aerial vehicle to guarantee that mounting platform 200 can carry on unmanned aerial vehicle firmly, guaranteed again that hasp portion 121 breaks away from with unmanned aerial vehicle more conveniently, thereby guarantee that mounting platform 200 dismantles conveniently.
According to a second aspect of the present invention, a carrying platform 200 is disclosed, referring to fig. 1 and fig. 4 to fig. 7, including the locking structure 100, further including a carrying seat 210 and a skeleton component 220, wherein the locking structure 100 is disposed on the carrying seat 210, the skeleton component 220 is assembled with the carrying seat 210 and is used for assembling a firearm 300, and the skeleton component 220 is adjustably disposed on the carrying seat 210 along a predetermined direction, so that the firearm 300 can be adjusted along its length direction.
Specifically, when the unmanned aerial vehicle assembles, gun 300 is carried on skeleton subassembly 220, and skeleton subassembly 220 assembles on mount 210, and mount 210 carries in the bottom of unmanned aerial vehicle, so, carries gun 300 in unmanned aerial vehicle's below. Wherein, skeleton subassembly 220 can be followed and preset the direction and adjusted, consequently, when the staff is at the accurate nature of test gun 300 when using, skeleton subassembly 220 is adjusted on carrying on seat 210 along preset the direction to make gun 300 adjust along self length direction, and then make gun 300 adjusted to suitable position, at this moment, gun 300's equilibrium reaches the best, thereby make gun 300 can aim at the target more stably, and carry out accurate shooting to the target.
In some embodiments, the frame assembly 220 includes two sub-frames 221, the two sub-frames 221 are disposed opposite each other and detachably connected, and the firearm 300 is assembled between the two sub-frames 221. Wherein, a plurality of first connecting portions 2213 are arranged at intervals on the outer wall of each sub-portion framework 221, and the plurality of first connecting portions 2213 are arranged at intervals along a preset direction, that is, along the length direction of the gun body. The mounting seat 210 has two first assembling portions 211, the two first assembling portions 211 are disposed opposite to each other, one first assembling portion 211 is connected to any one first connecting portion 2213 on one sub-portion frame 221, and the other first assembling portion 211 is connected to a corresponding first connecting portion 2213 on the other sub-portion frame 221, that is, the frame assembly 220 is assembled between the two first assembling portions 211. Specifically, when the position of the firearm 300 is adjusted, the first mounting portion 211 is connected to an appropriate one of the first connecting portions 2213, so that the frame assembly 220 is mounted at an appropriate position of the carrier 210, and the firearm 300 is mounted at an appropriate position of the carrier 210.
In some embodiments, the mounting platform 200 further comprises a locking mechanism 230, the locking mechanism 230 comprises a locking member 231, the locking member 231 has a second assembling portion 2312 and a second connecting portion 2311, the first connecting portion 2213 is assembled with the second connecting portion 2311, and the first assembling portion 211 is assembled with the second assembling portion 2312. Specifically, when the position of the firearm 300 needs to be adjusted, the worker separates the locking member 231 from the frame assembly 220, the frame assembly 220 is separated from the limitation of the locking member 231, the frame assembly 220 can be adjusted along the preset direction, so as to adjust the firearm 300 to a proper position, and thereafter, the locking member 231 is connected with the corresponding first connecting portion 2213, so as to fix the firearm 300 to a proper position.
In some embodiments, sub-portion skeleton 221 includes a body 2211, and firearm 300 fits between two bodies 2211. The sub-portion framework 221 further includes a guide rail 2212, the guide rail 2212 is fixedly connected to the exterior of the main body 2211 and is arranged along a predetermined direction, that is, along the length direction of the gun body, and the first connecting portion 2213 is arranged at an interval on one side of the guide rail 2212 away from the main body 2211; meanwhile, the carrying seat 210 has a sliding groove matched with the guide rail 2212, and the guide rail 2212 penetrates through the sliding groove and can slide along the sliding groove, so that the sliding connection between the framework component 220 and the carrying seat 210 is realized. It is from top to bottom seen that skeleton subassembly 220 and carry on seat 210 and adopt above-mentioned connected mode, guaranteed skeleton subassembly 220 and carried on seat 210 assembly together promptly, be convenient for skeleton subassembly 220 again along presetting the direction adjusting position, the length direction adjusting position of the body of a gun promptly.
In addition, since the guide rail 2212 is hidden in the sliding groove of the carrying seat 210, the carrying seat 210 and the framework component 220 can be compactly assembled together, and further, the carrying platform 200 is more balanced when in use.
Further, the first assembling portion 211 is a through groove opened in the mounting seat 210, the through groove is communicated with the sliding groove, the first connecting portion 2213 is located in the sliding groove, and an inner port of the through groove is disposed opposite to one end of the first connecting portion 2213. A part of the locking member 231 is inserted into the through groove, and the other part of the locking member 231 is inserted into the sliding groove, at this time, the second connecting portion 2311 of the locking member 231 is inserted into the first connecting portion 2213 of the guide rail 2212, and the second assembling portion 2312 of the locking member 231 is inserted into the through groove (the through groove is the first assembling portion 211). As can be seen from the above, the locking member 231 is disposed to fix the frame assembly 220 and the carrier 210 relatively, and further fix the firearm 300 on the frame assembly 220 and the carrier 210 relatively. It should be noted that the locking member 231 and the frame component 220 are connected in an embedded manner, and the locking member 231 and the carrying seat 210 are also connected in an embedded manner, so that the locking member 231 can be conveniently assembled and disassembled, thereby facilitating the assembly between the carrying seat 210 and the frame component 220 and the adjustment between the carrying seat 210 and the frame component 220.
It should be noted that the first connecting portion 2213 is a strip-shaped protrusion (refer to fig. 6) vertically disposed on a side portion of the guide rail 2212, the second connecting portion 2311 is a strip-shaped groove vertically disposed on the locking member 231, and the strip-shaped protrusion is embedded and matched with the strip-shaped groove; or, the first connecting portion 2213 is a vertical strip-shaped groove (not shown in the figure) arranged at the side portion of the guide rail 2212, the second connecting portion 2311 is a vertical strip-shaped protrusion arranged on the locking piece 231, and the strip-shaped protrusion and the strip-shaped groove are embedded and matched.
In some embodiments, the locking mechanism 230 further includes a locking assembly 232, the locking assembly 232 is connected with the mount 210 and the locking member 231, so as to fix the locking member 231 on the mount 210, the locking member 231 is maintained in embedded engagement with the mount 210 and the frame assembly 220, and the frame assembly 220 is stably assembled on the mount 210.
Further, the locking assembly 232 includes a guide rod 2321, a limiting member 2322 and a locking handle 2323, the guide rod 2321 sequentially penetrates through the carrying seat 210 and the locking member 231 in a sliding manner, the limiting member 2322 is fixedly connected with the lower end portion of the guide rod 2321, and the lower side of the carrying seat 210 abuts against the lower side, the locking handle 2323 is in threaded connection with the upper end portion of the guide rod 2321 and abuts against the upper top surface of the locking member 231, at this time, the locking assembly 232 fixes the locking member and the carrying seat 210 together, so that the locking member 231 is kept embedded in the through groove. When the frame assembly 220 needs to be adjusted, the worker rotates the locking handle 2323, so that the locking handle 2323 moves upwards, at this time, the locking member 231 can move upwards along the guiding rod 2321, so as to be separated from the first connecting portion 2213, and the frame assembly 220 can slide back and forth relative to the mount 210, so that the gun 300 can be adjusted.
According to the third aspect of the invention, the unmanned aerial vehicle comprises a body and the carrying platform 200, wherein the carrying platform 200 is assembled at the bottom of the unmanned aerial vehicle. Specifically, when the unmanned aerial vehicle assembles, gun 300 is carried on skeleton subassembly 220, and skeleton subassembly 220 assembles on mount 210, and mount 210 carries in the bottom of unmanned aerial vehicle, so, carries gun 300 in unmanned aerial vehicle's below. Wherein, skeleton subassembly 220 can be followed and preset the direction and adjusted, consequently, when the staff is at the accurate nature of test gun 300 when using, skeleton subassembly 220 is adjusted on carrying on seat 210 along preset the direction to make gun 300 adjust along self length direction, and then make gun 300 adjusted to suitable position, at this moment, gun 300's equilibrium reaches the best, thereby make gun 300 can aim at the target more stably, and carry out accurate shooting to the target.
The embodiments of the present invention have been described in detail with reference to the accompanying drawings, but the present invention is not limited to the above embodiments, and various changes can be made within the knowledge of those skilled in the art without departing from the gist of the present invention. Furthermore, the embodiments of the present invention and the features of the embodiments may be combined with each other without conflict.
Claims (10)
1. Hasp structure is applied to unmanned aerial vehicle's platform of carrying on, its characterized in that includes:
the support is used for being assembled on the carrying platform and provided with a first lug and a second lug;
the locking part comprises a locking part and an elastic part, the locking part is rotatably connected with the first lug around a first central shaft and is used for hooking the unmanned aerial vehicle, one end of the elastic part is connected with the locking part, and the other end of the elastic part is a transmission end;
the rotary handle comprises a rotating part, a transmission part and a handle part, the rotating part is rotatably connected with the second lug around a second central shaft, one end of the transmission part is connected with the rotating part, the other end of the transmission part is a driving end, the driving end is rotatably connected with the transmission end around a third central shaft, one end of the handle part is connected with the rotating part, the other end of the handle part is a handle end, and the first central shaft, the second central shaft and the third central shaft are arranged in parallel;
the elastic part can be suitable for the rotation of the rotating handle to generate elastic deformation so as to enable the locking fastener to rotate around the first central shaft; the elastic part can be switched between an initial state and a deformation state, when the elastic part is in the initial state, the lock catch part is in a hooking state, and when the elastic part is in the deformation state, the lock catch part is in a disengaging state.
2. A latch construction according to claim 1, wherein the handle end is spaced further from the second central axis than the drive end.
3. A latch construction according to claim 1, wherein the spacing between the drive end and the second central axis is greater than the spacing between the drive end and the first central axis.
4. The latch structure of claim 1, wherein one end of the latch portion is rotatably connected to the first protrusion, and the other end is a hooking end, and the distance between the hooking end and the first central axis is greater than the distance between the driving end and the first central axis.
5. The latch structure of claim 1 wherein one end of the latch portion is pivotally connected to the first lug and the other end is a hooking end, and the distance between the handle end and the second center axis is greater than the distance between the hooking end and the first center axis.
6. Carry on platform, its characterized in that includes:
the latch structure of any one of claims 1 to 5;
the lock catch structure is arranged on the carrying seat;
the frame subassembly, with carry on seat assembled connection for assemble gun, wherein, the frame subassembly along predetermineeing the adjustable setting in carry on the seat to make gun can follow self length direction and adjust.
7. The carrying platform according to claim 6, wherein the side wall of the framework component is provided with a plurality of first connecting portions at intervals along the preset direction, and the carrying seat is provided with a first assembling portion which can be assembled and connected with any one of the first connecting portions.
8. The carrying platform according to claim 7, wherein the frame assembly comprises a body and a guide rail, the body is used for assembling the gun, the guide rail is fixedly connected with the outside of the body and is arranged along the preset direction, the guide rail is provided with the first connecting part, and the carrying seat is provided with a sliding groove matched with the guide rail;
the carrying platform further comprises a locking mechanism, the locking mechanism comprises a locking piece, the locking piece is provided with a second assembling portion and a second connecting seat, the second assembling portion is in assembly connection with the first assembling portion, and the second connecting portion can be in assembly connection with any one of the first connecting portions.
9. The mounting platform of claim 8, wherein the first mounting portion is a through groove opened in the mounting base, the through groove is communicated with the sliding groove, and an inner port of the through groove is disposed toward the first connecting portion;
the second assembling portion is matched with the first assembling portion in an embedded mode, and the second connecting portion is matched with the first connecting portion in an embedded mode.
10. Unmanned aerial vehicle, its characterized in that includes:
a body;
the mounting platform according to any one of claims 1 to 9, which is mounted on a bottom portion of the machine body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111667479.0A CN114379785B (en) | 2021-12-30 | 2021-12-30 | Lock catch structure, carrying platform and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111667479.0A CN114379785B (en) | 2021-12-30 | 2021-12-30 | Lock catch structure, carrying platform and unmanned aerial vehicle |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN114379785A true CN114379785A (en) | 2022-04-22 |
| CN114379785B CN114379785B (en) | 2024-07-12 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202111667479.0A Active CN114379785B (en) | 2021-12-30 | 2021-12-30 | Lock catch structure, carrying platform and unmanned aerial vehicle |
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| CN (1) | CN114379785B (en) |
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| CN215255424U (en) * | 2021-03-08 | 2021-12-21 | 广东新科艺五金精密制造有限公司 | Lock body and sliding window lock catch |
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2021
- 2021-12-30 CN CN202111667479.0A patent/CN114379785B/en active Active
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| Publication number | Priority date | Publication date | Assignee | Title |
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| RU2086885C1 (en) * | 1993-12-14 | 1997-08-10 | Центральное конструкторское исследовательское бюро спортивно-охотничьего оружия | Pistol |
| TWM392987U (en) * | 2010-07-13 | 2010-11-21 | Inventec Corp | Elastic latch element and an apparatus having a latch and release mechanism using the same |
| CN102765426A (en) * | 2011-05-04 | 2012-11-07 | 现代自动车株式会社 | Hood latch for vehicle |
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| Publication number | Publication date |
|---|---|
| CN114379785B (en) | 2024-07-12 |
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