CN211996183U - Unmanned vehicles ventral structure - Google Patents
Unmanned vehicles ventral structure Download PDFInfo
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- CN211996183U CN211996183U CN202020219730.1U CN202020219730U CN211996183U CN 211996183 U CN211996183 U CN 211996183U CN 202020219730 U CN202020219730 U CN 202020219730U CN 211996183 U CN211996183 U CN 211996183U
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Abstract
The utility model discloses an unmanned aerial vehicle belly structure, the surface of the belly of the unmanned aerial vehicle is a mounting area for mounting airborne equipment, and the belly of the unmanned aerial vehicle is a plane; the mounting area comprises a first mounting area and a second mounting area which are arranged at intervals along the length direction of the belly; the first mounting area is arranged on the surface of the belly close to one end of a nose of the unmanned aerial vehicle, and the second mounting area is arranged on the surface of the belly close to one end of a tail of the unmanned aerial vehicle. The flat structural design of unmanned vehicles ventral has increased the effective carry space of unmanned vehicles ventral, can realize the simultaneous carry of two kinds of different airborne equipment to reach in the past only carry an airborne equipment, need fly the effect that just can accomplish a plurality of airborne equipment carries for a plurality of times, effectively improved the operating efficiency, reduced the operation risk.
Description
Technical Field
The utility model belongs to unmanned vehicles art field, concretely relates to unmanned vehicles ventral structure.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", 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 helicopter is a vertical take-off and landing (VTOL) unmanned aerial vehicle flying by radio ground remote control or/and autonomous control, belongs to a rotor unmanned aerial vehicle in structural form, and belongs to a VTOL unmanned aerial vehicle in function.
The unmanned aerial vehicle greatly expands the application range of the unmanned aerial vehicle. The unmanned aerial vehicle is a typical dual-purpose product for military and civilian use, and can be widely applied to a plurality of fields such as transportation, patrol, tourism, rescue and the like.
The belly of the existing unmanned aerial vehicle (including an unmanned helicopter) is mostly a cambered surface, so that the carrying area of the belly of the unmanned aerial vehicle is smaller.
SUMMERY OF THE UTILITY MODEL
Therefore, the utility model provides an unmanned vehicles ventral structure to solve the problem that current unmanned aerial vehicle ventral mounted area is little.
In order to achieve the above object, the present invention provides the following technical solutions:
according to the first aspect of the utility model, the surface of the belly of the unmanned aerial vehicle is a mounting area for mounting airborne equipment, and the belly of the unmanned aerial vehicle is a plane; the mounting area comprises a first mounting area and a second mounting area which are arranged at intervals along the length direction of the belly; the first mounting area is arranged on the surface of the belly close to one end of a nose of the unmanned aerial vehicle, and the second mounting area is arranged on the surface of the belly close to one end of a tail of the unmanned aerial vehicle.
Further, the onboard equipment includes, but is not limited to, cameras, lidar, optoelectronic pods, and jettisonings.
Further, one of the onboard apparatuses is detachably mounted on the ventral surface corresponding to the first mounting area or the second mounting area; or two or more of the airborne equipment are distributed on the ventral surfaces of the first mounting area and the second mounting area.
Further, the laser radar in the airborne equipment is detachably mounted on the surface of the belly corresponding to the first mounting area or the second mounting area; a laser emitting head of the laser radar faces the nose direction of the unmanned aerial vehicle; the camera in the airborne equipment is a wide-range camera, an aerial camera or an inclined camera, and the camera is arranged on the outer wall of the laser radar facing the tail direction of the unmanned aerial vehicle; the lens of the camera faces downward.
Further, the photoelectric pod in the airborne equipment is detachably mounted on the ventral surface corresponding to the first mounting area through a mounting plate.
Further, the thrower in the onboard equipment is detachably mounted on the belly surface corresponding to the second mounting area.
Furthermore, two sliding blocks are convexly arranged on the surface of the belly at intervals in parallel, and sliding grooves are respectively formed in the opposite surfaces of the two sliding blocks along the length direction of the sliding blocks; the top surface of the airborne equipment is convexly provided with a sliding rail matched with the sliding block, the sliding rail is provided with an inserting part matched with the sliding groove, and the inserting part is inserted into the sliding groove to form detachable mounting between the airborne equipment and the belly of the corresponding mounting area.
Furthermore, two the slider bottom surface has seted up the draw-in groove along slider length direction respectively, the slide rail protruding be equipped with draw-in groove matched with joint portion, the draw-in groove is located to joint portion card, forms the machine and carries equipment and correspond the detachable connection between the abdomen in second carry district.
Further, the unmanned aerial vehicle comprises an unmanned helicopter.
The embodiment of the utility model provides a have following advantage:
the flat (namely plane) design of the surface of the aircraft belly can increase the stability of the unmanned aircraft;
due to the flat design of the belly, the effective mounting space of the surface of the belly of the unmanned aerial vehicle is enlarged, and the simultaneous mounting of various different airborne equipment can be realized, for example, the partition design of a first mounting area and a second mounting area in the mounting areas can enable the surface of the belly to simultaneously mount two kinds of airborne equipment (such as an optical pod, a wide camera, an inclined camera, a tossing device, a laser radar and the like);
unmanned vehicles can carry 2 or more than 2 airborne equipment by flying one frame time, thereby achieving the effect that only one airborne equipment is carried by one frame time and a plurality of airborne equipment can be carried by flying a plurality of frame times in the past, effectively improving the operation efficiency and reducing the operation risk.
The damage of the equipment and the machine body caused by repeatedly replacing the mounting equipment is avoided;
the waste of labor cost and time caused by repeatedly replacing the equipment is avoided.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below. It should be apparent that the drawings in the following description are merely exemplary, and that other embodiments can be derived from the drawings provided by those of ordinary skill in the art without inventive effort.
The structure, ratio, size and the like shown in the present specification are only used for matching with the content disclosed in the specification, so as to be known and read by people familiar with the technology, and are not used for limiting the limit conditions which can be implemented by the present invention, so that the present invention has no technical essential significance, and any structure modification, ratio relationship change or size adjustment should still fall within the scope which can be covered by the technical content disclosed by the present invention without affecting the efficacy and the achievable purpose of the present invention.
Fig. 1 is a schematic structural diagram of an unmanned aerial vehicle belly structure provided by an unmanned helicopter as an example in embodiment 1 of the present invention;
fig. 2 is a schematic structural diagram of an unmanned helicopter as an example according to embodiment 1 of the present invention, in which an optoelectronic pod and a camera are mounted on a cabin of an unmanned aircraft belly structure;
fig. 3 is a schematic view of a structure of a slider, an airborne device, and a slide rail in an abdomen structure of an unmanned aerial vehicle according to embodiment 1 of the present invention;
fig. 4 is a schematic view of a structure of a slider, an airborne device, and a slide rail in an abdomen structure of an unmanned aerial vehicle according to embodiment 2 of the present invention;
in the figure:
1. a ventral region 11, a mounting region 111, a first mounting region 112 and a second mounting region; (ii) a
2. A sliding block 21, a sliding groove 22 and a clamping groove;
3. a slide rail 31, an insertion part 32 and a clamping part;
10. a camera;
20. a laser radar, 201, a laser emitting head;
30. a photovoltaic pod;
100. an unmanned aerial vehicle 101, a nose 102 and a tail;
200. an onboard device.
Detailed Description
The present invention is described in terms of specific embodiments, and other advantages and benefits of the present invention will become apparent to those skilled in the art from the following disclosure. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
In the present invention, the terms "upper", "lower", "left", "right", "middle", and the like are used for the sake of clarity only, and are not intended to limit the scope of the present invention, and changes or adjustments of the relative relationship thereof are also considered to be the scope of the present invention without substantial changes in the technical content.
Example 1
Referring to fig. 1 to 3, in the belly structure of the unmanned aerial vehicle provided by the present invention, the surface of the belly 1 of the unmanned aerial vehicle 100 is a mounting area 11 for mounting the airborne equipment 200, and the belly 1 of the unmanned aerial vehicle 100 is a plane; the mounting area 11 comprises a first mounting area 111 and a second mounting area 112 which are arranged at intervals along the length direction of the belly 1; the first mounting region 111 is disposed on the surface of the belly 1 near the nose 101 end of the unmanned aerial vehicle 100, and the second mounting region 112 is disposed on the surface of the belly 1 near the tail 102 end of the unmanned aerial vehicle 100.
Further, the onboard apparatus 200 includes, but is not limited to, a camera 10, a lidar 20, a photovoltaic pod 30, and a jettison device (not shown).
Further, one of the onboard apparatuses 200 is detachably mounted on the surface of the belly 1 corresponding to the first mounting region 111 or the second mounting region 112; alternatively, two or more of the onboard apparatuses 200 are distributed on the ventral surfaces of the first mounting region 111 and the second mounting region 112.
The surface of the belly 1 is used for mounting one type of airborne equipment 200 alone or two or more types of airborne equipment 200 at the same time, and the carrying flexibility is improved according to the needs.
Further, the laser radar 20 in the onboard apparatus 200 is detachably mounted on the surface of the belly 1 corresponding to the first mounting area 111 or the second mounting area 112; the laser emitting head 201 of the laser radar 20 faces the head 101 of the unmanned aerial vehicle 100; the camera 10 in the airborne equipment 200 is a wide-width camera, an aerial camera or a tilt camera, and the camera 10 is installed on the outer wall of the laser radar 20 facing the tail 102 of the unmanned aerial vehicle 100; the lens (not shown) of the camera 10 faces downward.
Camera 10 and laser radar 20 carry simultaneously, and the integral type assembly can effectively save the carry space to can realize the linkage between camera 10 and the laser radar 20, laser radar 20 discovers the target, and camera 10 shoots, effectively improves the operating efficiency.
The linkage control among the camera 10, the laser radar 20 and the unmanned aerial vehicle 100 belongs to the prior art.
Further, the optoelectronic pod 30 in the onboard apparatus 200 is detachably mounted on the surface of the belly 1 corresponding to the first mounting area 111 through a mounting plate 301.
The photoelectric pod 30 can be detachably mounted, and maintenance is convenient.
The control relationship between the optoelectronic pod 30 and the unmanned aerial vehicle 100 belongs to the prior art.
Further, the projectile in the onboard apparatus 200 is detachably mounted on the surface of the belly 1 corresponding to the second mounting area 112.
The mount of the thrower can be independently mounted on the surface of the belly 1, and can also be mounted with other airborne equipment 200 (such as a laser radar) in a matching manner, and the control on the throwing of the thrower belongs to the prior art.
Furthermore, two sliding blocks 2 are convexly arranged on the surface of the belly 1 at intervals in parallel, and sliding grooves 21 are respectively formed in the opposite surfaces of the two sliding blocks 2 along the length direction of the sliding blocks 2;
the top surface of the airborne equipment 200 is convexly provided with a sliding rail 3 matched with the sliding block 2, the sliding rail 3 is provided with an inserting part 31 matched with the sliding groove 21, and the inserting part 31 is inserted in the sliding groove 21 to form detachable mounting between the airborne equipment 200 and the belly 1 corresponding to the mounting area 11.
Further, the unmanned aerial vehicle 100 includes an unmanned helicopter.
It should be noted that, the cooperation design of slide rail 3 and slider 2 is only the utility model discloses in realize the form of dismantling the connection between airborne equipment 200 and the ventral portion 1, all the other feasible ways of dismantling the connection between airborne equipment 200 and the ventral portion 1 surface all fall into the utility model discloses a protection scope.
The utility model provides a use of unmanned vehicles ventral structure as follows:
when the mounting method is used, if the laser radar 20 and the camera 10 need to be mounted, the camera 10 is mounted on the outer wall of the laser radar 20 facing the tail 102 direction of the unmanned aerial vehicle 100, the lens of the camera 10 faces downwards, the top surface of the laser radar 20 is convexly provided with the sliding rail 3, the laser radar 20 is assembled with the sliding block 2 on the surface of the belly 1 through the sliding rail 3, and the laser emitting head 201 of the laser radar 20 faces the head 101 direction of the unmanned aerial vehicle 100, so that the mounting of the laser radar 20 on the surface of the belly 1 is realized;
if the photoelectric pod 30 needs to be mounted, the slide rail 3 can be arranged on the top surface of the photoelectric pod 30 in a protruding mode, and the photoelectric pod 30 can also be detachably connected with the surface of the belly 1 through the mounting plate 301 (for example, through screw assembly);
if the throwing device needs to be carried, a sliding rail 3 can be convexly arranged on the top surface of the throwing device, and the throwing device can also be assembled with the surface of the belly 1 through a screw;
wherein one of the onboard apparatuses 200 is detachably mounted on the surface of the belly 1 corresponding to the first mounting region 111 or the second mounting region 112; alternatively, two or more of the onboard apparatuses 200 are distributed on the ventral surfaces of the first mounting region 111 and the second mounting region 112.
In order to ensure the stable mounting of the airborne equipment 200 on the surface of the belly 1, a lock catch structure or a pin structure can be added at the joint of the sliding block 2 and the sliding rail 3 to ensure the stable connection.
Due to the flat design of the belly, the effective mounting space of the unmanned aerial vehicle is enlarged, and the simultaneous mounting of a plurality of different airborne devices 200 can be realized, for example, the partition design of a first mounting area and a second mounting area in the mounting area can enable the surface of the belly of the unmanned aerial vehicle to simultaneously mount two kinds of airborne devices 200 (such as an optical pod, a wide camera, an inclined camera, a tossing device, a laser radar and the like);
unmanned vehicles can mount 2 or more than 2 airborne equipment 200 for one flight, so that the effect that only one airborne equipment 200 is mounted for one flight in the past and a plurality of devices can be mounted for multiple flights of flight is achieved, the operation efficiency is effectively improved, and the operation risk is reduced.
The damage of the equipment and the machine body caused by repeatedly replacing the mounting equipment is avoided;
the waste of labor cost and time caused by repeatedly replacing the equipment is avoided.
Example 3
Referring to fig. 4, the bottom surfaces of the two sliders 2 are respectively provided with a clamping groove 22 along the length direction of the slider 2, the slide rail 3 is convexly provided with a clamping portion 32 matched with the clamping groove 22, and the clamping portion 32 is clamped in the clamping groove 22 to form detachable connection between the airborne equipment 200 and the surface of the abdomen 1 corresponding to the second mounting region 112.
The stable assembly between the slide block 2 and the slide rail 3 can be ensured by the matching design of the clamping groove 22 and the clamping portion 32, and the stability of the mounting of the airborne equipment 200 is ensured.
The rest is the same as example 1.
Although the invention has been described in detail with respect to the general description and the specific embodiments, it will be apparent to those skilled in the art that modifications and improvements can be made based on the invention. Therefore, such modifications and improvements are intended to be within the scope of the invention as claimed.
Claims (9)
1. An unmanned aerial vehicle belly structure is characterized in that,
the surface of the belly (1) of the unmanned aerial vehicle (100) is a mounting area (11) for mounting airborne equipment (200), and the belly (1) of the unmanned aerial vehicle (100) is a plane;
the mounting area (11) comprises a first mounting area (111) and a second mounting area (112) which are arranged at intervals along the length direction of the belly (1);
the first mounting area (111) is arranged on the surface of the belly (1) close to one end of a nose (101) of the unmanned aerial vehicle (100), and the second mounting area (112) is arranged on the surface of the belly (1) close to one end of a tail (102) of the unmanned aerial vehicle (100).
2. The UAV belly structure according to claim 1, characterized in that the onboard equipment (200) includes, but is not limited to, cameras (10), lidar (20), optoelectronic pods (30), and jettisoninters.
3. The unmanned aerial vehicle belly structure according to claim 2, characterized in that one of said onboard devices (200) is removably mounted to a belly (1) surface corresponding to a first mounting zone (111) or a second mounting zone (112);
or two or more types of the onboard equipment (200) are distributed on the ventral surface of the first mounting area (111) and the second mounting area (112).
4. The UAV ventral structure according to claim 3, characterised in that the lidar (20) in the airborne equipment (200) is detachably mounted to the surface of the ventral (1) corresponding to the first mounting zone (111) or the second mounting zone (112);
a laser emitting head (201) of the laser radar (20) faces the direction of a nose (101) of the unmanned aerial vehicle (100);
the camera (10) in the airborne equipment (200) is a wide-range camera, an aerial camera or an inclined camera, and the camera (10) is arranged on the outer wall of the laser radar (20) facing the tail (102) of the unmanned aerial vehicle (100);
the lens of the camera (10) faces downwards.
5. The UAV ventral structure according to claim 3, characterized in that the optoelectronic pod (30) of the onboard equipment (200) is detachably mounted on the surface of the ventral (1) corresponding to the first mounting area (111) by means of a mounting plate (301).
6. The UAV ventral structure according to claim 3, characterised in that the jettison device of the on-board unit (200) is detachably mounted on the surface of the ventral (1) corresponding to the second mounting area (112).
7. The unmanned aerial vehicle belly structure according to any one of claims 1 and 3-6, wherein two sliding blocks (2) are convexly arranged on the surface of the belly (1) at intervals in parallel, and sliding grooves (21) are respectively formed in opposite surfaces of the two sliding blocks (2) along the length direction of the sliding blocks (2);
the top surface of the airborne equipment (200) is convexly provided with a sliding rail (3) matched with the sliding block (2), the sliding rail (3) is provided with an inserting part (31) matched with the sliding groove (21), and the inserting part (31) is inserted into the sliding groove (21) to form detachable mounting between the airborne equipment (200) and the belly (1) corresponding to the mounting area (11).
8. The unmanned aerial vehicle belly structure of claim 7, characterized in that, the bottom surfaces of the two sliders (2) are respectively provided with a clamping groove (22) along the length direction of the slider (2), the slide rail (3) is convexly provided with a clamping portion (32) matched with the clamping groove (22), and the clamping portion (32) is clamped in the clamping groove (22) to form a detachable connection between the airborne equipment (200) and the corresponding belly (1) of the second mounting region (112).
9. The UAV belly structure according to claim 1 wherein the UAV (100) comprises an unmanned helicopter.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020219730.1U CN211996183U (en) | 2020-02-27 | 2020-02-27 | Unmanned vehicles ventral structure |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020219730.1U CN211996183U (en) | 2020-02-27 | 2020-02-27 | Unmanned vehicles ventral structure |
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| CN211996183U true CN211996183U (en) | 2020-11-24 |
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| CN202020219730.1U Active CN211996183U (en) | 2020-02-27 | 2020-02-27 | Unmanned vehicles ventral structure |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102023115961A1 (en) | 2022-06-30 | 2024-01-04 | Tusas-Turk Havacilik Ve Uzay Sanayii Anonim Sirketi | Carrier system |
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- 2020-02-27 CN CN202020219730.1U patent/CN211996183U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102023115961A1 (en) | 2022-06-30 | 2024-01-04 | Tusas-Turk Havacilik Ve Uzay Sanayii Anonim Sirketi | Carrier system |
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20210713 Address after: 050000 No.303, unit 1, building 2, No.2 Huayao East Street, Chang'an District, Shijiazhuang City, Hebei Province Patentee after: Wang Li Address before: 519000 room 1302, unit 2, building 2, No. 39, Honghui 1st Road, Hongqi Town, Jinwan District, Zhuhai City, Guangdong Province Patentee before: ZHUHAI JIWEI TECHNOLOGY Co.,Ltd. |
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| TR01 | Transfer of patent right |