A lifting device capable of lifting and turning a load vertically

By designing the lifting device and load-bearing frame of the lifting equipment, the problems of low efficiency and interference in the flipping and lifting of rocket sections were solved, and efficient and safe section flipping and assembly were achieved.

CN115893177BActive Publication Date: 2025-12-12BEIJING LINGKONG TIANXING TECH CO LTD
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Patent Information

Application Number
CN202211568134.4
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2022-12-08
Publication Date
2025-12-12
Estimated Expiration
2042-12-08

AI Technical Summary

Technical Problem

The existing rocket segment flipping and hoisting process is inefficient, labor-intensive, and prone to interference between steel cables and control surfaces, making assembly difficult.

Method used

Design a lifting device that includes a hoisting device and a load-bearing frame device. Avoid interference with steel cables by using a cable support assembly. Achieve stable tilting of the compartment by using an adjustable connection hole and an adapter seat. Reduce tilting torque and improve ease of operation.

Benefits of technology

It improved the efficiency of rocket segment assembly, reduced the intensity of manual labor, avoided interference between steel cables and control surfaces, and ensured the stability and safety of the assembly process.

✦ Generated by Eureka AI based on patent content.

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Abstract

The present application relates to a kind of lifting device that can be vertically lifted and overturn the object being lifted.The lifting device includes a hanging device and a load-bearing frame device installed at the bottom of the hanging device.The hanging device includes two opposite steel cables, and a cable support assembly is installed between the two steel cables.The load-bearing frame device includes a cross-shaped support, a first lifting arm is installed in front of the left arm, a second lifting arm is installed in front of the right arm, a plurality of adjusting connection holes are provided on the two lifting arms, a lifting lug is installed at the position of one of the adjusting connection holes using a connecting bolt, the lower ends of the two steel cables are connected to the two lifting lugs, a first support is installed on the inner side of the upper arm of the cross-shaped support, a second support is installed on the inner side of the lower arm of the cross-shaped support, a first adapter seat is installed at the front end of the first support through a hinge shaft, and a second adapter seat is installed at the front end of the second support through a hinge shaft.The present application has the advantages of simple structure, convenient operation, reduced labor intensity, improved cabin assembly efficiency and assembly process stability.
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Description

TECHNICAL FIELD

[0001] The present application belongs to the technical field of aerospace equipment, and particularly relates to a lifting appliance capable of vertically lifting and overturning a hoisted object. BACKGROUND

[0002] With the increasing demand for fast-paced, fast-response and multi-task launching of aerospace rockets and the increasing launch density, higher and higher requirements are put forward for the assembly speed of the rocket.

[0003] In the existing rocket cabin section assembly process, overturning and hoisting need to be performed, and in the existing operation mode, the overturning and hoisting of the cabin section is usually realized by using a hand-operated hoist, specifically: the cabin section is first lifted vertically, and then the hand-operated hoist is used to overturn the cabin section from the vertical posture to the horizontal posture. In this process, the hand-operated hoist is low in efficiency, long in operation time, and prolongs the overall assembly time of the rocket cabin section. In addition, in the existing operation mode, the labor intensity is large, and when manually realizing the rapid overturning of a cabin section weighing several hundred kilograms, the overturning resistance is large, so how to enable the manual labor to exert a small force to realize the overturning of the cabin section is one of the significant needs in the industry. Furthermore, in the existing operation, under the working condition of installing a large rudder surface on the tail section of the rocket, the steel cable and the rudder surface often interfere with each other during the hoisting and assembly overturning of the tail end, resulting in difficulty in hoisting and assembly overturning.

[0004] In summary, it is necessary to develop and design a lifting appliance facility for assisting in the hoisting and assembly of the rocket cabin section and having an overturning function. SUMMARY

[0005] The present application provides a lifting appliance capable of vertically lifting and overturning a hoisted object, which has the advantages of simple structure, convenient operation, reduced labor intensity, improved cabin section assembly efficiency and assembly process stability. In the process of rocket cabin section assembly, the lifting appliance can quickly realize the overturning of the cabin section from the vertical state to the horizontal state, while avoiding large overturning torque and mutual interference between the steel cable and the rudder surface during the overturning and hoisting process.

[0006] The technical scheme adopted by the present application to solve the technical problems existing in the prior art is: a lifting device capable of vertically lifting and overturning a hoisted object comprises a hanging device and a force bearing frame device installed at the bottom of the hanging device; the hanging device comprises two opposite steel cables, and a cable supporting assembly is installed between the two steel cables to support the middle part of the two steel cables apart by a certain distance; the force bearing frame device comprises a cross-shaped support, a first lifting arm is installed in front of the left arm of the cross-shaped support, a second lifting arm is installed in front of the right arm of the cross-shaped support, a plurality of adjusting connection holes are arranged on the first lifting arm and the second lifting arm respectively, a lifting lug is installed on one of the adjusting connection holes by using a connecting bolt, the lower ends of the two steel cables are connected with the two lifting lugs respectively, a first support is installed on the inner side of the upper arm of the cross-shaped support, a second support is installed on the inner side of the lower arm of the cross-shaped support, a first transfer seat is installed at the front end of the first support by using a hinge shaft, and a second transfer seat is installed at the front end of the second support by using a hinge shaft.

[0007] Preferably, the first transfer seat comprises a T-shaped first transfer plate and a U-shaped first transfer base, the middle part of the first transfer plate is fixedly connected with the front end of the first transfer base, connecting holes are arranged at the two ends of the first transfer plate, and the front end of the first support is located in the groove of the first transfer base and is hingedly connected by using the hinge shaft.

[0008] Preferably, the second transfer seat comprises a T-shaped second transfer plate and a U-shaped second transfer base, the middle part of the second transfer plate is fixedly connected with the front end of the second transfer base, connecting holes are arranged at the two ends of the second transfer plate, and the front end of the second support is located in the groove of the second transfer base and is hingedly connected by using the hinge shaft.

[0009] Preferably, the first support is a T-shaped shaft seat, the diameter of the outer end of the first support is greater than the diameter of the inner end, and the outer end of the first support is fixedly welded with the upper arm of the cross-shaped support; the second support is a T-shaped shaft seat, the diameter of the outer end of the second support is greater than the diameter of the inner end, and the outer end of the second support is fixedly welded with the lower arm of the cross-shaped support.

[0010] Preferably, triangular reinforcing rib plates are welded and installed between the adjacent arms of the cross-shaped support, between the left arm and the first lifting arm, and between the right arm and the second lifting arm.

[0011] Preferably, the cable supporting assembly comprises a supporting cross beam, upper end inwardly inclined supporting inner plates are welded and installed at the two ends of the supporting cross beam, fixed outer plates are arranged on the outer sides of the supporting inner plates, the supporting inner plates and the fixed outer plates are fixedly connected by using a plurality of bolts, and the middle part of the steel cable is clamped and fixed between the supporting inner plates and the fixed outer plates.

[0012] Preferably, lifting rings are arranged at the upper ends and the lower ends of the steel cables, and the lifting rings at the lower ends of the steel cables are connected with the lifting lugs.

[0013] The present application has the following advantages and positive effects:

[0014] The present application provides a hoist with reasonable structure design, which can vertically lift and overturn the hoisted object, and is applied to the auxiliary operation of the cabin segment hoisting and assembly operation in the rocket cabin segment hoisting and assembly operation. Compared with the existing hoist device and hoisting mode, the hoist in the present application avoids the problem of mutual interference between the steel cable and the rudder surface in the overturning hoisting process by setting the stay cable assembly between the two steel cables and spreading the two steel cables.

[0015] In the present application, the force bearing frame device is set, and the force bearing frame device is composed of a cross-shaped support, two opposite hoisting arms, and two groups of inner supports and adapter seats, so that the hoisted object, that is, the rocket cabin segment, is easily fixed and connected to the force bearing frame device, and is easily disassembled after the hoisting and assembly operation is completed, which is convenient to operate.

[0016] In the present application, the lower ends of the two steel cables are connected with the first hoisting arm and the second hoisting arm of the force bearing frame device through the lifting lugs and connecting bolts, and the positions of the two lifting lugs on the first hoisting arm and the second hoisting arm can be adjusted and set, so that after the hoisted object, that is, the rocket cabin segment, is installed on the present hoist, the distance between the connecting line of the lifting point and the center of gravity of the hoisted object can be minimized by adjusting the connection position between the lifting lug and the hoisting arm, which can avoid a large overturning torque, make the operation easier to perform, reduce the labor intensity of manual operation, improve the cabin assembly efficiency and improve the stability and safety of the assembly process. BRIEF DESCRIPTION OF DRAWINGS

[0017] Figure 1 is a structural schematic diagram of the present application, in a vertical attitude;

[0018] Figure 2 is a structural schematic diagram of the hoisting device in the present application;

[0019] Figure 3 is a structural schematic diagram of the force bearing frame device in the present application, an external view;

[0020] Figure 4 is a structural schematic diagram of the force bearing frame device in the present application, an external view;

[0021] Figure 5 is a structural schematic diagram of the force bearing frame device in the present application, an internal view;

[0022] Figure 6 is a structural schematic diagram of the present application, in a horizontal attitude.

[0023] In the drawings:

[0024] 1, steel cable; 2, support inner plate; 3, fixed outer plate; 4, support crossbeam; 5, bearing frame device; 51, cross-shaped support; 52, first lifting arm; 53, second lifting arm; 54, adjusting connecting hole; 55, first adapter seat; 56, second adapter seat; 57, first support; 58, second support; 59, hinged shaft; 6, lifting lug; 7, connecting bolt. DETAILED DESCRIPTION

[0025] In order to further understand the invention content, characteristics and effects of the present application, the following examples are described in detail.

[0026] Please refer to Figure 1 and Figure 6 , the lifting device of the present application can vertically lift and overturn the lifted object, which comprises a hanging device and a bearing frame device 5 installed at the bottom of the hanging device. The upper end of the hanging device is connected with the crane equipment, the lower end of the hanging device is connected with the bearing frame device 5, and the lifted object, i.e. the rocket cabin section, is installed on the bearing frame device 5, Figure 1 , which is a structural schematic diagram of the present lifting device in a vertical posture, Figure 6 , which is a structural schematic diagram of the present lifting device in a horizontal posture. In the process of auxiliary lifting and assembly, the state of the present lifting device is changed from the state in Figure 1 to the state in Figure 6 .

[0027] Please refer to Figure 1 and Figure 2 , it can be seen that:

[0028] The hanging device comprises two opposite steel cables 1, and a cable supporting assembly is installed between the two steel cables 1 to support the middle part of the two steel cables 1 at a certain distance. By using the cable supporting assembly to support the two steel cables 1, the problem of interference between the steel cables 1 and the lifted object during lifting and assembly is effectively avoided, and the stability and safety of the lifting and assembly process are ensured.

[0029] In this embodiment, a lifting lug is arranged at the upper end and the lower end of each of the two steel cables 1. The lifting lug at the upper end is used to connect with the crane equipment, and the lifting lug at the lower end is used to connect with the bearing frame device 5.

[0030] In this embodiment, the cable supporting assembly comprises a support crossbeam 4, and an upper end inwardly inclined support inner plate 2 is welded and installed at both ends of the support crossbeam 4. A fixed outer plate 3 is arranged on the outer side of the support inner plate 2, and the support inner plate 2 and the fixed outer plate 3 are fixedly connected by a plurality of bolts. The middle part of the steel cable 1 is clamped and fixed between the support inner plate 2 and the fixed outer plate 3.

[0031] As shown in the figure, the length dimension of the support beam 4 is greater than the width dimension of the load-bearing frame device 5, and different opening effects can be generated on the two steel cables 1 when the support cable assembly is moved. When displacement is required, the bolts between the two sets of support inner plates 2 and the fixed outer plates 3 are first disassembled, the steel cables 1 are pulled to displace them, and then the fixed outer plates 3 are buckled on the support inner plates 2, and the bolts are installed and fastened. The steel cables 1 are clamped and fixed between the support inner plates 2 and the fixed outer plates 3.

[0032] Please refer to Figure 3 , Figure 4 and Figure 5 It can be seen that:

[0033] The load-bearing frame device 5 includes a cross-shaped support 51 having upper, lower, left and right arms arranged in a cross shape.

[0034] A first boom 52 is installed in front of the left arm of the cross-shaped support 51, and a second boom 53 is installed in front of the right arm of the cross-shaped support 51. A plurality of adjustment connection holes 54 are provided on the first boom 52 and the second boom 53, respectively, and a lifting lug 6 is installed at the position of one of the adjustment connection holes 54 by a connecting bolt 7. The lower ends of the two steel cables 1 are connected to the two lifting lugs 6, respectively. As shown in the figure, the left arm and the first boom 52 are arc-shaped transitioned, and the right arm and the second boom 53 are arc-shaped transitioned.

[0035] In this embodiment, triangular reinforcing rib plates are welded and installed between adjacent arms of the cross-shaped support 51, as well as between the left arm and the first boom 52 and between the right arm and the second boom 53, to improve the overall structural strength of the load-bearing frame device 5. The main part of the load-bearing frame device 5 can be processed by one-piece casting to further improve the overall structural strength.

[0036] As shown in the figure, the first boom 52 and the second boom 53 each have a plurality of transversely penetrating adjustment connection holes 54, and the adjustment connection holes 54 are arranged at equal intervals. The lifting lug 6 includes a lug plate, and a connection hole is provided at the upper end and the lower end of the lug plate. The connecting bolt 7 penetrates the adjustment connection hole 54 and the connection hole at the lower end of the lifting lug 6, and the lifting ring at the lower end of the steel cable 1 is connected to the connection hole at the upper end of the lifting lug 6. When the lifting point position needs to be adjusted, the connecting bolt 7 is disassembled and the lifting lug 6 is installed at the position of another adjustment connection hole 54.

[0037] A first support 57 is installed inside the upper arm of the cross-shaped support 51, and a second support 58 is installed inside the lower arm of the cross-shaped support 51. A first adapter seat 55 is installed at the front end of the first support 57 through a hinge shaft 59, and a second adapter seat 56 is installed at the front end of the second support 58 through a hinge shaft 59. Among them, the first support 57 and the second support 58 both play a supporting role, and the first adapter seat 55 and the second adapter seat 56 are used to install the hoisted object, that is, the rocket cabin section.

[0038] In this embodiment, the first adapter 55 includes a T-shaped first adapter plate and a U-shaped first adapter base. The middle part of the first adapter plate is welded and fixedly connected to the front end of the first adapter base. Connection holes are provided at both ends of the first adapter plate. The front end of the first support 57 is located in the groove of the first adapter base and is hinged by the hinge shaft 59.

[0039] In this embodiment, the second adapter 56 includes a T-shaped second adapter plate and a U-shaped second adapter base. The middle part of the second adapter plate is welded and fixedly connected to the front end of the second adapter base. Connection holes are provided at both ends of the second adapter plate. The front end of the second support 58 is located in the groove of the second adapter base and is hinged by the hinge shaft 59.

[0040] As shown in the figure, the first adapter 55 and the second adapter 56 are arranged opposite each other, that is, symmetrically arranged with the center plane of the first boom 52 and the second boom 53 as the center. The object to be lifted, i.e. the rocket section, is placed between the first boom 52 and the second boom 53. The end of the rocket section is provided with a reserved connection point. Each reserved connection point is connected to the first adapter 55 and the second adapter 56 by bolts. Specifically, the bolts are passed through the connection holes on the adapter plates of the first adapter 55 and the second adapter 56 and the connection holes at the reserved connection point positions.

[0041] In this embodiment, the first support 57 is a T-shaped shaft seat with a diameter at its outer end greater than that at its inner end. The outer end of the first support 57 is welded and fixed to the upper arm of the cross-shaped bracket 51. The second support 58 is a T-shaped shaft seat with a diameter at its outer end greater than that at its inner end. The outer end of the second support 58 is welded and fixed to the lower arm of the cross-shaped bracket 51.

[0042] like Figure 5 As shown, since the first adapter 55 is hinged to the first support 57 and the second adapter 56 is hinged to the second support 58, the load-bearing frame device 5 can be connected to the suspended object in two states: one is as follows Figure 5 In one embodiment, both the first adapter 55 and the second adapter 56 are deflected to the inside. In another embodiment, both the first adapter 55 and the second adapter 56 are each rotated outward by 90° with the hinge axis 59 as the center.

[0043] Operation method:

[0044] Before the hoisting operation, the object to be hoisted, i.e. the rocket compartment, is in a vertical position. The hoisting equipment is used to move and lower the hoisting device, so that the load-bearing frame device 5 is moved to the upper part of the rocket compartment. The hoisting device is then lowered so that the load-bearing frame device 5 is perpendicularly connected to the object to be hoisted, and the upper part of the object to be hoisted is fixedly connected to the first adapter 55 and the second adapter 56.

[0045] According to the calculation of the center of gravity of the hoisted object, the mounting positions of the two lifting lugs 6 on the two lifting arms are adjusted to minimize the distance between the connecting line between the lifting points on the first lifting arm 52 and the second lifting arm 53 and the center of gravity of the hoisted object, so as to reduce the overturning moment and make the lifting and overturning operation easier to perform;

[0046] After the connection of the hoisted object is completed, the crane equipment starts to lift, lifts the present lifting tool and the rocket cabin section to a certain height, and then overturns the load-bearing frame device 5 under the action of manual assistance, so that the state of the present lifting tool changes from the vertical state shown in Figure 1 to the horizontal state shown in Figure 6 In this process, the rocket cabin section changes from a vertical posture to a horizontal posture, and then assembly is performed; after the assembly is completed, the connection between the end of the rocket cabin section and the first adapter seat 55 and the second adapter seat 56 is released, the present lifting tool is lifted and transferred by the crane equipment to be separated from the rocket cabin section.

Claims

1. A lifting device capable of vertically lifting and tilting the suspended object, characterized in that: The utility model provides a kind of lifting device, including hanging device and the force frame device (5) installed at the bottom of hanging device;Hanging device includes two opposite steel cables (1), and the middle part of two steel cables (1) is supported a certain distance apart by supporting cable assembly installed between two steel cables (1);Force frame device (5) includes cross type support (51), first boom (52) is installed in the front of left arm of cross type support (51), second boom (53) is installed in the front of right arm of cross type support (51), a plurality of adjusting connection holes (54) are respectively provided on first boom (52) and second boom (53), and lug (6) is installed in the position of one of adjusting connection holes (54) using connecting bolt (7), the lower end of two steel cables (1) is connected with two lugs (6) respectively, first support (57) is installed in the inner side of upper arm of cross type support (51), second support (58) is installed in the inner side of lower arm of cross type support (51), first adapter seat (55) is installed in the front end of first support (57) by hinged axle (59), second adapter seat (56) is installed in the front end of second support (58) by hinged axle (59).

2. The lifting device according to claim 1, wherein: First adapter seat (55) includes T-shaped first adapter plate and U-shaped first adapter base, the middle part of first adapter plate is fixedly connected with the front end of first adapter base, connecting hole is provided at both ends of first adapter plate, the front end of first support (57) is located in the groove of first adapter base and is hingedly connected using the hinged axle (59).

3. The lifting device of claim 2, wherein: Second adapter seat (56) includes T-shaped second adapter plate and U-shaped second adapter base, the middle part of second adapter plate is fixedly connected with the front end of second adapter base, connecting hole is provided at both ends of second adapter plate, the front end of second support (58) is located in the groove of second adapter base and is hingedly connected using the hinged axle (59).

4. The lifting device of claim 3, wherein: First support (57) is T-shaped axle seat, the diameter of outer end is greater than the diameter of inner end, and the outer end of first support (57) is welded and fixed with the upper arm of cross type support (51);Second support (58) is T-shaped axle seat, the diameter of outer end is greater than the diameter of inner end, and the outer end of second support (58) is welded and fixed with the lower arm of cross type support (51).

5. The lifting device of claim 4, wherein: Triangular reinforcing rib plate is welded and installed between adjacent arms of cross type support (51), between left arm and first boom (52), and between right arm and second boom (53).

6. The lifting device of claim 5, wherein: Supporting inner plate (2) is welded and installed at both ends of supporting cross beam (4) and inclines inward, fixed outer plate (3) is arranged at the outer side of supporting inner plate (2), and supporting inner plate (2) and fixed outer plate (3) are fixedly connected by a plurality of bolts, and the middle part of steel cable (1) is clamped and fixed between supporting inner plate (2) and fixed outer plate (3).

7. The lifting device of claim 6, wherein: Lifting ring is arranged at the upper end and the lower end of steel cable (1), and the lifting ring at the lower end of steel cable (1) is connected with lug (6).

Citation Information

Patent Citations

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