CN217535177U

CN217535177U - Hoisting device of actuating cylinder of motion system of full-motion flight simulator

Info

Publication number: CN217535177U
Application number: CN202221664675.2U
Authority: CN
Inventors: 王樑
Original assignee: Accel Tianjin Flight Simulation Co Ltd
Current assignee: Accel Tianjin Flight Simulation Co Ltd
Priority date: 2022-06-29
Filing date: 2022-06-29
Publication date: 2022-10-04
Anticipated expiration: 2032-06-29

Abstract

The utility model relates to a hoist and mount technical field especially relates to a hoist device of full-motion flight simulator motion system pressurized strut, including the outer loop and the centre gripping inner ring that open and shut that set up with one heart, fixed mounting has a plurality of track bearings on the outer loop inner wall that opens and shuts, and fixed mounting has the hoisting ring on the outer loop outer wall that opens and shuts, and the centre gripping inner ring is equipped with the sliding ring, every with the fixed sliding ring that is equipped with of the corresponding position of track bearing blocks respectively and establishes on the sliding ring. The device provided by the utility model simple structure, hoist and mount are efficient, and conveniently control rotation angle.

Description

Hoisting device of actuating cylinder of motion system of full-motion flight simulator

Technical Field

The utility model relates to a hoist and mount technical field especially relates to a hoist device of full-motion flight simulator motion system pressurized strut.

Background

In the process of installing the actuating cylinder of the six-degree-of-freedom motion system on the full-motion flight simulator, the actuating cylinder of the motion system needs to be lifted and then moved to a specified hinge for installation, and the angle of the actuating cylinder needs to be adjusted by rotating the actuating cylinder during installation. However, the rotation angle after hoisting is very difficult due to the heavy weight of the actuator cylinder, and the rotation angle needs to be adjusted repeatedly to the correct position when the rotation angle is improper. The existing actuator cylinder hoisting mode is that a hoisting belt is tied to the middle of an actuator cylinder for hoisting, a special hoisting device is not arranged, the angle adjustment difficulty in the hoisting process is high, the accuracy is poor, the control is not easy, the time consumption is long, and the hoisting gravity center is easy to shift.

SUMMERY OF THE UTILITY MODEL

The utility model aims to solve the technical problem that a simple structure is provided, hoist and mount efficiency is high, and the hoist device of the all-movable flight simulator motion system pressurized strut of convenient control rotation angle.

The utility model discloses a realize through following technical scheme:

a hoisting device of a full-motion flight simulator motion system actuator cylinder comprises an opening and closing outer ring and a clamping inner ring which are concentrically arranged, wherein a plurality of track bearings are fixedly mounted on the inner wall of the opening and closing outer ring, a hoisting ring is fixedly mounted on the outer wall of the opening and closing outer ring, a sliding ring is fixedly arranged at the position, corresponding to the track bearings, of the clamping inner ring, and each track bearing is clamped on the sliding ring.

Furthermore, the outer loop that opens and shuts includes outer loop main part, hinge and the face that opens and shuts, the outer loop main part includes first outer loop main part and second outer loop main part, the hinge is installed between first outer loop main part and second outer loop main part, the fixed tip of locating first outer loop main part and second outer loop main part of face that opens and shuts, and through first bolted connection between the face that opens and shuts of first outer loop main part and second outer loop main part. Further, the first outer ring main body and the second outer ring main body respectively comprise an upper ring body, a lower ring body and a supporting column fixedly connected between the upper ring body and the lower ring body.

Preferably, the track bearings are fixedly mounted on the inner walls of the upper ring body and the lower ring body respectively.

Furthermore, the hoisting ring is fixedly arranged in the middle of the opening and closing surface of the first outer ring main body or the second outer ring main body and is fixedly locked with the opening and closing surface of the second outer ring main body or the first outer ring main body through a second bolt.

Furthermore, the clamping inner ring is composed of a plurality of inner ring main bodies, gaps are reserved between adjacent inner ring main bodies, bolt inclined holes corresponding to each other are formed between the adjacent inner ring main bodies, and the adjacent inner ring main bodies are fixed at the bolt inclined holes through third bolts.

Preferably, the top and the bottom of the inner ring main body are respectively and fixedly provided with a sliding ring protruding out of the inner ring main body. Furthermore, an anti-slip pad is fixedly arranged on the inner wall of the clamping inner ring.

Beneficial effects of the utility model

The application provides a hoist device of full-dynamic flight simulator motion system pressurized cylinder has following advantage: the device has the advantages of simple structure, convenient, fast and efficient hoisting, and can accurately control the rotation angle of the actuating cylinder in the hoisting process, and the gravity center deviation can not occur, and the safety is higher in the hoisting process.

Drawings

FIG. 1 is a schematic structural view of a hoisting device;

figure 2 is a schematic illustration of ram lifting.

In the figure, 1, an opening and closing outer ring, 2, a track bearing, 3, a non-slip mat, 4, a hinge, 5, an outer ring main body, 6, a support column, 7, a lower ring body, 8, a bolt inclined hole, 9, a clamping inner ring, 10, an opening and closing surface, 11, a hoisting ring, 12, a second bolt, 13, a first bolt, 14, a sliding ring, 15, an upper ring body and 16, actuating cylinders are arranged.

Detailed Description

The utility model provides a hoist device of full-automatic flight simulator motion system pressurized strut, its includes the outer loop 1 and the centre gripping inner ring 9 that open and shut that set up with one heart, fixed mounting has a plurality of track bearing 2 on the outer loop inner wall that opens and shuts, track bearing can adopt the welded mode with open and shut outer loop inner wall fixed connection, convenient operation is swift, and firm reliable.

The outer wall of the opening and closing outer ring is fixedly provided with a hoisting ring 11, the clamping inner ring is fixedly provided with a sliding ring 14 at a position corresponding to the track bearings, and each track bearing is clamped on the sliding ring. The track bearing is arranged to enable the opening and closing outer ring and the clamping inner ring to rotate relatively under the condition of keeping concentricity. When in hoisting, the clamping inner ring clamps the actuating cylinder 16, and the opening and closing outer ring and the clamping inner ring can rotate relatively through the track bearing. When the actuating cylinder needs to rotate by a certain angle, the actuating cylinder only needs to be manually rotated to drive the clamping inner ring to rotate on the track bearing.

Further, the outer loop that opens and shuts includes outer loop main part 5, hinge 4 and face 10 that opens and shuts, the outer loop main part includes first outer loop main part and second outer loop main part, the hinge is installed between first outer loop main part and second outer loop main part, and the setting of hinge can make and can realize opening and shutting between first outer loop main part and the second outer loop main part. The opening and closing surface is fixedly arranged at the end parts of the first outer ring main body and the second outer ring main body, the opening and closing surfaces of the first outer ring main body and the second outer ring main body are connected through a first bolt 13, the opening and closing surfaces of the first outer ring main body and the second outer ring main body can be fastened together through the first bolt, and the first outer ring main body and the second outer ring main body are closed. Further, the first outer ring main body and the second outer ring main body respectively comprise an upper ring body 15, a lower ring body 7 and a support column 6 fixedly connected between the upper ring body and the lower ring body, and the track bearings are respectively and fixedly installed on the inner walls of the upper ring body and the lower ring body. Go up the setting of ring body, lower ring body and support column for the outer loop that opens and shuts forms open structure, both made things convenient for the locking and the opening of centre gripping inner ring, can make again that the ring body, lower ring body all pass through track bearing with the centre gripping inner ring and be connected, overall structure is more firm, moves more reliably.

Further, the hoisting ring is fixedly installed in the middle of the opening and closing surface of the first outer ring main body or the second outer ring main body and is fixed with the opening and closing surface of the second outer ring main body or the first outer ring main body through a second bolt 12. When the lifting ring is fixedly installed on the opening and closing surface of the first outer ring main body, the opening and closing surfaces of the lifting ring and the second outer ring main body are fixed through bolts after the opening and closing outer ring is closed, and when the lifting ring is fixedly installed on the opening and closing surface of the second outer ring main body, the opening and closing surfaces of the lifting ring and the first outer ring main body are fixed through bolts after the opening and closing outer ring is closed, so that the lifting ring is more stably and reliably installed, and the lifting ring is prevented from falling off or rotating between the opening and closing outer ring and the lifting ring in the lifting process.

Further, the clamping inner ring is composed of a plurality of inner ring main bodies, a gap is reserved between every two adjacent inner ring main bodies, bolt inclined holes 8 corresponding to each other are formed between every two adjacent inner ring main bodies, and the adjacent inner ring main bodies are fixed at the bolt inclined holes through third bolts (not shown). When the actuating cylinder is hoisted, the actuating cylinder penetrates through the clamping inner ring and the clamping inner ring is positioned at the gravity center position of the actuating cylinder, and then the third bolt is screwed down, so that the actuating cylinder is clamped by the clamping inner ring and is prevented from rotating or sliding relatively.

Optimized, the top and the bottom of the inner ring main body are respectively and fixedly provided with a sliding ring protruding out of the inner ring main body, so that the track bearing is convenient to install, the overall structure is more stable, and the running is more stable.

Furthermore, the inner wall of the clamping inner ring is fixedly provided with a non-slip mat 3, the non-slip mat can be a wear-resistant rubber mat or made of other elastic wear-resistant materials, the friction force between the clamping inner ring and the actuating cylinder can be increased, and the gravity center of the actuating cylinder is prevented from shifting.

When the hoisting device is hoisted, the opening and closing outer ring and the clamping inner ring are both in an opening state, the actuating cylinder penetrates through the clamping inner ring of the hoisting device and enables the clamping inner ring to be located at the gravity center position of the actuating cylinder, the clamping inner ring is locked to form a closed circular ring, then the opening and closing surface of the opening and closing outer ring is locked by a bolt, and then the hoisting ring is further fixed with the opening and closing surface and then begins to be hoisted.

In the hoisting process, when the actuating cylinder needs to rotate for a certain angle, the actuating cylinder can drive the clamping inner ring to freely rotate on the track bearing only by manually rotating the actuating cylinder, so that the rotation angle of the actuating cylinder can be freely adjusted.

The device can keep the outer ring that opens and shuts, centre gripping inner ring and pressurized cylinder three between concentric, under the prerequisite that the outer ring that opens and shuts keeps static, centre gripping inner ring can rotate along track bearing with the pressurized cylinder together to realize the accurate control of pressurized cylinder rotation angle. The device has the advantages of simple structure, convenient, quick and efficient hoisting, no relative sliding and rolling between the clamping inner ring and the actuating cylinder in the hoisting process, and stable and reliable operation.

To sum up, the utility model provides a pair of hoist device of full-motion flight simulator motion system pressurized cylinder, simple structure, hoist and mount are efficient, and convenient control rotation angle.

The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention, and various modifications and changes may be made by those skilled in the art. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. The utility model provides a hoist device of full-dynamic flight simulator motion system pressurized strut which characterized in that: the clamping device comprises an opening and closing outer ring and a clamping inner ring which are concentrically arranged, wherein a plurality of track bearings are fixedly mounted on the inner wall of the opening and closing outer ring, a hoisting ring is fixedly mounted on the outer wall of the opening and closing outer ring, a sliding ring is fixedly arranged at the position of the clamping inner ring corresponding to the track bearings, and each track bearing is clamped on the sliding ring.

2. The lifting device of the actuating cylinder of the motion system of the full-motion flight simulator according to claim 1, wherein the opening and closing outer ring comprises an outer ring main body, a hinge and an opening and closing surface, the outer ring main body comprises a first outer ring main body and a second outer ring main body, the hinge is installed between the first outer ring main body and the second outer ring main body, the opening and closing surface is fixedly arranged at the end parts of the first outer ring main body and the second outer ring main body, and the opening and closing surface of the first outer ring main body and the opening and closing surface of the second outer ring main body are connected through a first bolt.

3. The hoisting device of the actuating cylinder of the motion system of the full-motion flight simulator as defined in claim 2, wherein the first outer ring body and the second outer ring body each comprise an upper ring body, a lower ring body and a support pillar fixedly connected between the upper ring body and the lower ring body.

4. The lifting device for the actuator cylinder of the motion system of the full-motion flight simulator as claimed in claim 3, wherein the track bearings are fixedly mounted on the inner walls of the upper ring body and the lower ring body, respectively.

5. The hoisting device of the actuating cylinder of the motion system of the full-motion flight simulator according to claim 2, wherein the hoisting ring is fixedly installed in the middle of the opening and closing surface of the first outer ring body or the second outer ring body and is fixedly locked with the opening and closing surface of the second outer ring body or the first outer ring body through a second bolt.

6. The lifting device for the actuating cylinder of the motion system of the full-motion flight simulator as claimed in claim 1, wherein the clamping inner ring is composed of a plurality of inner ring bodies, a gap is reserved between adjacent inner ring bodies, bolt inclined holes corresponding to each other are arranged between adjacent inner ring bodies, and the adjacent inner ring bodies are fixed at the bolt inclined holes by a third bolt.

7. The lifting device for the actuating cylinder of the motion system of the full-motion flight simulator as claimed in claim 6, wherein the top and the bottom of the inner ring body are respectively and fixedly provided with a sliding ring protruding out of the inner ring body.

8. The lifting device for the actuating cylinder of the motion system of the full-motion flight simulator as claimed in claim 1, wherein the inner wall of the clamping inner ring is fixedly provided with a non-slip mat.