CN215922574U

CN215922574U - Film-grade camera mounting equipment with vibration filtering function for multi-axis aircraft

Info

Publication number: CN215922574U
Application number: CN202122110683.4U
Authority: CN
Inventors: 刘依纯
Original assignee: Lingkong Culture Technology Shanghai Co ltd
Current assignee: Lingkong Culture Technology Shanghai Co ltd
Priority date: 2021-09-02
Filing date: 2021-09-02
Publication date: 2022-03-01
Anticipated expiration: 2031-09-02

Abstract

The utility model discloses film-grade camera mounting equipment with a vibration filtering function for a multi-axis aircraft, which comprises a fixed plate, wherein a connecting plate is movably mounted above the fixed plate, a fixed support is fixedly mounted above the connecting plate, a damping ring is movably mounted above the fixed plate, a fixed rod is fixedly mounted on the surface of the outer side of the damping ring, a fixed support rod is movably embedded into the surface of one end of the fixed rod, a first snap ring is fixedly mounted at one end of the fixed support rod, a second snap ring is movably mounted at one side of the first snap ring, and rubber pads are movably mounted in the inner rings of the first snap ring and the second snap ring. The film-grade camera mounting equipment with the vibration filtering function for the multi-axis aircraft can prevent the vibration generated by the flight of the aircraft from being transmitted to the camera through the fixed support, improve the stability of the shot picture of the camera and enable the mounting equipment to be suitable for various types of aircraft.

Description

Film-grade camera mounting equipment with vibration filtering function for multi-axis aircraft

Technical Field

The utility model relates to the field of mounting equipment, in particular to film-grade camera mounting equipment which is used for a multi-axis aircraft and has a vibration filtering function.

Background

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 obtain information, processes image information by a computer, and manufactures the image according to certain precision requirements, and the whole system has outstanding characteristics in the aspects of design and optimized combination and is a novel application technology integrating high-altitude shooting, remote control, remote measuring technology, video image microwave transmission and computer image information processing; the film-grade camera mounting equipment that is used for multiaxis aircraft and possesses and strain and shake the function has certain drawback when using, and the vibrations that the aircraft flight produced can transmit the camera through the fixed bolster, and the shooting picture of camera is unstable, and mounting equipment adopts the bolt-up in the aircraft below, can not make mounting equipment be applicable to the aircraft of multiple model.

SUMMERY OF THE UTILITY MODEL

The utility model mainly aims to provide movie-grade camera mounting equipment which is used for a multi-axis aircraft and has a vibration filtering function, and the movie-grade camera mounting equipment can effectively solve the problems in the background technology.

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

a film level camera carry equipment that is used for multiaxis aircraft and possesses and strain shake function, which comprises a fixing plate and i comprises a fixing plate, fixed plate top movable mounting has the connecting plate, connecting plate top fixed mounting has the fixed bolster, fixed plate top movable mounting has the damping ring, damping ring outside fixed surface installs the dead lever, dead lever one end surface activity embedding installs fixed branch, fixed branch one end fixed mounting has the snap ring No. one, snap ring one side movable mounting has No. two snap rings, No. one the snap ring with No. two equal movable mounting of snap ring inner circle has the rubber pad.

Preferably, fixed surface installs the stopper on the fixed plate, fixed surface installs the screw rod on the fixed plate, the screw rod runs through the connecting plate, and with connecting plate swing joint, the screw rod outside is close upper end department movable mounting and has the nut.

Preferably, the inside movable mounting of shock attenuation ring has hollow block, the shock attenuation ring pass through hollow block with screw rod swing joint, the fixed embedding in hollow block side surface installs the spiral rubber tube, the inside fixed mounting of spiral rubber tube has powerful spring.

Preferably, the other end of the spiral rubber tube is fixedly connected with the inner surface of the damping ring, the outer side surface of the hollow block is fixedly provided with a buffer block at four corners, the other side surface of the buffer block is fixedly connected with the inner surface of the damping ring, and the upper surface and the lower surface of the damping ring are fixedly provided with rubber rings.

Preferably, the lower surface of the fixing rod is movably embedded with a threaded knob at one end close to the lower surface of the fixing rod, the upper surface of the fixing support rod is provided with a threaded hole, and the threaded knob penetrates through the lower surface of the fixing rod and is movably connected with the threaded hole.

Preferably, the through-hole has been seted up to fixed stay upper surface near one end department, No. two snap ring upper surface and lower surface are close a department fixed mounting of department have the lantern ring, No. two snap rings pass through the lantern ring with fixed stay swing joint, the inside movable mounting of lantern ring has the bull stick, the bull stick runs through the through-hole, No. one the snap ring with No. two the snap ring other end passes through bolt swing joint.

Compared with the prior art, the utility model has the following beneficial effects:

in the utility model, a camera is fixed between fixed supports, when in use, a first snap ring is clamped on the surface of a support leg of an aircraft, a second snap ring is closed, the first snap ring and the second snap ring are fixed by bolts, then a screw knob is rotated to separate the screw knob from a screw hole, the extension length of a fixed support rod is adjusted, the screw knob is screwed into the screw hole, a hanging device can be connected and fixed with aircrafts of different models by adjusting the length of the fixed support rod and replacing rubber pads with different thicknesses, so that the hanging device is suitable for various aircrafts, when the aircrafts fly, the vibration generated by the aircrafts is transmitted to the fixed support rod and transmitted to a damping ring through a fixed rod, a hollow block can slightly move by a spiral rubber tube and a strong spring, the contact between the hollow block and the damping ring is reduced, and the vibration of the hollow block is further absorbed by the damping block and the rubber ring, the vibration generated by the aircraft is eliminated inside the damping ring, so that the camera is prevented from being driven to vibrate together by the vibration generated when the aircraft flies, the influence of the aircraft on the camera is reduced, and the shot picture is stable.

Drawings

FIG. 1 is a schematic view of the overall structure of a film-grade camera mounting device with a shock filtering function for a multi-axis aircraft according to the present invention;

FIG. 2 is a disassembled view of the overall structure of the film-grade camera mounting device with the vibration filtering function for the multi-axis aircraft according to the present invention;

FIG. 3 is a split view of a fixing rod II and a clamp ring structure of the film-grade camera mounting equipment with the vibration filtering function for a multi-axis aircraft according to the present invention;

FIG. 4 is a sectional view of a shock absorbing ring of the film-grade camera mounting device with shock absorbing function for a multi-axis aircraft according to the present invention.

In the figure: 1. a fixing plate; 101. a limiting block; 102. a screw; 103. a nut; 2. a connecting plate; 201. fixing a bracket; 3. a shock-absorbing ring; 301. a hollow block; 302. a spiral rubber tube; 303. a strong spring; 304. a buffer block; 305. a rubber ring; 4. fixing the rod; 401. fixing the supporting rod; 402. a threaded hole; 403. a threaded knob; 404. a through hole; 5. a first snap ring; 501. a second snap ring; 502. a collar; 503. a rotating rod; 504. a bolt; 6. and (7) a rubber pad.

Detailed Description

In order to make the technical means, the creation characteristics, the achievement purposes and the effects of the utility model easy to understand, the utility model is further described with the specific embodiments.

As shown in fig. 1-4, the film-grade camera mounting device for a multi-axis aircraft and having a vibration filtering function comprises a fixing plate 1, wherein a connecting plate 2 is movably mounted above the fixing plate 1, a fixing support 201 is fixedly mounted above the connecting plate 2, a damping ring 3 is movably mounted above the fixing plate 1, a fixing rod 4 is fixedly mounted on the surface of the outer side of the damping ring 3, a fixing support rod 401 is movably embedded into the surface of one end of the fixing rod 4, a first snap ring 5 is fixedly mounted at one end of the fixing support rod 401, a second snap ring 501 is movably mounted on one side of the first snap ring 5, and rubber pads 6 are movably mounted on inner rings of the first snap ring 5 and the second snap ring 501;

a limiting block 101 is fixedly arranged on the upper surface of the fixing plate 1, a screw 102 is fixedly arranged on the upper surface of the fixing plate 1, the screw 102 penetrates through the connecting plate 2 and is movably connected with the connecting plate 2, and a nut 103 is movably arranged on the outer side of the screw 102 close to the upper end; a hollow block 301 is movably mounted in the damping ring 3, the damping ring 3 is movably connected with the screw 102 through the hollow block 301, a spiral rubber pipe 302 is fixedly embedded in the surface of one side of the hollow block 301, and a strong spring 303 is fixedly mounted in the spiral rubber pipe 302; the other end of the spiral rubber tube 302 is fixedly connected with the inner surface of the damping ring 3, the buffer blocks 304 are fixedly mounted on the outer side surface of the hollow block 301 at four corners, the other side surface of the buffer block 304 is fixedly connected with the inner surface of the damping ring 3, the rubber rings 305 are fixedly mounted on the upper surface and the lower surface of the damping ring 3, the hollow block 301 can slightly move by the spiral rubber tube 302 and the strong spring 303, the contact between the hollow block 301 and the damping ring 3 is reduced, meanwhile, the vibration of the hollow block 301 is reduced, and the vibration generated by an aircraft is eliminated inside the damping ring 3 through further absorption of the buffer blocks 304 and the rubber rings 305, so that the phenomenon that the camera is driven by the vibration generated during the flight of the aircraft to vibrate together can be avoided, the influence of the aircraft on the camera is reduced, and the shot picture is stable; a threaded knob 403 is movably embedded and mounted at one end of the lower surface of the fixing rod 4 close to the lower surface, a threaded hole 402 is formed in the upper surface of the fixing support rod 401, and the threaded knob 403 penetrates through the lower surface of the fixing rod 4 and is movably connected with the threaded hole 402; through-hole 404 has been seted up to fixed support rod 401 upper surface near one end department, No. two snap rings 501 upper surface and lower surface are close one end department fixed mounting and have lantern ring 502, No. two snap rings 501 pass through lantern ring 502 and fixed support rod 401 swing joint, the inside movable mounting of lantern ring 502 has bull stick 503, bull stick 503 runs through-hole 404, No. 5 snap rings and No. two snap ring 501 other ends pass through bolt 504 swing joint, length and the rubber pad 6 of changing different thickness through adjusting fixed support rod 401, it is fixed to make the carry equipment can be connected with the aircraft of different models, it is applicable to multiple aircraft to make it.

It should be noted that, the film-grade camera mounting equipment with the function of vibration filtering for the multi-axis aircraft is characterized in that when the film-grade camera mounting equipment is mounted, a camera is fixed between the fixed supports 201, when the film-grade camera mounting equipment is used, the first snap ring 5 is clamped on the surface of a support leg of the aircraft, the second snap ring 501 is closed, the first snap ring 5 and the second snap ring 501 are fixed through the bolt 504, the threaded knob 403 is rotated to separate the threaded knob 403 from the threaded hole 402, the extending length of the fixed support rod 401 is adjusted, the threaded knob 403 is screwed into the threaded hole 402, the mounting equipment can be connected and fixed with aircrafts of different models by adjusting the length of the fixed support rod 401 and replacing rubber pads 6 with different thicknesses, the film-grade camera mounting equipment is suitable for various aircrafts, when the aircrafts fly, the vibration generated by the aircrafts is transmitted to the fixed support rod 401 and is transmitted to the damping ring 3 through the fixed rod 4, spiral rubber tube 302 and powerful spring 303 make hollow block 301 slightly remove, reduce the contact between hollow block 301 and the damping ring 3, simultaneously reduce hollow block 301's vibrations, the further absorption of rethread buffer block 304 and rubber ring 305, the vibrations that make the aircraft produce are at the inside elimination of damping ring 3, thereby the vibrations that produce when can avoiding the aircraft flight drive the camera and shake together, reduce the influence of aircraft to the camera, make the picture of shooing stable.

The foregoing shows and describes the general principles and broad features of the present invention and advantages thereof. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are described in the specification and illustrated only to illustrate the principle of the present invention, but that various changes and modifications may be made therein without departing from the spirit and scope of the present invention, which fall within the scope of the utility model as claimed. The scope of the utility model is defined by the appended claims and equivalents thereof.

Claims

1. A film level camera carry equipment that is used for multiaxis aircraft and possesses and strain and shake function, its characterized in that: including fixed plate (1), fixed plate (1) top movable mounting has connecting plate (2), connecting plate (2) top fixed mounting has fixed bolster (201), fixed plate (1) top movable mounting has damping ring (3), damping ring (3) outside fixed surface installs dead lever (4), dead lever (4) one end movable embedding of surface installs fixed branch (401), fixed branch (401) one end fixed mounting has snap ring (5) No. one, snap ring (5) one side movable mounting has snap ring (501) No. two, snap ring (5) with No. two equal movable mounting of snap ring (501) inner circle has rubber pad (6).

2. The cinematographic camera mounting device for multi-axis aerial vehicles with shock filtering capability of claim 1, wherein: fixed surface installs stopper (101) on fixed plate (1), fixed surface installs screw rod (102) on fixed plate (1), screw rod (102) run through connecting plate (2), and with connecting plate (2) swing joint, screw rod (102) outside is close upper end department movable mounting and has nut (103).

3. The film-grade camera mounting apparatus for multi-axis aircraft with shock filtering function according to claim 2, wherein: damping ring (3) inside movable mounting has hollow block (301), damping ring (3) pass through hollow block (301) with screw rod (102) swing joint, hollow block (301) one side fixed surface embedding installs spiral rubber tube (302), spiral rubber tube (302) inside fixed mounting has powerful spring (303).

4. The cinematographic camera mounting device for multi-axis aerial vehicles with shock filtering capability of claim 3, wherein: spiral rubber tube (302) other end with damping ring (3) inside fixed surface connects, the equal fixed mounting in four corners department that hollow block (301) outside surface is located has buffer block (304), buffer block (304) opposite side surface with damping ring (3) inside fixed surface connects, damping ring (3) upper surface and the equal fixed mounting of lower surface have rubber ring (305).

5. The cinematographic camera mounting device for multi-axis aerial vehicles with shock filtering capability of claim 4, wherein: the lower surface of the fixing rod (4) is movably embedded with a threaded knob (403) at one end close to the upper surface of the fixing support rod (401), a threaded hole (402) is formed in the upper surface of the fixing support rod (401), and the threaded knob (403) penetrates through the lower surface of the fixing rod (4) and is movably connected with the threaded hole (402).

6. The cinematographic camera mounting device for multi-axis aerial vehicles with shock filtering capability of claim 5, wherein: through-hole (404) have been seted up to fixing support rod (401) upper surface near one end department, No. two snap ring (501) upper surface and lower surface are close one end department fixed mounting and have a lantern ring (502), No. two snap ring (501) pass through lantern ring (502) with fixing support rod (401) swing joint, lantern ring (502) inside movable mounting has bull stick (503), bull stick (503) run through-hole (404), snap ring (5) with No. two snap ring (501) other ends pass through bolt (504) swing joint.