CN217146393U - Holder mounting device for unmanned aerial vehicle - Google Patents
Holder mounting device for unmanned aerial vehicle Download PDFInfo
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- CN217146393U CN217146393U CN202221249219.1U CN202221249219U CN217146393U CN 217146393 U CN217146393 U CN 217146393U CN 202221249219 U CN202221249219 U CN 202221249219U CN 217146393 U CN217146393 U CN 217146393U
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- unmanned aerial
- mounting
- aerial vehicle
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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Abstract
The utility model discloses a cloud platform carry device for unmanned aerial vehicle, including fixed bolster, central mounting bracket and coupling assembling, the fixed bolster is equipped with supporting part and extension, and the supporting part is connected with unmanned aerial vehicle's installation face, and extension and supporting part parallel arrangement and extension and unmanned aerial vehicle's installation face between have the holding clearance, and the central mounting bracket is equipped with linking arm portion and installation department, and linking arm portion can put into the holding clearance to be connected with the extension through coupling assembling in the accommodation space; the installation part is used for connecting airborne remote sensing equipment. The arm that links of center mounting bracket is connected through the extension that utilizes the fixed bolster, when unmanned aerial vehicle rose, the extension can play the arm that links that the support propped effect, made the effort dispersion to reduce coupling assembling's atress, improve cloud platform carry device's life. The problem of current unmanned aerial vehicle cloud platform carry device reduce life because the fastener atress is big in the flight of unmanned aerial vehicle ascent and descent is solved.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, concretely relates to cloud platform carry device for unmanned aerial vehicle.
Background
An unmanned aircraft, referred to as "drone", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. The unmanned aerial vehicle has the advantages of simple structure and low use cost, not only can complete the task executed by the piloted aircraft, but also is more suitable for the task which is not suitable for being executed by the piloted aircraft.
Currently, image acquisition using drones has been widely used and accepted in various industries, such as aerial photography, mapping, disaster surveying, and the like. The unmanned aerial vehicle aerial photography uses an unmanned aerial vehicle as an aerial platform, uses airborne remote sensing equipment such as a high-resolution CCD digital camera, a light optical camera, an infrared scanner, a laser scanner, a magnetic measuring instrument and the like to acquire information, processes image information by using a computer, and makes the image according to certain precision requirements. In order to facilitate installation of the shooting equipment, a holder device is generally installed on the unmanned aerial vehicle and used for supporting the shooting equipment such as a camera, a camera and a thermal imager. However, the existing mounting device for the holder of the unmanned aerial vehicle is only locked by the fastening piece simply, and in the ascending flight process of the unmanned aerial vehicle, the fastening piece can be pulled by a large force, so that the mounting device for the holder of the unmanned aerial vehicle is easy to damage in repeated ascending and descending.
SUMMERY OF THE UTILITY MODEL
In order to overcome above-mentioned current unmanned aerial vehicle cloud platform carry device and reduce life's technical defect because the fastener atress is big in the flight of unmanned aerial vehicle ascending and descending, the utility model provides a cloud platform carry device for unmanned aerial vehicle.
In order to solve the above problem, the utility model discloses realize according to following technical scheme:
the utility model relates to a cloud platform carry device for unmanned aerial vehicle, including fixed bolster, central mounting bracket and coupling assembling, the fixed bolster is equipped with supporting part and extension, the supporting part is connected with unmanned aerial vehicle's installation face, the extension with the supporting part parallel arrangement just there is the holding clearance between the installation face of extension and unmanned aerial vehicle, the central mounting bracket is equipped with linking arm portion and installation department, the linking arm portion can be put into the holding clearance, and in the accommodation space through coupling assembling with the extension is connected; the installation part is used for connecting airborne remote sensing equipment.
Further, the fixed bolster includes two symmetrical sub-fixed bolsters that set up, sub-fixed bolster includes first horizontal arm, vertical arm and the horizontal arm of second, the supporting part sets up on first horizontal arm, the extension sets up at the horizontal arm of second.
Further, the sub-fixing bracket is an Contraband-shaped bracket.
Furthermore, the central mounting bracket be equipped with a plurality ofly with the linking arm of second transverse arm adaptation, the linking arm constitutes linking arm portion, the linking arm passes through coupling assembling is connected with the second transverse arm.
Further, the center mounting bracket is of a symmetrical structure, the mounting part is a mounting shell seat, and the mounting shell seat is arranged on a symmetrical line of the center mounting bracket.
Furthermore, the connecting assembly comprises eight damping balls and fasteners, and the eight damping balls are respectively arranged at four corners of the fixed support by taking two damping balls as units; the symmetry is equipped with four linking arms around the center mounting bracket, and the end of every linking arm is equipped with first shock attenuation mounting hole, corresponds on the fixed bolster and is equipped with second shock attenuation mounting hole, the fastener passes first shock attenuation mounting hole, shock attenuation ball and second shock attenuation mounting hole in proper order and fixes.
Furthermore, the damping ball is a high-performance damping ball for spaceflight, and the fastener comprises a screw, a stud or a rivet.
Further, cloud platform carry device includes cloud platform interface unit spare, cloud platform interface unit mount the center mounting bracket on the installation shell seat, cloud platform interface unit spare is from last to including inserting wiring board, nuclear core plate and fast-assembling lower cover down in proper order.
Furthermore, a shooting equipment mounting bayonet with a locking piece is arranged at the center of the patch board, and a data interface matched with the output interface of the shooting equipment is arranged at the center of the core board; the quick-mounting lower cover is an aluminum alloy sealing cover body, and a communication port is formed in the side face of the quick-mounting lower cover.
Furthermore, the fixed support and the central mounting frame are made of aluminum alloy materials.
Compared with the prior art, the beneficial effects of the utility model are that:
the arm that links of center mounting bracket is connected through the extension that utilizes the fixed bolster, when unmanned aerial vehicle rose, the extension can play the arm that links that the support propped effect, made the effort dispersion to reduce coupling assembling's atress, improve cloud platform carry device's life.
Drawings
The following detailed description of embodiments of the invention is provided with reference to the accompanying drawings, in which:
fig. 1 is a first schematic structural diagram of an embodiment of a pan-tilt mounting device for an unmanned aerial vehicle according to the present invention;
fig. 2 is a schematic structural diagram of a second embodiment of the pan/tilt/zoom mounting apparatus for an unmanned aerial vehicle according to the present invention;
fig. 3 is a structural exploded view three of an embodiment of the holder mounting device for an unmanned aerial vehicle according to the present invention;
fig. 4 is a fourth enlarged view of a part D in fig. 3 of the holder mounting apparatus for an unmanned aerial vehicle according to the present invention;
fig. 5 is a schematic structural diagram of a fifth embodiment of the central mounting frame of the pan/tilt/zoom mounting apparatus of the present invention;
fig. 6 is an exploded view six of an embodiment of a cradle head interface assembly in the cradle head mounting apparatus of the present invention;
fig. 7 is the structure diagram seven of an embodiment of the cloud platform mount device installed on unmanned aerial vehicle.
In the figure:
10-a fixed support, 20-a central mounting rack, 30-a connecting assembly and 40-a holder interface assembly;
10 a-support, 10 b-extension;
20 a-connecting arm portion, 20 b-mounting portion;
10A-a sub-fixing bracket, 11-a first transverse arm, 12-a vertical arm and 13-a second transverse arm;
21-connecting arm, 22-mounting shell seat;
31-damping balls, 32-fasteners;
41-patch board, 42-core board and 43-quick-assembly lower cover.
Detailed Description
The preferred embodiments of the present invention will be described in conjunction with the accompanying drawings, and it will be understood that they are presented herein only to illustrate and explain the present invention, and not to limit the present invention.
As shown in fig. 1-7, the utility model discloses a preferred structure for cloud platform carry device of unmanned aerial vehicle.
As shown in fig. 1 and 7, the pan/tilt/zoom (pan/tilt/zoom) mounting device for an unmanned aerial vehicle according to the present invention comprises a fixing bracket 10, a central mounting bracket 20 and a connecting assembly 30, wherein the fixing bracket 10 is provided with a supporting portion 10a and an extending portion 10b, the supporting portion 10a is connected with a mounting surface of the unmanned aerial vehicle, the extending portion 10b is arranged in parallel with the supporting portion 10a, an accommodating gap exists between the extending portion 10b and the mounting surface of the unmanned aerial vehicle, the central mounting bracket 20 is provided with a connecting arm portion 20a and a mounting portion 20b, and the connecting arm portion 20a can be placed in the accommodating gap and is connected with the extending portion 10b through the connecting assembly 30 in the accommodating space; the mounting portion 20b is used for connecting an onboard remote sensing device. Through the even arm portion 20a that utilizes extension 10b of fixed bolster 10 to connect central mounting bracket 20, when unmanned aerial vehicle rose, extension 10b can play the even arm portion 20a effect of the support, made the effort dispersion to reduce coupling assembling 30's atress, improve cloud platform carry the life of device.
As shown in fig. 2 to fig. 4, the fixing bracket 10 of the present invention comprises two symmetrically disposed sub-fixing brackets 10A, the sub-fixing bracket 10A comprises a first transverse arm 11, a vertical arm 12 and a second transverse arm 13, the supporting portion 10A is disposed on the first transverse arm 11, and the extending portion 10b is disposed on the second transverse arm 13.
The utility model discloses creatively, sub-fixed bolster 10A is "Contraband" type support.
The utility model discloses creatively, central mounting bracket 20 be equipped with a plurality ofly with the linking arm 21 of the 13 adaptations of second transverse arm, linking arm 21 constitutes even arm 20a, linking arm 21 passes through coupling assembling 30 is connected with the 13 adaptations of second transverse arm.
The utility model discloses creatively, center mounting bracket 20 is symmetrical structure, installation department 20b is installation shell seat 22, installation shell seat 22 sets up on the line of symmetry of center mounting bracket 20. The symmetrical structure can ensure that the central mounting frame 20 is connected to the fixed support 10 to ensure uniform stress, and the whole service life is prolonged.
As shown in fig. 5, the connecting assembly 30 of the present invention includes a damping ball 31 and a fastening member 32, the damping ball 31 has eight through holes, the damping balls 31 are respectively disposed at four corners of the fixing bracket 10 by taking two as units, the corners are rectangular structures and are not specifically referred to as angle components on the shape of the fixing bracket; the symmetry is equipped with four linking arms 21 around central mounting bracket 20, and the end of every linking arm 21 is equipped with first shock attenuation mounting hole, corresponds on fixed bolster 10 and is equipped with second shock attenuation mounting hole, fastener 32 passes first shock attenuation mounting hole, shock attenuation ball 31 and second shock attenuation mounting hole in proper order and fixes. The shock absorption balls 31 are used for connecting the fixed support 10 and the central mounting frame 20, so that the shock caused by the influence of airflow on the airborne remote sensing equipment connected with the central mounting frame 20 can be effectively buffered.
In one embodiment, the damping ball 31 is a hollow damping ball and has two ends provided with retaining rings for being inserted into the first damping mounting hole and the second damping mounting hole for positioning.
The utility model discloses creatively, damping ball 31 adopts space flight to use high performance damping ball, fastener 32 includes screw, double-screw bolt, pin or rivet. Damping shock attenuation ball helps reducing the resonance amplitude of unmanned aerial vehicle structure to avoid the unmanned aerial vehicle structure to cause structural damage because of dynamic stress reaches the limit, damping shock attenuation ball helps cloud platform mounting device to receive the transient impact after, resumes stable state fast, guarantees that machine carries remote sensing equipment operating condition is stable simultaneously.
As shown in fig. 6, the utility model discloses creatively, cloud platform carry device includes cloud platform interface module 40, cloud platform interface module 40 installs center mounting bracket 20 on the installation shell seat 22, cloud platform interface module 40 is from last to including down in proper order plug board 41, nuclear core plate 42 and fast-assembling lower cover 43. Can carry out signal connection, swift convenient to the airborne remote sensing equipment through cloud platform interface module 40.
The utility model discloses creatively, the central part of wiring board 41 is equipped with the shooting equipment installation bayonet socket of taking the locking piece, the center of core plate 42 is equipped with the data interface with shooting equipment output interface assorted; the quick-mounting lower cover 43 is an aluminum alloy sealing cover body, and a communication port is formed in the side face of the quick-mounting lower cover. Through set up shooting equipment fixing bayonet socket and data interface at cloud platform interface module 40, be convenient for change different machine carries remote sensing equipment, the practicality is stronger.
Creatively, the fixed bolster 10 with the center mounting bracket 20 all adopts aluminum alloy material. Specifically, the fixed support 10 is an aluminum alloy support, the central mounting frame 20 is an aluminum alloy mounting frame, and the aluminum alloy has the advantages of being light and hard.
A cloud platform carry device theory of operation for unmanned aerial vehicle be:
through the even arm portion 20a that utilizes extension 10b of fixed bolster 10 to connect central mounting bracket 20, when unmanned aerial vehicle rose, extension 10b can play the even arm portion 20a effect of the support, made the effort dispersion to reduce coupling assembling 30's atress, improve cloud platform carry the life of device.
Other structures of the holder mounting device for the unmanned aerial vehicle in the embodiment are referred to in the prior art.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements.
In the description of the present invention, it is to be understood that the terms "central," "lateral," "upper," "lower," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like are used in the positional or positional relationship indicated in the drawings to facilitate the description of the invention, and are not intended to indicate or imply that the device or element so indicated must have a particular orientation, be constructed and operated in a particular orientation, and are therefore not to be considered limiting of the invention.
The above description is only a preferred embodiment of the present invention, and is not intended to limit the present invention in any way, so that any modification, equivalent change and modification made by the technical spirit of the present invention to the above embodiments do not depart from the technical solution of the present invention, and all fall within the scope of the technical solution of the present invention.
Claims (10)
1. A holder mounting device for an unmanned aerial vehicle is characterized by comprising a fixed support (10), a central mounting rack (20) and a connecting assembly (30),
the fixing support (10) is provided with a supporting part (10a) and an extending part (10b), the supporting part (10a) is connected with the mounting surface of the unmanned aerial vehicle,
the extension part (10b) and the support part (10a) are arranged in parallel, and an accommodating gap exists between the extension part (10b) and the installation surface of the unmanned aerial vehicle,
the central mounting rack (20) is provided with a connecting arm part (20a) and a mounting part (20b),
the connecting arm part (20a) can be placed into the accommodating gap and is connected with the extending part (10b) in the accommodating space through a connecting component (30); the mounting part (20b) is used for connecting an onboard remote sensing device.
2. A cloud deck mounting device for unmanned aerial vehicles according to claim 1,
the fixed support (10) comprises two symmetrically arranged sub-fixed supports (10A),
the sub-fixing bracket (10A) comprises a first transverse arm (11), a vertical arm (12) and a second transverse arm (13),
the support (10a) is arranged on a first transverse arm (11) and the extension (10b) is arranged on a second transverse arm (13).
3. A cloud deck mounting device for unmanned aerial vehicles according to claim 2,
the sub-fixing support (10A) is an Contraband-shaped support.
4. A cloud deck mounting device for unmanned aerial vehicles according to claim 2,
the central mounting frame (20) is provided with a plurality of connecting arms (21) adapted to the second transverse arms (13), the connecting arms (21) constituting the connecting arm portions (20a),
the connecting arm (21) is connected to the second transverse arm (13) via the connecting assembly (30).
5. A cloud deck mounting device for unmanned aerial vehicles according to claim 4,
the central mounting rack (20) is of a symmetrical structure, the mounting part (20b) is a mounting shell seat (22),
the mounting shell seat (22) is arranged on a symmetrical line of the central mounting frame (20).
6. A cloud platform carry device for unmanned aerial vehicle of claim 5, characterized in that:
the connecting assembly (30) comprises a damping ball (31) and a fastener (32),
eight damping balls (31) are arranged and are respectively arranged at four corners of the fixed bracket (10) by taking two damping balls as units; the symmetry is equipped with four linking arms (21) around central mounting bracket (20), and the end of every linking arm (21) is equipped with first shock attenuation mounting hole, corresponds on fixed bolster (10) and is equipped with second shock attenuation mounting hole, fastener (32) are passed first shock attenuation mounting hole, shock attenuation ball (31) and second shock attenuation mounting hole in proper order and are fixed.
7. A cloud platform carry device for unmanned aerial vehicle according to claim 6, characterized in that
The damping ball (31) is a high-performance damping ball for spaceflight, and the fastener (32) comprises a screw, a stud, a pin or a rivet.
8. A cloud deck mounting device for unmanned aerial vehicles according to claim 5,
cloud platform carry device includes cloud platform interface module (40), cloud platform interface module (40) installation center mounting bracket (20) on installation shell seat (22), cloud platform interface module (40) are from last to including down in proper order plug board (41), nuclear core plate (42) and fast-assembling lower cover (43).
9. A cloud deck mounting device for unmanned aerial vehicles according to claim 8,
a shooting equipment mounting bayonet with a locking piece is arranged at the center of the patch board (41), and a data interface matched with an output interface of the shooting equipment is arranged at the center of the core board (42); the quick-mounting lower cover (43) is an aluminum alloy sealing cover body, and a communication port is formed in the side face of the quick-mounting lower cover.
10. A cloud deck mounting device for unmanned aerial vehicles according to claim 1,
the fixed support (10) and the central mounting rack (20) are made of aluminum alloy materials.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221249219.1U CN217146393U (en) | 2022-05-20 | 2022-05-20 | Holder mounting device for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221249219.1U CN217146393U (en) | 2022-05-20 | 2022-05-20 | Holder mounting device for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217146393U true CN217146393U (en) | 2022-08-09 |
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ID=82672023
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221249219.1U Active CN217146393U (en) | 2022-05-20 | 2022-05-20 | Holder mounting device for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217146393U (en) |
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2022
- 2022-05-20 CN CN202221249219.1U patent/CN217146393U/en active Active
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