CN214578589U

CN214578589U - Aircraft camera shooting damping device

Info

Publication number: CN214578589U
Application number: CN202120562722.1U
Authority: CN
Inventors: 康业伟
Original assignee: Zhejiang Xizhoushe Aerospace Technology Group Co ltd
Current assignee: Zhejiang Xizhoushe Aerospace Technology Group Co ltd
Priority date: 2021-03-19
Filing date: 2021-03-19
Publication date: 2021-11-02
Anticipated expiration: 2031-03-19

Abstract

The utility model provides an aircraft damping device that makes a video recording, including establishing the installing support that is used for fixed camera on the aircraft, establishing carry out a plurality of absorbing ball bodies of absorbing to the camera on the installing support, absorbing ball body includes spherical shock absorber, establishes the snap ring at spherical shock absorber both ends, the snap ring with form the draw-in groove between the spherical shock absorber, absorbing ball body passes through the draw-in groove joint is in on the installing support, absorbing ball body is hollow structure, spherical shock absorber comprises three outside bellied arc shock absorption arm. The picture that can make the aircraft transmission is more clear stable, has effectively reduced the shake and the ripple scheduling problem of picture, and camera stability is higher, and the shock attenuation effect is better.

Description

Aircraft camera shooting damping device

Technical Field

The utility model relates to an aircraft damping device technical field, concretely relates to aircraft damping device that makes a video recording.

Background

The aircraft is at the in-process of flight, often can install the camera and take photo by plane, and the camera of usefulness of taking photo by plane can hang on the aircraft through camera stores pylon and shock attenuation ball, the camera is installed and is carried out the shock attenuation through shock attenuation ball on the stores pylon after, and the quality of shock attenuation ball can the clear stability of picture and reduce picture shake/ripple scheduling problem that the aircraft transmitted directly of influence, at present, conventional shock attenuation ball is shown as patent 201420015975.7's shock attenuation ball, owing to adopt 360 degrees structure of covering entirely, and structural deformation does not set up and shakes the position of inhaling, so the shock attenuation effect is not good.

Disclosure of Invention

In order to solve certain or some technical problem that exists among the prior art, the utility model provides an aircraft damping device that makes a video recording can make the picture that the aircraft transmitted more clear stable, has effectively reduced the shake and the ripple scheduling problem of picture, and camera stability is higher, and the shock attenuation effect is better.

For solving the above-mentioned prior art problem, the utility model discloses a following scheme:

the utility model provides an aircraft damping device that makes a video recording, is including establishing the installing support that is used for fixed camera on the aircraft, establishing carry out a plurality of absorbing ball bodies of absorbing to the camera on the installing support, absorbing ball body includes spherical shock attenuation body, establishes the snap ring at spherical shock attenuation body both ends, the snap ring with form the draw-in groove between the spherical shock attenuation body, absorbing ball body passes through the draw-in groove joint is in on the installing support, absorbing ball body is hollow structure, spherical shock attenuation body is inhaled the shake arm by three outside bellied arc and is constituteed.

Furthermore, an arc-shaped convex reinforcing rib is arranged on the outer side of the arc-shaped shock absorption arm.

Further, the thickness of the arc-shaped shock absorption arm is gradually increased from the middle to the two ends.

Furthermore, the damping ball body is made of rubber.

Further, the mounting bracket comprises two first brackets arranged on the aircraft and a second bracket arranged on the first brackets, the second bracket is hung on the first brackets through the damping ball bodies, and the camera is fixed on the second bracket.

Further, first support includes that one end is fixed support arm on the aircraft, establish hang the arm on the support arm, establish hang the first joint hole at arm both ends, the second support is including being used for the installation the mount of camera, establishing four linking arms of mount both sides, establishing second joint hole on the linking arm, the damping ball body both ends the draw-in groove joint respectively is in first joint hole with the second joint is downthehole.

Compared with the prior art, the beneficial effects of the utility model reside in that:

spherical shock attenuation body is inhaled by three outside bellied arc and is inhaled the shake arm and constitute, thereby the triangular shock-absorbing structure of equipartition has been formed, when absorbing shock through the shock attenuation ball body, inhale the shake arm through the arc of three 120 degrees contained angles and inhale and shake, can resist the deformation that all directions atress brought, especially the arc is inhaled the middle department size of inhaling the shake arm and is done for a short time, it is little than other to shake the regional size in the middle of the arm, let it concentrate deformation zone regulation position at this and warp, it is unanimous all from this to warp, can reach the uniformity of deformation, fine filtration vibrations, the picture quality of steady camera, the picture that makes the aircraft transmission is more clear stable, effectively reduced the shake and ripple scheduling problem of picture, camera stability is higher, the shock attenuation effect is better.

Drawings

Fig. 1 is a schematic structural view of the present invention;

FIG. 2 is a schematic structural view of the damping ball body of the present invention;

in the figure: the shock absorption device comprises a camera 1, a mounting bracket 2, a second bracket 3, a fixing frame 4, a connecting arm 5, a first clamping hole 6, a suspension arm 7, a first bracket 8, a shock absorption ball body 9, a second clamping hole 10, a supporting arm 11, an arc shock absorption arm 12, a reinforcing rib 13, a clamping ring 14, a spherical shock absorption body 15 and a clamping groove 16.

Detailed Description

The present invention will be further described with reference to the accompanying drawings and the detailed description, and it should be noted that the embodiments or technical features described below can be arbitrarily combined to form a new embodiment without conflict.

As shown in fig. 1 and 2, an aircraft damping device that makes a video recording, including establishing installing support 2 that is used for fixed camera 1 on the aircraft, establishing carry out a plurality of shock attenuation ball body 9 of absorbing shock to camera 1 on installing support 2, shock attenuation ball body 9 includes spherical shock attenuation body 15, establishes the snap ring 14 at spherical shock attenuation body 15 both ends, snap ring 14 with form draw-in groove 16 between the spherical shock attenuation body 15, shock attenuation ball body 9 passes through draw-in groove 16 joint is in on installing support 2, shock attenuation ball body 9 is hollow structure, spherical shock attenuation body 15 is inhaled shake arm 12 by three outside bellied arc and is constituteed.

In the in-service use process, camera 1 is fixed on the aircraft through installing support 2, inhale shake through shock attenuation ball body 9 at the flight shooting in-process, spherical shock attenuation body 15 is inhaled the arc by three outside bellied and is inhaled the shake arm 12 and constitute, thereby the triangular structure of inhaling of equipartition has been formed, when carrying out the shock attenuation through shock attenuation ball body 9, inhale shake arm 12 through the arc of three 120 degrees contained angles and inhale shake, can resist the deformation that the all direction atress brought, the picture that makes the aircraft transmission is more clear stable, the shake that has effectively reduced the picture and ripple scheduling problem.

In a further improvement, an arc-shaped convex reinforcing rib 13 is arranged on the outer side of the arc-shaped shock absorption arm 12.

Inhale the vertical position in the shock arm 12 outside through the arc and set up strengthening rib 13, can play balanced stabilizing effect, can effectual improvement arc inhale the stress intensity of shock arm 12, improve its stability.

The further improvement is that the thickness of the arc-shaped shock absorption arm 12 is gradually increased from the middle to two ends, the arc-shaped shock absorption arm 12 forms a concentrated deformation area through the middle area, and the shock absorption ball body 9 is made of rubber.

Especially, the size of the middle part of the arc shock absorption arm 12 is made small, the size of the middle area of the shock absorption arm is smaller than that of other shock absorption arms, the shock absorption arm deforms at the specified position of the concentrated deformation area, the deformation consistency starts from this point, the deformation consistency can be achieved, the shock can be filtered well, the image quality of the camera 1 is stabilized, the stability of the camera 1 is higher, and the shock absorption effect is better.

In a further improvement, the mounting bracket 2 comprises two first brackets 8 arranged on the aircraft and a second bracket 3 arranged on the first brackets 8, the second bracket 3 is suspended on the first brackets 8 through the damping ball bodies 9, and the camera 1 is fixed on the second bracket 3.

When installing fixedly through installing support 2 to camera 1, the one end of two first supports 8 is fixed on the aircraft, and second support 3 hangs on first support 8 through a plurality of shock attenuation ball bodies 9, and camera 1 is fixed on second support 3, and the effect is better when the shock attenuation.

The improvement is that, the first support 8 includes that one end is fixed support arm 11 on the aircraft, establish hang arm 7 on the support arm 11, establish hang the first joint hole 6 at arm 7 both ends, the second support 3 is including being used for the installation camera 1's mount 4, establish four linking arms 5 at mount 4 both sides, establish second joint hole 10 on linking arm 5, the draw-in groove 16 at shock attenuation ball body 9 both ends joint respectively in first joint hole 6 with in the second joint hole 10.

Wherein the suspension arm 7 of first support 8 is fixed on the aircraft through support arm 11 suspension formula, snap ring 14 of shock attenuation ball body 9 upper end carries out fixed connection through draw-in groove 16 after inserting first joint hole 6, and snap ring 14 of shock attenuation ball body 9 lower extreme carries out fixed connection through draw-in groove 16 after inserting second joint hole 10 on linking arm 5, thereby make second support 3 fix on first support 8 through shock attenuation ball body 9 suspension type, and camera 1 then installs on mount 4, and adopt four bumper shock absorber bodies to carry out the four corners fixed, when the flight is shot, can make whole aircraft damping device's that makes a video recording shock attenuation effect better, moreover, the steam generator is simple in structure, and convenient for installation, the dismouting is simple and convenient, long service life.

The above embodiments are only preferred embodiments of the present invention, and the protection scope of the present invention cannot be limited thereby, and any insubstantial changes and substitutions made by those skilled in the art based on the present invention are all within the protection scope of the present invention.

Claims

1. The utility model provides an aircraft damping device that makes a video recording, is in including establishing the installing support that is used for fixed camera on the aircraft, establishing carry out a plurality of shock attenuation ball bodies of absorbing shock attenuation to the camera on the installing support, its characterized in that: the damping ball body comprises a spherical damping body and clamping rings arranged at two ends of the spherical damping body, wherein the clamping rings and the spherical damping body form clamping grooves, the damping ball body is connected with the mounting support in a clamping groove manner, the damping ball body is of a hollow structure, and the spherical damping body is composed of three outwards-protruding arc-shaped damping arms.

2. The aircraft camera shock absorbing device of claim 1, wherein: the outside of the arc shock absorption arm is provided with an arc convex reinforcing rib.

3. The aircraft camera shock absorbing device of claim 1, wherein: the thickness of the arc-shaped shock absorption arm is gradually increased from the middle to the two ends.

4. The aircraft camera shock absorbing device of claim 1, wherein: the damping ball body is made of rubber.

5. An aircraft camera shock absorbing device according to any one of claims 1 to 4, wherein: the mounting bracket comprises two first brackets arranged on the aircraft and a second bracket arranged on the first brackets, the second bracket is hung on the first brackets through the damping ball body, and the camera is fixed on the second bracket.

6. An aircraft camera shock absorbing device according to claim 5, wherein: first support includes that one end is fixed support arm on the aircraft, establish hang the arm on the support arm, establish hang the first joint hole at arm both ends, the second support is including being used for the installation the mount of camera, establishing four linking arms of mount both sides, establishing second joint hole on the linking arm, shock attenuation ball body both ends the draw-in groove difference joint is in first joint hole with the second joint is downthehole.