CN219838938U - Equipment for rocket transport - Google Patents

Equipment for rocket transport Download PDF

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Publication number
CN219838938U
CN219838938U CN202320990771.4U CN202320990771U CN219838938U CN 219838938 U CN219838938 U CN 219838938U CN 202320990771 U CN202320990771 U CN 202320990771U CN 219838938 U CN219838938 U CN 219838938U
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China
Prior art keywords
pull rod
plate
transportation
push
pull
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CN202320990771.4U
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Chinese (zh)
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罗唯烜
邓世翚
窦洪康
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Wuhan Dawson Aerospace Technology Co ltd
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Wuhan Dawson Aerospace Technology Co ltd
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Abstract

The utility model discloses rocket transferring equipment, which comprises a box body, a transportation underframe, push-pull assemblies, axial limiting devices, quick-release universal wheels, brackets and quick-release tower buckles, wherein the push-pull assemblies are connected to the middle of two ends of the transportation underframe, the push-pull assemblies are connected to the transportation underframe through pin shafts, the axial limiting devices are arranged above the two ends of the transportation underframe, the axial limiting devices are positioned on the side edges of the push-pull assemblies, the bases of the axial limiting devices are connected to the transportation underframe through bolts, the bottom of the transportation underframe is fixedly provided with a plurality of quick-release universal wheels, three brackets are uniformly and fixedly connected above the transportation underframe, the box body is arranged on the transportation underframe, and a plurality of quick-release tower buckles are arranged around the bottom of the box body and are buckled with the transportation underframe. The utility model realizes the short-distance transportation of the rocket by only pushing and pulling manually without the assistance of a transfer trolley, reduces transfer equipment and saves repeated loading and unloading time.

Description

Equipment for rocket transport
Technical Field
The utility model relates to the technical field of rocket transportation, in particular to equipment for rocket transportation.
Background
Along with the continuous development of the aerospace technology, the rocket is taken as a spaceflight tool, and artificial earth satellites, manned spacecraft, space stations, space detectors and the like are fed into a preset orbit, so that the rocket is greatly launched, and along with the wider and wider application of the rocket, the rocket transporting equipment has to be mentioned. At present, the packaging box equipment for rocket transportation is basically only suitable for long-distance transportation, the rocket transportation at a short distance needs a transfer car, and because the rocket main body is huge, the transportation process is complex, and when in short-distance transportation, a plurality of equipment is often needed to be matched, repeated loading and unloading are carried out, and the fixed safety risk exists in the repeated loading and unloading process.
Chinese patent CN113771727a discloses a rocket transporting vehicle for docking and adjusting a launching cradle, the transporting vehicle comprising: the device comprises a transfer trolley, a fixing frame, a transverse adjusting device, a longitudinal adjusting and compressing device and a locking device; the fixing frame is arranged on the transfer trolley; the transverse adjusting device comprises a plurality of transverse adjusting oil cylinders symmetrically arranged at two sides of the transfer trolley; the transverse adjusting cylinders are arranged along the transverse direction of the transfer trolley and fixed on the fixing frame; the longitudinal adjustment compacting device comprises a plurality of longitudinal adjustment cylinders symmetrically arranged at the front end and the rear end of the transfer cart; the plurality of longitudinal adjustment cylinders are arranged along the longitudinal direction of the transfer trolley and are fixed on the fixing frame; the locking device is arranged on the fixing frame; the locking device is used for locking and connecting the transfer trolley and the transmitting frame. The utility model realizes the rapid butt joint of the rocket transfer vehicle and the launching frame and ensures the butt joint precision of the rocket transfer vehicle and the launching frame.
The prior art has a complex structure, the rocket can be transported under the condition of a powered device, special equipment with simple structure and convenient transportation is needed in the rocket short-distance transportation process, the loading and unloading can be fast carried out, the risk of loading and unloading is avoided, the holding of the transportation equipment can be reduced, and meanwhile, the safe transportation of the rocket and the short-distance transportation work of convenience and rapidness can be realized.
Disclosure of Invention
Based on the technical problems in the background technology, the utility model provides the equipment for rocket transportation, which has the advantages of simple structure, convenient transportation, rapid loading and unloading, reduced transportation equipment, time saving and convenient, rapid and safe realization of short-distance transportation work of the rocket only by manual pushing and pulling.
In order to achieve the above purpose, the present utility model adopts the following technical scheme:
the utility model provides a equipment for rocket is transported, includes box, transportation chassis, push-and-pull subassembly, axial stop device, quick detach type universal wheel, bracket and quick detach formula tower knot, the centre at transportation chassis both ends all is connected with push-and-pull subassembly, and push-and-pull subassembly passes through the round pin hub connection on the transportation chassis, the top at transportation chassis both ends all is equipped with axial stop device, axial stop device is located push-and-pull subassembly's side, axial stop device's base passes through bolted connection on the transportation chassis, the bottom of transportation chassis is fixed with a plurality of quick detach type universal wheels, transportation chassis top equipartition fixedly connected with three bracket, be equipped with the box on the transportation chassis, be equipped with a plurality of quick detach formula tower knots around the bottom of the box, quick detach formula tower knot and transportation chassis lock joint.
Preferably, the bracket comprises a front plate and a rear plate, the bottom of the front plate and the bottom of the rear plate are welded with connecting plates, the bottom of the bracket is matched with the connecting plates through clamping grooves of the transportation underframe and is fixed, the front plate and the rear plate are connected with a clamp, the right end of the clamp is connected with the right upper end of the front plate and the rear plate through a pin shaft, n-type groove plates are welded in cavities of the left end plates of the front plate and the rear plate, a slipknot bolt is vertically arranged at the center position of the top of the n-type groove plates, and the head of the slipknot bolt is connected with the left end of the clamp through the pin shaft.
Preferably, the push-pull assembly comprises a first pull rod connecting plate and a second pull rod connecting plate fixed on the transport underframe; a pull rod is arranged between the first pull rod connecting plate and the second pull rod connecting plate, and the first pull rod connecting plate and the second pull rod connecting plate are movably connected through a first pin; the side of pull rod is provided with the second pull rod fixed plate, the top of first pull rod connecting plate is equipped with first pull rod fixed plate, the second pull rod fixed plate is located directly over the first pull rod fixed plate, first pull rod fixed plate and second pull rod fixed plate are connected through the second pin.
Compared with the prior art, the utility model has the following beneficial effects:
(1) According to the utility model, the rocket is placed on the bracket of the transport underframe, the two ends of the bracket clamp are connected by adopting pins, so that the bracket clamp is vertically fixed, the two ends of the rocket are adjusted to be fixed on the axial limiting device of the transport underframe, so that the rocket is propped against the rocket, the front and back movement of the rocket can be prevented, then the rocket is sleeved by the box body, the transport underframe is connected through the quick-release tower buckle around the box body, and the reloading and fixing process is very convenient and quick
(2) According to the utility model, after the rocket is fixed, the foot brake of the quick-release universal wheel on the transport underframe is loosened, and the pull rod of the push-pull assembly is manually pulled, so that the short-distance transport of the rocket can be realized, the transport is convenient, the transport equipment is reduced, the time is saved, the short-distance transport work of the rocket can be conveniently, quickly and safely realized by only manual push-pull, the power transport is not needed, the efficiency in the short-distance transport of the rocket is improved, and the maneuvering resources are saved.
Drawings
FIG. 1 is a schematic view of an apparatus for rocket transport according to the present utility model;
FIG. 2 is a schematic view of the bracket structure of the present utility model;
FIG. 3 is a schematic view of a push-pull assembly of the present utility model;
fig. 4 is an enlarged schematic view of a portion of an apparatus for rocket transporting according to the present utility model.
The reference numerals are as follows: 1. a case; 2. a transport chassis; 3. a push-pull assembly; 4. an axial limiting device; 5. quick-dismantling universal wheels; 6. a bracket; 7. quick-release tower buckles; 8. a rocket; 6-1, front and rear plates; 6-2, connecting the plates; 6-3, clamping hoop; 6-4, U-shaped groove plates; 6-5, a slipknot bolt; 3-1 a first pull rod connecting plate; 3-2, a second pull rod connecting plate; 3-3, a first pull rod fixing plate; 3-4 second pull rod fixing plates; 3-5, a second pin; 3-6, a first pin; 3-7, pull rod
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and fully with reference to the accompanying drawings, in which it is evident that the embodiments described are some, but not all embodiments of the utility model. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Example 1
The utility model provides a equipment for rocket is transported, includes box 1, transportation chassis 2, push-and-pull subassembly 3, axial stop device 4, quick detach universal wheel 5, bracket 6 and quick detach formula tower knot 7, the centre at transportation chassis 2 both ends all is connected with push-and-pull subassembly 3, and push-and-pull subassembly 3 passes through the round pin hub connection on transportation chassis 2, the top at transportation chassis 2 both ends all is equipped with axial stop device 4, axial stop device 4 is located the side of push-and-pull subassembly 3, the base of axial stop device 4 passes through bolted connection on transportation chassis 2, the bottom of transportation chassis 2 is fixed with a plurality of quick detach formula universal wheels 5, transportation chassis 2 top equipartition fixedly connected with three bracket 6, be equipped with box 1 on the transportation chassis 2, be equipped with a plurality of quick detach formula tower knots 7 around the bottom of box 1, quick detach formula tower knot 7 and transportation chassis 2 lock joint can realize transporting the function.
In this embodiment, the bracket 6 includes front and back plates 6-1, the connecting plate 6-2 is welded at the bottom of the front and back plates 6-1, the bottom of the bracket 6 is fixed to the connecting plate 6-2 through the clamping groove of the transport chassis 2, the front and back plates 6-1 are connected with the clamp 6-3, the right end of the clamp 6-3 is connected with the right upper end of the front and back plates 6-1 through a pin shaft, the n-shaped groove plate 6-4 is welded in the cavity of the left end plate of the front and back plates 6-1, a slipknot bolt 6-5 is vertically arranged at the center position of the top of the n-shaped groove plate 6-4, and the head of the slipknot bolt 6-5 is connected with the left end of the clamp 6-3 through a pin shaft, so that the vertical limiting of the rocket is realized.
In this embodiment, the push-pull assembly 3 comprises a first pull rod connecting plate 3-1 and a second pull rod connecting plate 3-2 fixed on the transport chassis 2; a pull rod 3-7 is arranged between the first pull rod connecting plate 3-1 and the second pull rod connecting plate 3-2, and the first pull rod connecting plate 3-1 and the second pull rod connecting plate are movably connected through a first pin 3-6; the side of pull rod 3-7 is provided with second pull rod fixed plate 3-4, the top of first pull rod connecting plate 3-1 is equipped with first pull rod fixed plate 3-3, second pull rod fixed plate 3-4 is located first pull rod fixed plate 3-3 directly over, first pull rod fixed plate 3-3 and second pull rod fixed plate 3-4 are connected through second pin 3-5.
The application principle of the utility model is as follows:
according to the utility model, the quick-release universal wheel is manually fixed before the vehicle is assembled, the foot brake is stepped down to enable the foot brake to be unable to move, the rocket 8 is hoisted and placed in an inner arc of a front plate 6-1 and a rear plate 6-1 of a bracket 6, the right end of the rocket is connected with the right end of a clamp 6-3 through a pin shaft, the clamp 6-3 is hooped with the rocket, a loose joint bolt 6-5 at the left end of the front plate 6-1 and the rear plate 6-1 is adjusted, after the adjustment is completed, an outer hexagonal nut 6-6 is screwed to the upper surface of the 6-4 to enable the loose joint bolt 6-5 to be fastened, the head of the loose joint bolt 6-5 is connected with a through hole reserved at the left end of the clamp 6-3 through the pin shaft, vertical limit is carried out on the rocket 8, the bolts at the top and the top of an axial limiting device 4 at the tail end of the rocket 8 are adjusted, the bolts are adjusted to be fixed against the end of the rocket 8, the axial positioning of the rocket 8 is realized, the box 1 is hoisted and is placed on the transport chassis 2, the quick-release universal wheel 5 is loosened through the quick-release tower 7 around the box 1, after the rocket is assembled, the quick-release universal wheel 5 is fastened, the quick-release universal wheel 5 is enabled to rotate, the push-pull assembly is pulled down, the second universal wheel 3 is required to be pulled to be matched with the vertical pull rod 3, and the quick-pull assembly is required to be pulled to be rotated, and turned to be matched with the vertical to be in a certain angle 3.
The foregoing is only a preferred embodiment of the present utility model, but the scope of the present utility model is not limited thereto, and any person skilled in the art, who is within the scope of the present utility model, should make equivalent substitutions or modifications according to the technical scheme of the present utility model and the inventive concept thereof, and should be covered by the scope of the present utility model.

Claims (3)

1. The utility model provides a device for rocket transporting, its characterized in that, including box (1), transportation chassis (2), push-and-pull subassembly (3), axial stop device (4), quick detach universal wheel (5), bracket (6) and quick detach formula tower knot (7), the centre at transportation chassis (2) both ends all is connected with push-and-pull subassembly (3), and push-and-pull subassembly (3) all are equipped with axial stop device (4) through the round pin hub connection on transportation chassis (2), the top at transportation chassis (2) both ends all is equipped with axial stop device (4), axial stop device (4) are located the side of push-and-pull subassembly (3), the base of axial stop device (4) passes through bolted connection on transportation chassis (2), the bottom of transportation chassis (2) is fixed with a plurality of quick detach formula universal wheels (5), transportation chassis (2) top equipartition fixedly connected with three bracket (6), be equipped with box (1) on transportation chassis (2), box (1) bottom all around is equipped with a plurality of quick detach formula tower knot (7), quick detach formula tower knot (2) and connect.
2. An apparatus for rocket transporting according to claim 1, wherein the bracket (6) comprises a front plate (6-1) and a rear plate (6-1), the bottom of the front plate (6-1) is welded with a connecting plate (6-2), the bottom of the bracket (6) is fixed to the connecting plate (6-2) through the fit of the clamping groove of the transport chassis (2), the front plate (6-1) and the rear plate (6-1) are connected with a clamp (6-3), the right end of the clamp (6-3) is connected with the right upper end of the front plate (6-1) through a pin shaft, an n-shaped groove plate (6-4) is welded in the cavity of the left end plate of the front plate (6-1), a slipknot bolt (6-5) is vertically arranged at the center position of the top of the n-shaped groove plate (6-4), and the head of the slipknot bolt (6-5) is connected with the left end of the clamp (6-3) through a pin shaft.
3. An apparatus for rocket transport according to claim 1, wherein the push-pull assembly (3) comprises a first drawbar connection plate (3-1) and a second drawbar connection plate (3-2) fixed to the transport chassis (2); a pull rod (3-7) is arranged between the first pull rod connecting plate (3-1) and the second pull rod connecting plate (3-2), and the first pull rod connecting plate, the second pull rod connecting plate and the second pull rod connecting plate are movably connected through a first pin (3-6); the side of pull rod (3-7) is provided with second pull rod fixed plate (3-4), the top of first pull rod connecting plate (3-1) is equipped with first pull rod fixed plate (3-3), second pull rod fixed plate (3-4) are located directly over first pull rod fixed plate (3-3), first pull rod fixed plate (3-3) and second pull rod fixed plate (3-4) are connected through second pin (3-5).
CN202320990771.4U 2023-04-27 2023-04-27 Equipment for rocket transport Active CN219838938U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202320990771.4U CN219838938U (en) 2023-04-27 2023-04-27 Equipment for rocket transport

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202320990771.4U CN219838938U (en) 2023-04-27 2023-04-27 Equipment for rocket transport

Publications (1)

Publication Number Publication Date
CN219838938U true CN219838938U (en) 2023-10-17

Family

ID=88298755

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202320990771.4U Active CN219838938U (en) 2023-04-27 2023-04-27 Equipment for rocket transport

Country Status (1)

Country Link
CN (1) CN219838938U (en)

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