CN218617229U

CN218617229U - Installation structure of horizontal mounting panoramic camera of small aircraft

Info

Publication number: CN218617229U
Application number: CN202223200149.3U
Authority: CN
Inventors: 刘佳乐; 陈卓仪
Original assignee: Yunchuang Zhanhui Technology Shenzhen Co ltd
Current assignee: Yunchuang Zhanhui Technology Shenzhen Co ltd
Priority date: 2022-11-30
Filing date: 2022-11-30
Publication date: 2023-03-14
Anticipated expiration: 2032-11-30

Abstract

The utility model provides a horizontal carry panoramic camera mounting structure of small-size aircraft, place box, connecting bolt, string support plate and installing support including panoramic camera, the installing support is installed at aircraft lower extreme position, and the rotatable carrier plate of hanging of installing support lower extreme is installed, it places the box with panoramic camera through connecting bolt and links to each other to hang the support plate, panoramic camera places the box and places box inner chamber and panoramic camera size phase-match setting for half open form square box and panoramic camera. The utility model discloses the focus is more steady when the carry panoramic camera flies, and the windage is littleer, rocks also littleer, can the effectual security that promotes the flight to just to the ground direction at flight shooting in-process camera lens, more effectual high-quality imaging area of utilization ratio, the rocking of panoramic camera is littleer, makes the pressure of anti-shake alleviate, has improved the upper limit of the shooting of low shutter speed under the dim light condition, makes data acquisition more effective.

Description

Horizontal mounting panoramic camera mounting structure of small aircraft

Technical Field

The utility model relates to a panoramic camera mounting structure field especially relates to a horizontal carry panoramic camera mounting structure of small aircraft.

Background

At present, all the existing small aircraft loaders adopt 1/4 inch screws for photographic equipment, and the small aircraft loaders are combined with carbon fiber plates to be manufactured, the heads of the existing small aircraft loaders face downwards during loading of panoramic cameras, and the existing small aircraft loaders are inverted and hung to be scraped, so that the defects of the technical scheme are obvious: 1. due to the particularity of the consumer-grade panoramic camera, the camera structure is a fisheye lens with two view angles of more than 180 degrees at two sides, the imaging is circular with distortion, the deformation of an imaging center area is small, more pixels are occupied than the two sides, the imaging quality of the central area of the fisheye lens is far higher than that of the edge, the panoramic camera is hung on an unmanned aerial vehicle to shoot a main collecting area to form a landform below, and the waste of the central high-quality imaging area is caused by a vertical hanging mode. 2. When the aircraft is vertically mounted, the wind resistance is large in the flying process of the aircraft, the gravity center is close to the lower part and can be thrown away, the danger and the uncertainty are increased for the flying safety, the imaging quality is relatively good, the smear is possibly presented at the lower shutter speed, and the data acquisition quality is influenced.

There is a need for a novel panoramic camera mounting structure that is more stable in mounting panoramic cameras in a suspended manner and can be adjusted to obtain better camera shooting imaging effect, and the above problems can be solved.

SUMMERY OF THE UTILITY MODEL

The utility model provides a horizontal carry panoramic camera mounting structure of small aircraft through carrying out the technological transformation to current aircraft carry ware structure, has solved the relatively poor problem of current aircraft carry camera imaging quality.

In order to achieve the purpose, the utility model adopts the technical proposal that:

the utility model provides a horizontal carry panoramic camera mounting structure of small-size aircraft, includes that panoramic camera places box, connecting bolt, string support plate and installing support, the installing support is installed at aircraft lower extreme position, and the rotatable string support plate of installing support lower extreme, it places the box with panoramic camera through connecting bolt and links to each other to hang the support plate, panoramic camera places the box and places box inner chamber and panoramic camera size phase-match setting for half open form square box and panoramic camera.

Preferably, the upper surface of the panoramic camera placing box is provided with three lower side mounting holes, the lower side mounting holes are symmetrically triangular and are respectively arranged, the hanging support plate is provided with three upper side mounting holes corresponding to the lower side mounting holes in position, and the upper side mounting holes and the lower side mounting holes are fixedly connected and provided with connecting bolts.

Preferably, the outside cover of connecting bolt is equipped with the buffering protective sheath, the buffering protective sheath is contradicted and is set up between panorama camera placing box upper surface and carry board lower bottom surface.

Preferably, the bottom surface of the mounting bracket is movably connected with the mounting plate through a rotating part.

Preferably, the portion of rotating is including rotating the mount pad and rotating the bolt, it sets up the bottom surface position at the installing support to rotate the fixed setting of mount pad, the projection of carry board upper surface is provided with the rotation connecting plate, it inserts the setting of rotation mount pad to rotate the connecting plate, the rotation mounting hole has been seted up on the rotation connecting plate, the rotation bolt passes the rotation mounting hole that rotates the mount pad and rotate the connecting plate in proper order and installs the carry board in rotation mount pad department.

Preferably, arc-shaped clamping groove structures are arranged at two ends of the mounting support and are clamped with the horizontal rod parts of the floor support on two sides of the lower end of the aircraft.

Preferably, the outer surface of the panoramic camera placing box is provided with a plurality of ventilation and air hole structures which are arranged at intervals.

The beneficial effects of the utility model reside in that:

the utility model discloses be provided with the installing support at aircraft lower extreme carry, carry board and panoramic camera and place the box, panoramic camera places the box and is used for the fixed panoramic camera of placing, panoramic camera places the box and links to each other with carrying board through three connecting bolt, and carry stability is stronger, and carries board and installing support and can adjust turned angle through rotating the bolt to adjust panoramic camera's shooting angle, it is more convenient to use. The aircraft focus is more steady when the carry panoramic camera flies, and the windage is littleer, rocks also littleer, can the effectual security that promotes the flight to just to the ground direction at the in-process camera lens of shooting of flight, more effective high-quality imaging area of utilization ratio, the rocking of panoramic camera is littleer, makes the pressure of anti-shake alleviate, has improved the upper limit of the shooting of low shutter speed under the dim light condition, makes data acquisition more effective.

Drawings

FIG. 1 is a block diagram of the present invention;

FIG. 2 is a schematic side view of the present invention;

FIG. 3 is a schematic view of the hanging plate and the panoramic camera placing box of the present invention;

FIG. 4 is a schematic view of the installation structure of the rotating part of the present invention;

the reference numbers illustrate: box 1 is placed to panorama camera, downside mounting hole 11, ventilative bleeder vent structure 12, connecting bolt 2, hang support plate 3, upside mounting hole 31, rotate connecting plate 32, rotate mounting hole 321, installing support 4, arc draw-in groove structure 41, panorama camera 5, buffering protective sheath 6, rotation portion 7, rotation mount pad 71, rotate bolt 72, aircraft 8, floor stand horizontal pole 81.

Detailed Description

The following detailed description of the present invention will be made with reference to the accompanying drawings and examples.

Please refer to and show in fig. 1-4, the utility model provides a horizontal carry panoramic camera mounting structure of small aircraft, place box 1, connecting bolt 2, carry board 3 and installing support 4 including panoramic camera, installing support 4 is installed at 8 lower extreme positions of aircraft, and the rotatable carry board 3 of installing support 4 lower extreme, carry board 3 places box 1 through connecting bolt 2 and panoramic camera and links to each other, panoramic camera places box 1 and places box 1 inner chamber and 5 size phase-matches of panoramic camera and set up for half open form square box and panoramic camera.

Further, in order to obtain better connection stability, three lower side mounting holes 11 are formed in the upper surface of the panoramic camera placing box 1, the lower side mounting holes 11 are symmetrically triangular and are respectively arranged, three upper side mounting holes 31 corresponding to the lower side mounting holes 11 in position are formed in the hanging support plate 3, and the upper side mounting holes 31 and the lower side mounting holes 11 are fixedly connected through connecting bolts 2.

The size of the panoramic camera 5 is measured, three-dimensional software is used for modeling along the size outline of the panoramic camera 5, a half-opening square box for modeling is used for loading the panoramic camera 5, three lower side mounting holes 11 with the diameter of 9.8mm are reserved on the upper side of the panoramic camera placing box 1, and the mounting plate 3 is provided with corresponding upper side mounting holes 31 to be connected with the panoramic camera placing box 1.

Further, the upper side mounting hole 31 and the lower side mounting hole 11 are further provided with stepped bolt mounting positions, and the bolt mounting positions can more stably mount and fix the connecting bolt 2.

Further, in order to obtain better shooting stability, the outside cover of connecting bolt 2 is equipped with buffering protective sheath 6, buffering protective sheath 6 conflicts to set up and places between box 1 upper surface and the bottom surface under carry plate 3 in the panorama camera. Buffering protective sheath 6 is the elasticity material, can play the buffering, and absorbing effect reduces 5 trembles of panoramic camera.

Further, the bottom surface of the mounting bracket 4 is movably connected with the hanging and carrying plate 3 through a rotating part 7.

Further, in order to realize that the support plate 3 can rotate relatively to the installing support 4 and adjust, the portion 7 that rotates is including rotating mount pad 71 and rotating bolt 72, rotate the fixed bottom surface position that sets up at the installing support 4 of mount pad 71, the support plate 3 upper surface protrusion is provided with rotates connecting plate 32, it inserts rotation mount pad 71 and sets up to rotate connecting plate 32, rotation mounting hole 321 has been seted up on the connecting plate 32, rotate bolt 72 and pass rotation mount pad 71 and the rotation mounting hole 321 that rotates connecting plate 32 in proper order and will hang the support plate 3 and install in rotation mount pad 71 department. The angle and the position of the panoramic camera placing box 1 can be conveniently fixed by adjusting the tightness degree through rotating the bolt 72.

Further, in order to conveniently and detachably mount the fixed mounting support 4 on the aircraft 8, arc-shaped slot structures 41 are arranged at two ends of the mounting support 4, and the arc-shaped slot structures 41 are partially clamped with the floor stand cross rods 81 on two sides of the lower end of the aircraft 8.

Further, in order to obtain better ventilation and heat dissipation effects, the outer surface of the panoramic camera placing box 1 is provided with a plurality of ventilation and air hole structures 12 which are arranged at intervals.

This embodiment is provided with installing support 4, carry board 3 and panoramic camera at 8 lower extremes of aircraft carry and places box 1, panoramic camera places box 1 and is used for the fixed panoramic camera 5 of placing, panoramic camera places box 1 and links to each other with carry board 3 through three connecting bolt 2, and carry stability is stronger, and carry board 3 and installing support 4 can adjust turned angle through rotating bolt 72 to adjust panoramic camera 5's shooting angle, it is more convenient to use. The focus is more steady when the aircraft 8 carries panoramic camera 5 flight, and the windage is littleer, rocks also littleer, can the effectual security that promotes the flight to just to ground direction at the flight shooting in-process camera lens, more effectual high-quality imaging area of utilization ratio, panoramic camera 5 rocks littleer, makes the pressure of anti-shake alleviate, has improved the upper limit of the shooting of low shutter speed under the dim light condition. Making data acquisition more efficient.

Finally, although the present invention has been described in detail with reference to the preferred embodiments, it should be understood by those skilled in the art that the present invention can be modified or replaced by other means without departing from the spirit and scope of the present invention, which should be construed as limited only by the appended claims.

The utility model discloses the standard part that uses all can purchase from the market, and dysmorphism piece all can be customized according to the description with the record of attached drawing, and the concrete connected mode of each part all adopts conventional means such as ripe bolt, rivet, welding among the prior art, and machinery, part and equipment all adopt conventional model among the prior art, and including the connected mode of circuit connection adoption conventional among the prior art, detailed description is not repeated here.

In the description of the present invention, unless expressly stated or limited otherwise, the terms "mounted," "connected," and "fixed" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral part; can be mechanically or electrically connected; either directly or through an intermediary, either internally or in any other relationship. The specific meaning of the above terms in the present invention can be understood in specific cases for those skilled in the art.

Claims

1. The utility model provides a horizontal carry panoramic camera mounting structure of small-size aircraft, its characterized in that includes that panoramic camera places box, connecting bolt, hangs support plate and installing support, the installing support is installed at aircraft lower extreme position, and the rotatable carrier plate of hanging of installing support lower extreme is installed, it places the box with panoramic camera through connecting bolt and links to each other to hang the support plate, panoramic camera places the box and places box inner chamber and panoramic camera size phase-match setting for half open form square box and panoramic camera.

2. The installation structure of a horizontal mounted panoramic camera of a small aircraft as claimed in claim 1, wherein the panoramic camera storage box has three lower mounting holes on its upper surface, the lower mounting holes are symmetrically triangular and are disposed respectively, the mounting plate has three upper mounting holes corresponding to the lower mounting holes, and the upper mounting holes and the lower mounting holes are fixedly connected by connecting bolts.

3. The installation structure of a horizontal mounting panoramic camera for a small aircraft as claimed in claim 2, wherein a buffer protective sleeve is sleeved outside the connecting bolt, and the buffer protective sleeve is arranged between the upper surface of the panoramic camera placing box and the lower bottom surface of the mounting plate in an abutting mode.

4. The mounting structure of a small aircraft horizontal mounting panoramic camera of claim 1, wherein the bottom surface of the mounting bracket is movably connected with the mounting plate through a rotating part.

5. The installation structure of a horizontal mounting panoramic camera for a small aircraft according to claim 4, wherein the rotating part comprises a rotating mounting seat and a rotating bolt, the rotating mounting seat is fixedly arranged at the bottom of the mounting bracket, a rotating connecting plate is convexly arranged on the upper surface of the mounting plate, the rotating connecting plate is inserted into the rotating mounting seat, a rotating mounting hole is formed in the rotating connecting plate, and the rotating bolt sequentially penetrates through the rotating mounting seat and the rotating mounting hole of the rotating connecting plate to install the mounting plate at the rotating mounting seat.

6. The mounting structure of a horizontal mounting panoramic camera for a small aircraft according to claim 1, wherein arc-shaped clamping groove structures are arranged at two ends of the mounting bracket and are clamped with the cross bar portions of the floor stand at two sides of the lower end of the small aircraft.

7. The mounting structure of the panoramic camera for the horizontal mounting of the small aircraft as claimed in claim 1, wherein the panoramic camera placing box is provided with a plurality of ventilation holes at intervals on the outer surface.