CN110654556A - Unmanned aerial vehicle load dismouting structure - Google Patents
Unmanned aerial vehicle load dismouting structure Download PDFInfo
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- CN110654556A CN110654556A CN201910948285.4A CN201910948285A CN110654556A CN 110654556 A CN110654556 A CN 110654556A CN 201910948285 A CN201910948285 A CN 201910948285A CN 110654556 A CN110654556 A CN 110654556A
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- 238000009434 installation Methods 0.000 claims description 13
- 238000000034 method Methods 0.000 abstract description 8
- 230000005540 biological transmission Effects 0.000 description 5
- 238000007689 inspection Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 208000034699 Vitreous floaters Diseases 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 230000003416 augmentation Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000005265 energy consumption Methods 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
- B64D47/00—Equipment not otherwise provided for
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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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Abstract
The application relates to an unmanned aerial vehicle load dismouting structure, including fixed guide, two sliding rails and load mounting platform. The fixed guide rail comprises a fixed part, a moving part, an adapting part and two guide rails, the adapting part is fixedly connected with the moving part, the adapting part is connected with the fixed part in a sliding mode, the two guide rails are installed on the fixed part and the moving part respectively, and the fixed part is used for being fixedly connected with the unmanned aerial vehicle. The two movable slide rails are respectively connected with the two guide rails in a sliding manner. The load mounting platform is fixedly connected with the two movable sliding rails respectively, is positioned at one end, far away from the two guide rails, of the two movable sliding rails and is used for carrying various loads. Because fixed part and unmanned aerial vehicle fixed connection, the event removes the convenience that unmanned aerial vehicle load dismouting structure dismouting process has been improved in setting up of part and adapting unit, has improved the speed of staff dismouting load promptly. Through setting up load mounting platform, can carry on multiple load simultaneously on unmanned aerial vehicle.
Description
Technical Field
The application relates to the technical field of unmanned aerial vehicle accessories, in particular to an unmanned aerial vehicle load dismounting structure.
Background
With the high-speed construction of the power transmission line and the acceleration of the urbanization process in China, the running state of the overhead power transmission line influences the stability of a power system, and the unmanned aerial vehicle technology is mature day by day and is widely applied to the field of power transmission line inspection. But because the difference of operation demand, need carry on different types of work load equipment on unmanned aerial vehicle. In general, a load such as a camera or a laser may be mounted on the pan head or in the pod, and the pan head or the pod may be connected to the drone through a mechanical structure.
Most of the existing pod or cloud platform equipment is directly and fixedly connected below the body of the unmanned aerial vehicle in a screw connection mode. And the nacelle or the cloud platform is separated from the unmanned aerial vehicle in the transportation process, and after the nacelle or the cloud platform reaches a designated operation area, the nacelle or the cloud platform equipment is assembled on the unmanned aerial vehicle through an installation tool, so that corresponding operation tasks can be executed. The screw mounting means that adopts often at present need consume more time, needs the operation personnel to be equipped with corresponding hand simultaneously and twists the instrument, is unfavorable for the convenient installation and the dismantlement of operation equipment to influence unmanned aerial vehicle executive task's rapidity.
Disclosure of Invention
Based on this, it is necessary to provide an unmanned aerial vehicle load dismouting structure to the complicated problem of unmanned aerial vehicle load dismouting.
The application provides an unmanned aerial vehicle load dismouting structure, include:
the fixed guide rails comprise fixed parts, moving parts, connecting parts and two guide rails, the connecting parts are fixedly connected with the moving parts and are in sliding connection with the fixed parts, the two guide rails are respectively installed on the fixed parts and the moving parts, and the fixed parts are fixedly connected with the unmanned aerial vehicle;
the two movable slide rails are respectively connected with the two guide rails in a sliding manner; and
and the load mounting platform is fixedly connected with the two movable sliding rails respectively, is positioned at one end of the two movable sliding rails far away from the two guide rails, and is used for carrying various loads.
In one embodiment, the moving member defines a first mounting hole, the fixing member defines a sliding channel, the connecting member is disposed through the first mounting hole and extends into the sliding channel, and the connecting member slides in the sliding channel along a direction perpendicular to the sliding direction of the two movable sliding rails.
In one embodiment, the connecting member includes:
the sliding rod penetrates through the first mounting through hole and extends into the sliding channel;
the return spring is sleeved on the sliding rod;
the spring stopper is sleeved on the sliding rod, is fixedly connected with the sliding rod and is used for limiting the position of the end part of the reset spring; and
the abutting piece is sleeved on the sliding rod, penetrates through the first mounting through hole and is fixedly connected with the moving part, one end of the return spring abuts against the spring stopper, the other end of the return spring abuts against the abutting piece, and the abutting piece is used for limiting the position of the return spring, which is far away from the end part of the spring stopper, after the sliding rod, the return spring and the spring stopper are respectively mounted in the first mounting through hole and the sliding channel;
wherein a distance between the spring abutting surface of the spring stopper and the spring abutting surface of the abutting member is smaller than a free length of the return spring.
In one embodiment, the abutting member is provided with a stepped hole, the stepped hole is a through hole, the sliding rod penetrates through the stepped hole and extends into the sliding channel, the stepped hole is formed with an abutting end surface, and one end of the return spring, which is far away from the spring stopper, abuts against the abutting end surface.
In one embodiment, the handle is fixedly connected with the sliding rod and used for driving the sliding rod to slide in the sliding channel.
In one embodiment, the sliding channel includes a first channel, a second channel and a third channel, wherein the first channel is communicated with the first mounting through hole, the first channel and the third channel are communicated through the second channel, wherein the inner diameter of the second channel is smaller than the inner diameter of the first channel and the inner diameter of the third channel, respectively, and the inner diameter of the second channel is larger than the outer diameter of the sliding rod.
In one embodiment, the outer diameter of the spring stop is greater than the outer diameter of the return spring and the inner diameter of the second channel.
In one embodiment, the connecting member further includes a limiting member, the limiting member is fixedly connected to the sliding rod and located in the third channel, and the limiting member is used for limiting a sliding range of the sliding rod.
In one embodiment, the fixing member is provided with a mounting hole, the mounting hole is communicated with the third channel, and the limiting member is mounted on the sliding rod through the mounting hole.
In one embodiment, the fixed part is provided with a guide groove on the surface close to the moving part and far away from the two guide rails, and the moving part is provided with a guide boss which slides in the guide groove along the direction perpendicular to the sliding direction of the two moving slide rails.
In one embodiment, the load mounting platform defines a plurality of second mounting through holes for mounting the plurality of loads.
The application provides an unmanned aerial vehicle load dismouting structure through with adapting unit and moving part fixed connection to with adapting unit and fixed part sliding connection, adapting unit can drive the moving part and remove to the direction of keeping away from the fixed part. After the two movable sliding rails respectively slide into the two guide rails, the movable part and the fixed part can be pressed tightly by controlling the connecting part, so that the two movable sliding rails are fixed. Because fixed part and unmanned aerial vehicle fixed connection, the convenience that unmanned aerial vehicle load dismouting structure carried load has been improved in the setting of event moving part and adapting unit, has improved the speed of staff dismouting load promptly. Through setting up load mounting platform, can carry on multiple load simultaneously on unmanned aerial vehicle.
Drawings
Fig. 1 is a schematic view of a main section structure of an unmanned aerial vehicle load dismounting structure provided in an embodiment of the present application;
fig. 2 is a schematic view of a partial cross-sectional structure of a top view of a load dismounting structure of an unmanned aerial vehicle according to an embodiment of the present application;
fig. 3 is a schematic view of a structure that multiple loads are carried on to unmanned aerial vehicle load dismouting structure that this application embodiment provided.
Description of the reference numerals
100 unmanned aerial vehicle load dismouting structure
10 fixed guide rail
110 fixed part
111 slide channel
112 first channel
113 second channel
114 third channel
115 mounting hole
116 guide groove
120 moving part
121 first mounting through hole
122 guide boss
130 connecting part
131 sliding rod
132 return spring
133 spring stopper
134 abutting piece
135 stepped hole
136 against the end face
137 position limiting element
140 guide rail
20 movable sliding rail
30 load mounting platform
40 handle
50 screw
60 radar
70 vidicon
80 laser
Detailed Description
In order to make the aforementioned objects, features and advantages of the present application more comprehensible, embodiments accompanying the present application are described in detail below with reference to the accompanying drawings. In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present application. This application is capable of embodiments in many different forms than those described herein and those skilled in the art will be able to make similar modifications without departing from the spirit of the application and it is therefore not intended to be limited to the embodiments disclosed below.
It will be understood that when an element is referred to as being "secured to" another element, it can be directly on the other element or intervening elements may also be present. When an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this application belongs. The terminology used herein in the description of the present application is for the purpose of describing particular embodiments only and is not intended to be limiting of the application. As used herein, the term "and/or" includes any and all combinations of one or more of the associated listed items.
Existing unmanned aerial vehicles are classified according to different platform configurations, and mainly comprise a fixed-wing unmanned aerial vehicle, an unmanned helicopter and a multi-rotor unmanned aerial vehicle. Wherein, fixed wing unmanned aerial vehicle is military and most civilian unmanned aerial vehicle's mainstream platform, has the faster advantage of flying speed. The unmanned helicopter has the strongest flexibility and can vertically take off and hover in situ. The multi-rotor unmanned aerial vehicle is a first-choice platform for consumer-grade and partial civil use, has flexibility between a fixed wing and a helicopter, and has the advantages of simplicity in operation, lower cost and the like.
When an existing fixed-wing unmanned aerial vehicle, an existing unmanned helicopter and an existing multi-rotor unmanned aerial vehicle are used for mounting equipment, a cradle head or a pod is directly fixed below an unmanned aerial vehicle body through screws. Therefore, it takes a long time to install the mounting apparatus before the unmanned aerial vehicle performs the task. Meanwhile, a hand screwing tool for installing the screw is required to be equipped on the site. After the unmanned aerial vehicle executes the task, the screw is disassembled by using a corresponding tool. Consequently, current unmanned aerial vehicle mounting equipment dismouting has the complicated and long shortcoming of consuming time of operation. In addition, current unmanned aerial vehicle fuselage below carry on the structure and can only carry on a task load, so its executable task kind is comparatively single, can't satisfy the diversified demand of unmanned aerial vehicle operation task.
Please refer to fig. 1-2, the present application provides an unmanned aerial vehicle load dismounting structure 100. Unmanned aerial vehicle load dismouting structure 100 includes stationary rail 10, two movable slide 20 and load mounting platform 30. The fixed guide rail 10 includes a fixed part 110, a moving part 120, a connecting part 130 and two guide rails 140, the connecting part 130 is fixedly connected with the moving part 120, the connecting part 130 is slidably connected with the fixed part 110, the two guide rails 140 are respectively installed on the fixed part 110 and the moving part 120, and the fixed part 110 is fixedly connected with the unmanned aerial vehicle. The two movable rails 20 are slidably connected to the two guide rails 140. The load mounting platform 30 is fixedly connected to the two movable rails 20, and is located at one end of the two movable rails 20 away from the two guide rails 140, and is used for carrying a plurality of loads.
It is understood that the fixed rail 10 includes a fixed part 110, a moving part 120, a connecting part 130, and two rails 140. The fixed member 110 and the moving member 120 are disposed opposite to each other, and one end of the connecting member 130 may be fixedly connected to the moving member 120 and the other end may be slidably connected to the fixed member 110. The connecting component 130 can realize the clamping and the limiting between the fixed component 110 and the moving component 120, and the connecting component 130 can drive the moving component 120 to be far away from, close to or press the fixed component 110 in the process of relative sliding with the fixed component 110, so that the installation and the fixation of the two movable sliding rails 20 are realized. Connecting part 130's setting can prevent that it is not hard up to appear after fixed guide rail 10 and two movable slide rails 20 dock, has improved unmanned aerial vehicle load dismouting structure 100's reliability. In addition, two guide rails 140 of the fixed rail 10 have a guiding function.
In the use of unmanned aerial vehicle load dismouting structure 100, stationary rail 10 can pass through screw 50 and unmanned aerial vehicle fuselage fixed connection, and movable slide 20 passes through load mounting platform 30 fixed connection with unmanned aerial vehicle load. When the unmanned aerial vehicle performs the inspection task, the distance between the two guide rails 140 of the fixed guide rail 10, that is, the distance between the fixed member 110 and the moving member 120, is first widened by the connecting member 130, and then the moving rail 20 together with the load mounting platform 30, and the load of the unmanned aerial vehicle mounted on the load mounting platform 30 are moved relative to the fixed guide rail 10 along the preset mounting direction. When the movable slide rail 20 slides to reach the position right below the body of the unmanned aerial vehicle, the fixed guide rail 10 and the movable slide rail 20 can be further clamped by the connecting component 130, that is, the relative position between the fixed guide rail 10 and the movable slide rail 20 is locked. Above-mentioned dismouting process of unmanned aerial vehicle load need not any appurtenance, only needs the process of carrying on that the unmanned aerial vehicle load can be accomplished to the short time, has improved staff's operating efficiency.
It can be understood that this application does not do the restriction to fixed guide rail 10, two movable slide rail 20 and load mounting platform 30's material, as long as the material intensity that it adopted can satisfy unmanned aerial vehicle load and carry on can. In one of them embodiment, can adopt the material that the quality is lighter as far as possible, can realize the lightweight of unmanned aerial vehicle load dismouting structure 100 when guaranteeing unmanned aerial vehicle load quick assembly disassembly, be favorable to reducing unmanned aerial vehicle's energy consumption to improve unmanned aerial vehicle's operating efficiency.
The application provides an unmanned aerial vehicle load dismouting structure 100 through with adapting unit 130 and moving part 120 fixed connection to with adapting unit 130 and fixed part 110 sliding connection, adapting unit 130 can drive moving part 120 and remove to the direction of keeping away from fixed part 110. After the two movable sliding rails 20 respectively slide into the two guide rails 140, the movable member 120 and the fixed member 110 can be pressed by controlling the connecting member 130, so that the two movable sliding rails 20 are fixed. Because fixed part 110 and unmanned aerial vehicle fixed connection, the setting of removal part 120 and adapting unit 130 has improved the convenience of unmanned aerial vehicle load dismouting structure 100 in the dismouting process, has improved the speed of staff dismouting load promptly. Through setting up load mounting platform 30, can carry on multiple load simultaneously on unmanned aerial vehicle. Consequently, unmanned aerial vehicle load dismouting structure 100 that this application provided has simple structure's advantage, simple operation's advantage, can be used for polymorphic type or polytypic such as fixed wing unmanned aerial vehicle, unmanned helicopter and many rotor unmanned aerial vehicle to patrol and examine unmanned aerial vehicle carry, and can be applicable to transmission line's detection and safety maintenance.
In one embodiment, the moving member 120 is provided with a first mounting through hole 121, the fixing member 110 is provided with a sliding channel 111, the connecting member 130 is disposed through the first mounting through hole 121 and extends into the sliding channel 111, and the connecting member 130 slides in the sliding channel 111 along a direction perpendicular to the sliding direction of the two movable sliding rails 20. It is understood that one end of the connection member 130 extends into the sliding channel 111, and one end of the connection member 130 away from the sliding channel 111 is disposed in the first mounting through hole 121 and is fixedly connected with the moving member 120. Therefore, connecting part 130 can drive movable part 120 through self-movement and keep away from, be close to or the pressure fastening fixed part 110, so only can realize the dismouting of two movable slide rails 20 through control connecting part 130, make unmanned aerial vehicle load dismouting structure 100 have simple structure, the advantage of simple operation.
In one embodiment, the connecting member 130 includes a sliding rod 131, a return spring 132, a spring stopper 133, and an abutment 134. The sliding rod 131 penetrates through the first mounting through hole 121 and extends into the sliding channel 111. The return spring 132 is sleeved on the sliding rod 131. The spring stopper 133 is sleeved on the sliding rod 131, and is fixedly connected to the sliding rod 131 for limiting the position of the end of the return spring 132. The abutting member 134 is sleeved on the sliding rod 131, passes through the first installation through hole 121, and is fixedly connected to the moving member 120, one end of the return spring 132 abuts against the spring stopper 133, and the other end abuts against the abutting member 134, the abutting member 134 is used for limiting the position of the return spring 132 away from the end of the spring stopper 133 after the sliding rod 131, the return spring 132 and the spring stopper 133 are respectively installed in the first installation through hole 121 and the sliding channel 111. Wherein, the distance between the spring abutment surface of the spring stopper 133 and the spring abutment surface of the abutment member 134 is smaller than the free length of the return spring 132.
It is understood that the sliding rod 131 can be used as a guide post for the return spring 132, ensuring that the extension and contraction direction of the return spring 132 is unchanged. One end of the return spring 132 may be restrained by the abutment 134, and the other end of the return spring 132 may be restrained by the spring stopper 133. It should be noted that the initial state of the return spring 132 may be a compressed state, that is, the return spring 132 is in the compressed state before the two movable rails 20 are slid into the two guide rails 140 respectively. Wherein the spring stopper 133 may be directly coupled to the sliding rod 131 by a screw. Therefore, when the sliding rod 131 moves laterally, the spring stopper 133 can be driven to further compress the return spring 132. When the two movable sliding rails 20 slide on the two guide rails 140 in parallel to a predetermined position along a predetermined installation direction, the sliding rod 131 can be controlled to move towards the fixed component 110, and the left movable component 120 and the right fixed component 110 can be clamped by the elastic force of the return spring 132, so that the clamping and locking between the translatable fixed guide rail 10 and the movable sliding rail 20 can be realized. Therefore, the return spring 132 can provide a lateral fastening force for fixing the movable rail 20, and can simplify the installation manner of the movable rail 20.
In one embodiment, the abutting member 134 is provided with a stepped hole 135, the stepped hole 135 is a through hole, the sliding rod 131 is disposed through the stepped hole 135 and extends into the sliding channel 111, the stepped hole 135 is formed with an abutting end surface 136, and an end of the return spring 132 away from the spring stopper 133 abuts against the abutting end surface 136. It is understood that the abutment 134 may limit an end of the return spring 132 away from the spring stop 133. The stepped hole 135 formed in the abutting member 134 may form an abutting end surface 136, and the abutting end surface 136 contacts with the return spring 132, so that when the sliding rod 131 moves in a direction away from the fixed member 110, the abutting end surface 136 may limit the return spring 132, so that the lateral elastic force of the return spring 132 is enhanced, and a lateral fastening force is provided for the fixed member 110 and the moving member 120. The abutment 134 may be fixedly connected to the sliding rod 131 by the screw 50, and may be fixedly connected to the moving member 120 by the screw 50.
In one embodiment, the handle 40 is further included, and the handle 40 is fixedly connected to the sliding rod 131 for driving the sliding rod 131 to slide in the sliding channel 111. It is understood that the handle 40 may be directly fixed to the sliding rod 131 by a screw. In one embodiment, the handle 40 may be provided with a catch, i.e., the handle 40 may be temporarily restricted to the current position by the catch when the handle 40 moves the slide bar 131 laterally. After the installation of the movable sliding rail 20 is completed, the handle 40 is pulled out from the buckle, so that the return spring 132 is reset, that is, the movable component 120 is driven to press the fixing component 110, thereby clamping and locking the movable sliding rail 20.
In one embodiment, the sliding channel 111 includes a first channel 112, a second channel 113, and a third channel 114, wherein the first channel 112 communicates with the first mounting through hole 121, the first channel 112 and the third channel 114 communicate through the second channel 113, wherein an inner diameter of the second channel 113 is smaller than an inner diameter of the first channel 112 and an inner diameter of the third channel 114, respectively, and an inner diameter of the second channel 113 is larger than an outer diameter of the sliding rod 131. In one embodiment, the outer diameter of the spring stop 133 is greater than the outer diameter of the return spring 132 and the inner diameter of the second channel 113. It is understood that the sliding rod 131 may be inserted through the first installation through hole 121 and extend to the first, second and third passages 112, 113 and 114, respectively. The first channel 112 is configured to facilitate the sliding rod 131 to connect the moving member 120 and the fixing member 110, the second channel 113 is configured to limit the position of the sliding rod 131 that can be reached when the sliding rod 131 moves rightwards, and the third channel 114 is configured to limit the position of the sliding rod 131 that can be reached when the sliding rod 131 moves leftwards by providing the limiting member 137.
In one embodiment, the connecting component 130 further includes a limiting member 137, and the limiting member 137 is fixedly connected to the sliding rod 131 and located in the third channel 114 for limiting a sliding range of the sliding rod 131. In one embodiment, the fixing member 110 is provided with a mounting hole 115, the mounting hole 115 is communicated with the third channel 114, and the limiting member 137 is mounted on the sliding rod 131 through the mounting hole 115. It is understood that the end of the sliding rod 131 adjacent to the spring stop 133 can be directly screwed to the stop 137. The limiting member 137 is disposed to ensure that the translation amount of the return spring 132 when translating to the left side is not too large, and to prevent the connecting member 130 from falling off from the fixing member 110, thereby ensuring the stability of the relative position between the connecting member 130 and the fixing member 110.
In one embodiment, the fixed part 110 has a guide groove 116 formed on a surface thereof close to the moving part 120 and away from the two guide rails 140, and the moving part 120 has a guide boss 122, and the guide boss 122 slides in the guide groove 116 along a direction perpendicular to the sliding direction of the two movable slide rails 20. It can be understood that the guide slot 116 and the guide boss 122 are configured to enable the moving member 120 and the fixed member 110 to move in a fixed direction, so that the moving member 120 and the fixed member 110 are not misaligned when the return spring 132 is reset, and stability of relative positions of the moving slide 20 during the dismounting process is ensured. In one embodiment, the guide grooves 116 and the guide bosses 122 correspond to each other one by one.
In one embodiment, the load mounting platform 30 defines a plurality of second mounting through holes for mounting a plurality of loads. Referring to fig. 3, in one embodiment, the unmanned aerial vehicle load dismounting structure 100 may be equipped with a laser pan-tilt apparatus for removing floating objects on the power transmission line. The laser holder device has the functions of stability augmentation, automatic tracking, target distance measurement, high-energy laser emission and the like, and can effectively remove line floaters. In this embodiment, the stability-enhancing cradle head may adopt an azimuth-elevation two-axis frame structure, and is provided with a radar 60, a camera 70 and a laser 80. Wherein, load mounting platform 30 can adopt shock attenuation platform, and load mounting platform 30 can regard as cloud platform position base, can realize and increase the high frequency vibration isolation between steady cloud platform and the sliding rail 20. When the movable slide rail 20 moves to a specific position along a preset installation direction on the fixed guide rail 10, the unmanned aerial vehicle load dismounting structure 100 can realize clamping and locking between the two.
The technical features of the embodiments described above may be arbitrarily combined, and for the sake of brevity, all possible combinations of the technical features in the embodiments described above are not described, but should be considered as being within the scope of the present specification as long as there is no contradiction between the combinations of the technical features.
The above-mentioned embodiments only express several embodiments of the present application, and the description thereof is more specific and detailed, but not construed as limiting the claims. It should be noted that, for a person skilled in the art, several variations and modifications can be made without departing from the concept of the present application, which falls within the scope of protection of the present application. Therefore, the protection scope of the present patent shall be subject to the appended claims.
Claims (11)
1. The utility model provides an unmanned aerial vehicle load dismouting structure which characterized in that includes:
the fixed guide rail (10) comprises a fixed part (110), a moving part (120), a connecting part (130) and two guide rails (140), the connecting part (130) is fixedly connected with the moving part (120), the connecting part (130) is in sliding connection with the fixed part (110), the two guide rails (140) are respectively installed on the fixed part (110) and the moving part (120), and the fixed part (110) is used for being fixedly connected with the unmanned aerial vehicle;
two movable slide rails (20) which are respectively connected with the two guide rails (140) in a sliding manner; and
and the load mounting platform (30) is fixedly connected with the two movable sliding rails (20) respectively, is positioned at one end, far away from the two guide rails (140), of the two movable sliding rails (20), and is used for carrying various loads.
2. The unmanned aerial vehicle load dismounting structure according to claim 1, wherein the moving member (120) is provided with a first mounting through hole (121), the fixing member (110) is provided with a sliding channel (111), the connecting member (130) is inserted into the first mounting through hole (121) and extends into the sliding channel (111), and the connecting member (130) slides in the sliding channel (111) along a direction perpendicular to the sliding direction of the two moving slide rails (20).
3. The unmanned aerial vehicle load disassembly and assembly structure of claim 2, wherein the connecting member (130) comprises:
the sliding rod (131) penetrates through the first installation through hole (121) and extends into the sliding channel (111);
a return spring (132) sleeved on the sliding rod (131);
the spring stopper (133) is sleeved on the sliding rod (131), is fixedly connected with the sliding rod (131), and is used for limiting the position of the end part of the return spring (132); and
the abutting piece (134) is sleeved on the sliding rod (131), penetrates through the first installation through hole (121), and is fixedly connected with the moving part (120), one end of the return spring (132) abuts against the spring stopper (133), the other end of the return spring (132) abuts against the abutting piece (134), and the abutting piece (134) is used for limiting the position of the return spring (132) far away from the end part of the spring stopper (133) after the sliding rod (131), the return spring (132) and the spring stopper (133) are respectively installed in the first installation through hole (121) and the sliding channel (111);
wherein a distance between a spring abutment surface of the spring stopper (133) and a spring abutment surface of the abutment member (134) is smaller than a free length of the return spring (132).
4. The unmanned aerial vehicle load dismounting structure of claim 3, wherein the abutting member (134) is provided with a stepped hole (135), the stepped hole (135) is a through hole, the sliding rod (131) penetrates through the stepped hole (135) and extends into the sliding channel (111), the stepped hole (135) is formed with an abutting end surface (136), and one end of the return spring (132) far away from the spring stopper (133) abuts against the abutting end surface (136).
5. An unmanned aerial vehicle load dismounting structure according to claim 3, further comprising a handle (40), wherein the handle (40) is fixedly connected with the sliding rod (131) and is used for driving the sliding rod (131) to slide in the sliding channel (111).
6. The unmanned aerial vehicle load disassembly and assembly structure of claim 3, wherein the sliding channel (111) comprises a first channel (112), a second channel (113), and a third channel (114), wherein the first channel (112) communicates with the first mounting through hole (121), the first channel (112) and the third channel (114) communicate through the second channel (113), wherein an inner diameter of the second channel (113) is smaller than an inner diameter of the first channel (112) and an inner diameter of the third channel (114), respectively, and an inner diameter of the second channel (113) is larger than an outer diameter of the sliding rod (131).
7. The unmanned aerial vehicle load disassembly and assembly structure of claim 6, wherein an outer diameter of the spring stop (133) is larger than an outer diameter of the return spring (132) and an inner diameter of the second channel (113).
8. The unmanned aerial vehicle load disassembly and assembly structure of claim 6, wherein the connecting member (130) further comprises a stopper (137), and the stopper (137) is fixedly connected with the sliding rod (131) and located in the third channel (114) for limiting a sliding range of the sliding rod (131).
9. The unmanned aerial vehicle load dismounting structure according to claim 8, wherein the fixing member (110) is provided with a mounting hole (115), the mounting hole (115) is communicated with the third channel (114), and the limiting member (137) is mounted on the sliding rod (131) through the mounting hole (115).
10. The unmanned aerial vehicle load dismounting structure according to claim 1, wherein a surface of the fixed member (110) close to the moving member (120) and far from the two guide rails (140) is provided with a guide groove (116), the moving member (120) is provided with a guide boss (122), and the guide boss (122) slides in the guide groove (116) along a direction perpendicular to a sliding direction of the two moving slide rails (20).
11. The unmanned aerial vehicle load disassembly and assembly structure of claim 1, wherein the load mounting platform (30) is opened with a plurality of second mounting through holes for mounting the plurality of loads.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910948285.4A CN110654556A (en) | 2019-10-08 | 2019-10-08 | Unmanned aerial vehicle load dismouting structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910948285.4A CN110654556A (en) | 2019-10-08 | 2019-10-08 | Unmanned aerial vehicle load dismouting structure |
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| Publication Number | Publication Date |
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| CN110654556A true CN110654556A (en) | 2020-01-07 |
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| CN201910948285.4A Pending CN110654556A (en) | 2019-10-08 | 2019-10-08 | Unmanned aerial vehicle load dismouting structure |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114572409A (en) * | 2022-05-07 | 2022-06-03 | 北京卓翼智能科技有限公司 | A installation device and unmanned aerial vehicle for unmanned aerial vehicle load |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7647676B2 (en) * | 2005-07-28 | 2010-01-19 | Carnevali Jeffrey D | Thumb release mounting apparatus |
| CN105818994A (en) * | 2016-04-29 | 2016-08-03 | 湖北易瓦特科技股份有限公司 | Cloud terrace quick-detachable unmanned aerial vehicle |
| CN108443658A (en) * | 2018-03-29 | 2018-08-24 | 西南大学 | Vehicles display adaptive stabilizing mounting device |
| CN207876015U (en) * | 2018-02-06 | 2018-09-18 | 贵州电网有限责任公司 | A kind of multi-rotor unmanned aerial vehicle cruising inspection system Quick universal locking pin |
| CN208102361U (en) * | 2017-12-28 | 2018-11-16 | 深圳城际快机科技有限公司 | A kind of fast assembling disassembling structure based on unmanned aerial vehicle platform |
-
2019
- 2019-10-08 CN CN201910948285.4A patent/CN110654556A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7647676B2 (en) * | 2005-07-28 | 2010-01-19 | Carnevali Jeffrey D | Thumb release mounting apparatus |
| CN105818994A (en) * | 2016-04-29 | 2016-08-03 | 湖北易瓦特科技股份有限公司 | Cloud terrace quick-detachable unmanned aerial vehicle |
| CN208102361U (en) * | 2017-12-28 | 2018-11-16 | 深圳城际快机科技有限公司 | A kind of fast assembling disassembling structure based on unmanned aerial vehicle platform |
| CN207876015U (en) * | 2018-02-06 | 2018-09-18 | 贵州电网有限责任公司 | A kind of multi-rotor unmanned aerial vehicle cruising inspection system Quick universal locking pin |
| CN108443658A (en) * | 2018-03-29 | 2018-08-24 | 西南大学 | Vehicles display adaptive stabilizing mounting device |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114572409A (en) * | 2022-05-07 | 2022-06-03 | 北京卓翼智能科技有限公司 | A installation device and unmanned aerial vehicle for unmanned aerial vehicle load |
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Application publication date: 20200107 |