Transferring and assembling integrated universal adjusting platform for rocket engine

Abstract

The embodiment of the utility model provides a transferring and assembling integrated universal adjusting platform for a rocket engine. The transferring and assembling integrated universal adjusting platform comprises a carrying platform structure and a plurality of supporting leg structures arranged on the carrying platform structure. The loading platform structure comprises a walking assembly, a rotary lifting assembly and a translation assembly; the supporting leg structure is arranged on the side portion of the walking assembly. The rotary lifting assembly is arranged over the walking assembly and used for rotary lifting adjustment driving of the translation assembly. The translation assembly is arranged over the rotary lifting assembly and used for translation adjustment driving of the rocket motor. According to the utility model, the structure arrangement is reasonable, the rotation, transfer and translation operation of an object can be realized as required, the assembly stability can be improved by matching rotation with translation during assembly, the number of operators during the butt joint of a rocket engine and a test bed is reduced, and the production efficiency is improved. The technical defects that the difficulty is large and the consumed time is long when the rocket engine is assembled on the vertical test bed are overcome, and the transfer and assembly efficiency can be improved.

Description

Technical Field

[0001] This utility model relates to the field of rocket transport and assembly technology, specifically to an integrated universal adjustment platform for transporting and assembling rocket engines. Background Technology

[0002] After processing, liquid rockets require transportation and assembly operations. The most common transportation method for liquid rockets is horizontal transport, which requires corresponding transportation and assembly tooling. For example, Chinese patent application number 202010936729.5, patent name: Novel integrated tooling for transporting and flipping liquid rocket engines; and Chinese patent application number 202010936714.9, patent name: A transfer platform for docking rocket engines and rocket bodies with positioning structure.

[0003] In the process of realizing this invention, the inventors discovered that the prior art has at least the following problems: it cannot achieve rotation and flipping adjustment, and requires the use of a lifting device and a test bench thrust frame to complete the transfer and docking operation. Not only is the transfer and docking efficiency low, but it is also easy to cause collision damage to the engine, affecting the effectiveness and stability of transfer and assembly, thus limiting its practicality. Utility Model Content

[0004] In view of this, the purpose of this utility model embodiment is to provide a rocket engine transfer and assembly integrated universal adjustment platform with a reasonable structural design that is conducive to improving transfer and assembly efficiency.

[0005] To achieve the above objectives, this utility model provides an integrated universal adjustment platform for transporting and assembling rocket engines, including a cargo platform structure and a plurality of support leg structures disposed on the cargo platform structure.

[0006] The cargo platform structure includes a walking component, a rotating lifting component, and a translating component;

[0007] The supporting leg structure is disposed on the side of the walking assembly;

[0008] The rotary lifting assembly is positioned directly above the walking assembly and is used for the rotary lifting adjustment drive of the translation assembly;

[0009] The translation component is positioned directly above the rotary lifting component and is used for the translational adjustment drive of the rocket motor.

[0010] A further preferred embodiment is that the rotary lifting assembly includes a support base plate, several screw jacks, several reversing shafts, a lifting servo motor, a rotation motor, a rotary drive gear, a main servo commutator, and several slave servo commutators.

[0011] The supporting base plate is fixed on the lifting flanges of several screw jacks, and the movement of the screw jacks drives the supporting base plate to rise and fall.

[0012] Several of the aforementioned screw jacks are respectively connected to several of the aforementioned slave servo commutators via the reversing shaft;

[0013] Several of the slave servo commutators are connected to the master servo commutator via the commutation shaft;

[0014] The lifting servo motor is connected to the main servo commutator and is used for the lifting drive of the screw jack.

[0015] The rotating motor is fixed to the support base plate, and the rotating drive gear is fixed to the main shaft of the rotating motor;

[0016] The rotating motor is connected to the translation component via the rotating drive gear and is used for the rotational adjustment of the translation component.

[0017] A further preferred embodiment is that the number of screw jacks is four, and the number of slave commutators is two;

[0018] The four screw jacks are connected to the two slave servo commutators via the commutator shafts.

[0019] A further preferred embodiment is that the translation assembly includes an upper top plate, a lower bottom plate, a rotary driven gear, a connecting shaft, and a translation drive structure;

[0020] The center of the lower base plate is rotatably connected to the center of the top surface of the rotary lifting assembly via the connecting shaft;

[0021] The driven gear is fixed to the middle of the bottom surface of the lower base plate and is concentrically arranged with the connecting shaft. The driven gear meshes with the drive gear to achieve rotational drive.

[0022] The translation drive structure is fixed to the top surface of the lower base plate, and the upper top plate is connected to the translation drive structure.

[0023] The translation drive structure moves the upper top plate to translate on the top surface of the lower bottom plate.

[0024] A further preferred embodiment is that the translation drive structure includes a guide rail, a slider, a drive block, a translation control motor, and a translation ball screw;

[0025] The guide rail is fixed to the top surface of the lower base plate;

[0026] The slider is movably mounted on the guide rail, the drive block is helically connected to the translation ball screw, and both the slider and the drive block are fixedly connected to the bottom surface of the upper top plate.

[0027] The translation control motor is fixed to the top surface of the lower base plate, and the translation ball screw is fixed to the main shaft of the translation control motor through a coupling.

[0028] A further preferred embodiment is that a plurality of omnidirectional balls are evenly arranged along the bottom edge of the lower base plate;

[0029] The bottom of the omnidirectional ball is rolled on the top surface of the supporting base plate.

[0030] A further preferred embodiment is that an oil-free bushing is provided at the connection between the connecting shaft and the rotary lifting assembly.

[0031] A further preferred embodiment is that the walking assembly includes a walking base, a walking drive wheel assembly, a walking driven wheel assembly, and a connecting member;

[0032] The walking seat is provided with a through groove;

[0033] Both the driving wheel assembly and the driven wheel assembly are disposed on the top surface of the traveling seat, and the driving wheel assembly and the driven wheel assembly are connected to each other through the connecting member;

[0034] The wheel edges of the driving wheel assembly and the driven wheel assembly pass through the through groove and extend out of the bottom surface of the walking seat;

[0035] The rotary lifting assembly includes several screw jacks, the bottom of which is fixed to the traveling seat.

[0036] A further preferred embodiment is that the walking drive wheel assembly includes a wheel, a walking drive motor, a steering motor, a walking main gear, a walking transmission gear, a steering gear, a transmission chain, a crank, sector teeth, a steering drive gear, and a connecting rod;

[0037] The wheel is connected to the travel transmission gear via the crank, and the travel drive motor meshes with the travel transmission gear via the travel main gear;

[0038] The steering drive gear is fixed on the main shaft of the steering motor, the transmission gear chain is connected between the steering drive gear and the steering gear, and the steering gear meshes with the sector teeth;

[0039] The sector teeth are connected to the crank, and the steering drive gear drives the sector teeth to rotate and realizes the steering adjustment of the crank;

[0040] The two ends of the connecting rod are connected between the two cranks, so that the two cranks turn synchronously.

[0041] A further preferred embodiment is that the support leg structure includes a boom, a forearm, a lifting electric cylinder, and a telescopic electric cylinder;

[0042] The forearm is telescopically mounted in the telescopic cavities at both ends of the upper arm, and the telescopic electric cylinder is fixed between the telescopic cavities of the forearm and the upper arm.

[0043] The rotary lifting assembly includes a support base plate, the boom is fixed on the support base plate, and the lifting cylinder is fixed to the end of the forearm that extends out of the support base plate, for adjusting the lifting of the support base plate.

[0044] A further preferred embodiment is that a guide roller is provided between the telescopic cavity of the forearm and the upper arm;

[0045] A foot pad is fixed to the bottom surface of the end of the forearm that extends out of the supporting base plate.

[0046] The above technical solution has the following beneficial effects:

[0047] 1. The structure of this utility model is reasonable. Its cargo platform structure includes a walking component, a rotating lifting component, and a translating component. It can realize the rotation, transfer and translation operations of the cargo as needed. During assembly, the stability of the assembly can be improved by rotating and translating, which helps to reduce the number of operators when docking the rocket engine with the test stand. It also solves the technical shortcomings of the rocket engine assembly on the vertical test stand, which is difficult and time-consuming. It also helps to improve the efficiency of transfer and assembly.

[0048] 2. The rotary lifting assembly includes a support base plate, several screw jacks, several reversing shafts, a lifting servo motor, a rotary motor, a rotary drive gear, a main servo commutator, and several slave servo commutators. Through the above structure, the effectiveness and stability of the rotary lifting can be improved, and the vertical adjustment operation can be realized through the lifting servo motor to meet the assembly and use requirements of different situations.

[0049] 3. The translation assembly includes an upper top plate, a lower bottom plate, a rotary driven gear, a connecting shaft, and a translation drive structure; it helps improve the effectiveness and stability of translation, while also being easy to operate;

[0050] 4. The traveling assembly includes a traveling base, a traveling drive wheel assembly, a traveling driven wheel assembly, and connecting parts; the traveling assembly helps to ensure the effectiveness and stability of the entire structure's transport.

[0051] 5. The travel drive wheel assembly includes wheels, travel drive motor, steering motor, travel main gear, travel transmission gear, steering gear, transmission chain, crank, sector gear, steering drive gear and connecting rod; it can improve the reliability of travel drive and the effectiveness of steering adjustment, and meet the assembly requirements of different positions.

[0052] 6. The support leg structure includes a boom, a forearm, a lifting electric cylinder, and a telescopic electric cylinder; it can be adjusted as needed to meet the requirements of uneven ground conditions, ensuring the parallelism of the engine and the test bench thrust frame docking plane, and improving assembly efficiency and accuracy. Attached Figure Description

[0053] To more clearly illustrate the technical solutions in the embodiments of this utility model or the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0054] Figure 1 This is a structural schematic diagram of an embodiment of the present utility model;

[0055] Figure 2 This is a schematic diagram of the specific structure of the rotary lifting assembly in the embodiment of this utility model;

[0056] Figure 3 This is a schematic diagram of the structure of the rotary lifting assembly and the lower base plate in an embodiment of this utility model;

[0057] Figure 4 This is a schematic diagram of the specific structure of the translation component in the embodiment of this utility model;

[0058] Figure 5 This is a schematic diagram of the translation component from another perspective in an embodiment of this utility model;

[0059] Figure 6 This is a schematic diagram of the specific structure of the walking component in an embodiment of this utility model;

[0060] Figure 7 This is a schematic diagram of the specific structure of the walking drive wheel assembly in the walking assembly of this utility model embodiment;

[0061] Figure 8 for Figure 7 Another perspective on the structure diagram;

[0062] Figure 9 This is a schematic diagram of the supporting leg structure in an embodiment of the present invention;

[0063] Figure 10This is a schematic diagram of the assembly of the support leg structure and the walking component in an embodiment of this utility model.

[0064] Explanation of reference numerals in the attached figures:

[0065] 1. Cargo platform structure; 11. Walking assembly; 111. Walking base; 112. Walking drive wheel assembly; 113. Walking driven wheel assembly; 114. Connecting parts;

[0066] 1121. Wheel; 1122. Drive motor; 1123. Steering motor; 1124. Main drive gear; 1125. Drive transmission gear; 1126. Steering gear; 1127. Drive chain; 1128. Crank; 1129. Sector gear; 11210. Steering drive gear; 11211. Connecting rod;

[0067] 12. Rotary lifting assembly; 121. Support base plate; 122. Screw jack; 123. Reversing shaft; 124. Lifting servo motor; 125. Rotation motor; 126. Rotation drive gear; 127. Master servo commutator; 128. Slave servo commutator;

[0068] 13. Translation component; 131. Upper top plate; 132. Lower bottom plate; 133. Rotary driven gear; 134. Connecting shaft; 135. Translation drive structure;

[0069] 1351, Guide rail; 1352, Slider; 1353, Drive block; 1354, Translation control motor; 1355, Translation ball screw;

[0070] 2. Support leg structure; 21. Boom; 22. Forearm; 23. Lifting electric cylinder; 24. Telescopic electric cylinder;

[0071] 3. Omnidirectional ball;

[0072] 4. Oil-free bushing;

[0073] 5. Through groove;

[0074] 6. Guide rollers;

[0075] 7. Foot pads. Detailed Implementation

[0076] The features and exemplary embodiments of various aspects of this utility model will now be described in detail. Numerous specific details are set forth in the following detailed description to provide a comprehensive understanding of this utility model. However, it will be apparent to those skilled in the art that this utility model can be practiced without requiring some of these specific details. The following description of embodiments is merely intended to provide a better understanding of this utility model by illustrating examples of it. In the accompanying drawings and the following description, at least some well-known structures and techniques have not been shown to avoid unnecessarily obscuring the utility model; and, for clarity, the dimensions of some structures may be exaggerated. Furthermore, the features, structures, or characteristics described below can be combined in any suitable manner in one or more embodiments.

[0077] like Figures 1 to 10 As shown, a rocket engine transfer and assembly integrated universal adjustment platform includes a platform structure 1 and several support leg structures 2 disposed on the platform structure 1. The support leg structures 2 are distributed on both sides of the platform structure 1, and can be adjusted in height and parallelism by finding suitable support points. In this embodiment, the platform structure 1 includes a walking component 11, a rotation and lifting component 12, and a translation component 13. In practical applications, the components of the platform structure 1 can be circular or other common shapes; in this embodiment, they are circular to facilitate rotation and adjustment operations.

[0078] like Figure 1 As shown, during processing and assembly, the support leg structure 2 is located on the side of the walking assembly 11; the rotary lifting assembly 12 is located directly above the walking assembly 11 and is used for the rotary lifting adjustment drive of the translation assembly 13; the translation assembly 13 is located directly above the rotary lifting assembly 12 and is used for the translation adjustment drive of the rocket motor. Through the above structure, the lifting, translation, and adjustment operations of the overall structure can be realized, which is beneficial for meeting the usage requirements of different situations.

[0079] like Figure 2 and Figure 3 As shown, the rotary lifting assembly 12 includes a support base plate 121, several screw jacks 122, several reversing shafts 123, a lifting servo motor 124, a rotation motor 125, a rotation drive gear 126, a master servo commutator 127, and several slave servo commutators 128. The screw jacks 122, the master servo commutator 127, and the slave servo commutators 128 are all conventional structures in the prior art, and are simply applied.

[0080] During assembly, the support base plate 121 is fixed to the lifting flanges of several screw jacks 122. The movement of the screw jacks 122 drives the support base plate 121 to rise and fall. The screw jacks 122 are respectively connected to several slave servo commutators 128 through reversing shafts 123. The slave servo commutators 128 are connected to the master servo commutator 127 through reversing shafts 123. The lifting servo motor 124 is connected to the master servo commutator 127 and is used for the lifting drive of the screw jacks 122. The rotary motor 125 is fixed on the support base plate 121, and the rotary drive gear 126 is fixed on the main shaft of the rotary motor 125. The rotary motor 125 is connected to the translation assembly 13 through the rotary drive gear 126 and is used for the rotation adjustment of the translation assembly 13.

[0081] Furthermore, in this embodiment, there are four screw jacks 122 and two slave servo commutators 128; the four screw jacks 122 are connected to the two slave servo commutators 128 via commutator shafts 123. The lifting servo motor 124, in conjunction with the master servo commutator 127 and the slave servo commutators 128, enables synchronous lifting of the screw jacks 122, ensuring the synchronicity and effectiveness of the lifting, thus achieving the overall lifting action of the translation component 13. Simultaneously, the rotational motor 125, in conjunction with the rotational drive gear 126, enables the overall rotational action of the translation component 13. The rotational motor 125 provides the power source, driving the rotational driven gear 133. Since the rotational driven gear 133 is fixed on the lower base plate 132, the overall rotational action of the translation component 13 can be achieved.

[0082] Furthermore, in practical applications, the edge of the support base plate 121 is also welded and fixed with a skirt to protect the internal structure, improve the overall aesthetics, reduce the number of operators required when docking the rocket engine with the test stand, and also solve the technical shortcomings of the rocket engine being difficult and time-consuming to assemble on a vertical test stand.

[0083] like Figure 4 and Figure 5 As shown, in this embodiment, the translation component 13 includes an upper top plate 131, a lower bottom plate 132, a rotary driven gear 133, a connecting shaft 134, and a translation drive structure 135. During assembly, the center of the lower bottom plate 132 is rotatably connected to the center of the top surface of the rotary lifting component 12 via the connecting shaft 134. The rotary driven gear 133 is fixed in the middle of the bottom surface of the lower bottom plate 132 and is concentrically arranged with the connecting shaft 134. The rotary driven gear 133 meshes with the rotary drive gear 126 to achieve rotary drive. The translation drive structure 135 is fixed on the top surface of the lower bottom plate 132, and the upper top plate 131 is connected to the translation drive structure 135. The translation drive structure 135 drives the upper top plate 131 to translate on the top surface of the lower bottom plate 132.

[0084] Meanwhile, the translation drive structure 135 includes a guide rail 1351, a slider 1352, a drive block 1353, a translation control motor 1354, and a translation ball screw 1355; the guide rail 1351 is fixed to the top surface of the lower base plate 132; the slider 1352 is translatably mounted on the guide rail 1351, the drive block 1353 is helically connected to the translation ball screw 1355, and both the slider 1352 and the drive block 1353 are fixedly connected to the bottom surface of the upper top plate 131; the translation control motor 1354 is fixed to the top surface of the lower base plate 132, and the translation ball screw 1355 is fixed to the main shaft of the translation control motor 1354 through a coupling.

[0085] In this embodiment, the diameter of the driven rotary gear 133 is larger than the diameter of the driven rotary gear 126, and the translational drive structure 135 converts rotational force into linear motion, realizing the linear translation of the upper top plate 131. Through the above structure, the effectiveness and stability of the translation can also be guaranteed. In practical applications, the edge of the lower bottom plate 132 is also welded and fixed with a skirt to protect the internal structure and improve the overall aesthetic appearance.

[0086] Furthermore, in practical applications, a plurality of universal balls 3 are evenly arranged along the bottom edge of the lower base plate 132; the bottom of the universal balls 3 are rolled onto the top surface of the supporting base plate 121. These universal balls 3 not only facilitate support and rotation, but also, through the aforementioned structure, ensure smooth rotation of the lower base plate 132 on the supporting base plate 121, guaranteeing the effectiveness and reliability of the rotation. Simultaneously, an oil-free bushing 4 is provided at the connection between the connecting shaft 134 and the supporting base plate 121 of the rotating lifting assembly 12. This oil-free bushing 4 is made of tin bronze, ensuring smooth and unobstructed rotation.

[0087] like Figure 6 , Figure 8 As shown, the walking assembly 11 includes a walking seat 111, a walking drive wheel assembly 112, a walking driven wheel assembly 113, and a connecting member 114; the walking seat 111 is provided with a through groove 5.

[0088] During assembly, the driving wheel assembly 112 and the driven wheel assembly 113 are both located on the top surface of the travel seat 111, and the driving wheel assembly 112 and the driven wheel assembly 113 are connected by a connector 114; the wheel edges of the driving wheel assembly 112 and the driven wheel assembly 113 pass through the through groove 5 and extend out of the bottom surface of the travel seat 111; the rotary lifting assembly 12 includes a plurality of screw jacks 122, the bottom end of which is fixed on the travel seat 111.

[0089] The driving drive wheel assembly 112 includes a wheel 1121, a driving drive motor 1122, a steering motor 1123, a driving main gear 1124, a driving transmission gear 1125, a steering gear 1126, a transmission chain 1127, a crank 1128, a sector gear 1129, a steering drive gear 11210, and a connecting rod 11211. The wheel 1121 is connected to the driving transmission gear 1125 through the crank 1128, and the driving drive motor 1122 meshes with the driving transmission gear 1125 through the driving main gear 1124.

[0090] The steering drive gear 11210 is fixed on the main shaft of the steering motor 1123. The transmission gear chain 1127 is connected between the steering drive gear 11210 and the steering gear 1126, and the steering gear 1126 meshes with the sector gear 1129. The sector gear 1129 is connected to the crank 1128. The steering drive gear 11210 drives the sector gear 1129 to rotate and realizes the steering adjustment of the crank 1128. The two ends of the connecting rod 11211 are connected between the two cranks 1128, so that the two cranks 1128 turn synchronously.

[0091] The above structure ensures the effectiveness and reliability of the walking drive, effectively realizes the transfer operation, and also enables effective steering adjustment and control. Both the main walking gear 1124 and the walking transmission gear 1125 are bevel gears.

[0092] like Figure 9 , Figure 10 As shown, the support leg structure 2 includes a large arm 21, a small arm 22, a lifting cylinder 23, and a telescopic cylinder 24. The small arm 22 is telescopically disposed within the telescopic cavities at both ends of the large arm 21, and the telescopic cylinder 24 is fixed between the telescopic cavities of the small arm 22 and the large arm 21. The rotating lifting assembly 12 includes a support base plate 121, the large arm 21 is fixed on the support base plate 121, and the lifting cylinder 23 is fixed at the end of the small arm 22 extending out of the support base plate 121 for adjusting the lifting of the support base plate 121. Guide rollers 6 are provided between the telescopic cavities of the small arm 22 and the large arm 21; and foot pads 7 are fixed to the bottom surface of the end of the small arm 22 extending out of the support base plate 121.

[0093] In this embodiment, the above structure allows for adjustment of different positions via the telescopic electric cylinder 24 to ensure the search for a suitable support point. It also allows for lifting adjustment via the lifting electric cylinder 23. There are four lifting electric cylinders 23, each set individually, meaning that the corresponding height can be set individually. In cases of uneven ground, this helps to ensure the parallelism of the mating surfaces between the engine and the test bench thrust frame, improving the accuracy and effectiveness of the assembly.

[0094] The above technical solution has the following beneficial effects:

[0095] 1. The structure of this utility model is reasonable. The cargo platform structure includes a walking component, a rotating lifting component, and a translating component. It can realize the rotation, transfer and translation of the cargo as needed. During assembly, the stability of the assembly can be improved by rotating and translating, which helps to reduce the number of operators when docking the rocket engine with the test stand. It also solves the technical shortcomings of the rocket engine assembly on the vertical test stand, which is difficult and time-consuming. It also helps to improve the efficiency of transfer and assembly.

[0096] 2. The rotary lifting assembly includes a support base plate, several screw jacks, several reversing shafts, a lifting servo motor, a rotary motor, a rotary drive gear, a main servo commutator, and several slave servo commutators. Through the above structure, the effectiveness and stability of the rotary lifting can be improved, and the vertical adjustment operation can be realized through the lifting servo motor to meet the assembly and use requirements of different situations.

[0097] 3. The translation assembly includes an upper top plate, a lower bottom plate, a rotary driven gear, a connecting shaft, and a translation drive structure; it helps improve the effectiveness and stability of translation, while also being easy to operate;

[0098] 4. The traveling assembly includes a traveling base, a traveling drive wheel assembly, a traveling driven wheel assembly, and connecting parts; the traveling assembly helps to ensure the effectiveness and stability of the entire structure's transport.

[0099] 5. The travel drive wheel assembly includes wheels, travel drive motor, steering motor, travel main gear, travel transmission gear, steering gear, transmission chain, crank, sector gear, steering drive gear and connecting rod; it can improve the reliability of travel drive and the effectiveness of steering adjustment, and meet the assembly requirements of different positions.

[0100] 6. The support leg structure includes a boom, a forearm, a lifting electric cylinder, and a telescopic electric cylinder; it can be adjusted as needed to meet the requirements of uneven ground conditions, ensuring the parallelism between the engine and the test bench thrust frame, and improving assembly efficiency and accuracy.

[0101] In the description of this utility model, it should be noted that the terms "upper," "lower," "inner," and "outer," etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. These terms are used only for the convenience of describing the utility model and for simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on the utility model. Furthermore, the terms "first," "second," or "third" are used for descriptive purposes only and should not be construed as indicating or implying relative importance.

[0102] Unless otherwise explicitly specified and limited, the terms "installation," "connection," and "joining" in this utility model should be interpreted broadly. For example, they can refer to fixed connections, detachable connections, or integrated connections; similarly, they can refer to mechanical connections, electrical connections, or direct connections, or indirect connections through an intermediate medium, or connections within several components. Those skilled in the art can understand the specific meaning of the above terms in this utility model based on the specific circumstances.

[0103] Although the present invention has been described with reference to preferred embodiments, various modifications can be made thereto and components can be replaced with equivalents without departing from the scope of the invention. In particular, the technical features mentioned in the various embodiments can be combined in any manner, provided there is no structural conflict. The present invention is not limited to the specific embodiments disclosed herein, but includes all technical solutions falling within the scope of the claims.

Claims

1. A universal adjustment platform for transporting and assembling rocket engines, characterized in that: It includes a cargo platform structure (1) and several support leg structures (2) set on the cargo platform structure (1); The cargo platform structure (1) includes a walking component (11), a rotating lifting component (12), and a translating component (13); The supporting leg structure (2) is disposed on the side of the walking assembly (11); The rotary lifting assembly (12) is located directly above the walking assembly (11) and is used for the rotary lifting adjustment drive of the translation assembly (13); The translation component (13) is positioned directly above the rotary lifting component (12) and is used for the translation adjustment drive of the rocket engine.

2. The rocket engine transfer and assembly integrated universal adjustment platform according to claim 1, characterized in that: The rotary lifting assembly (12) includes a support base plate (121), a plurality of screw jacks (122), a plurality of reversing shafts (123), a lifting servo motor (124), a rotation motor (125), a rotary drive gear (126), a master servo commutator (127), and a plurality of slave servo commutators (128). The supporting base plate (121) is fixed on the lifting flanges of a plurality of screw jacks (122), and the screw jacks (122) drive the supporting base plate (121) to rise and fall. Several of the aforementioned screw jacks (122) are respectively connected to several of the aforementioned slave servo commutators (128) via the reversing shaft (123); Several of the slave servo commutators (128) are connected to the master servo commutator (127) via the commutation shaft (123); The lifting servo motor (124) is connected to the main servo commutator (127) and is used for the lifting drive of the screw jack (122); The rotary motor (125) is fixed on the support base plate (121), and the rotary drive gear (126) is fixed on the main shaft of the rotary motor (125); The rotary motor (125) is connected to the translation assembly (13) via the rotary drive gear (126) and is used for the rotational adjustment of the translation assembly (13).

3. The rocket engine transfer and assembly integrated universal adjustment platform according to claim 2, characterized in that: The number of the screw jacks (122) is four, and the number of the slave commutators (128) is two; The four screw jacks (122) are connected to the two slave servo commutators (128) via the commutator shafts (123).

4. The rocket engine transfer and assembly integrated universal adjustment platform according to claim 2, characterized in that: The translation component (13) includes an upper top plate (131), a lower bottom plate (132), a rotary driven gear (133), a connecting shaft (134), and a translation drive structure (135); The center of the lower base plate (132) is rotatably connected to the center of the top surface of the rotary lifting assembly (12) via the connecting shaft (134); The driven gear (133) is fixed in the middle of the bottom surface of the lower base plate (132) and is concentrically arranged with the connecting shaft (134). The driven gear (133) meshes with the drive gear (126) to achieve rotational drive. The translation drive structure (135) is fixed to the top surface of the lower base plate (132), and the upper top plate (131) is connected to the translation drive structure (135); The translation drive structure (135) moves to cause the upper top plate (131) to translate on the top surface of the lower bottom plate (132).

5. The rocket engine transfer and assembly integrated universal adjustment platform according to claim 4, characterized in that: The translation drive structure (135) includes a guide rail (1351), a slider (1352), a drive block (1353), a translation control motor (1354), and a translation ball screw (1355); The guide rail (1351) is fixed to the top surface of the lower base plate (132); The slider (1352) can be translatably mounted on the guide rail (1351), the drive block (1353) is spirally connected to the translation ball screw (1355), and both the slider (1352) and the drive block (1353) are fixedly connected to the bottom surface of the upper top plate (131). The translation control motor (1354) is fixed on the top surface of the lower base plate (132), and the translation ball screw (1355) is fixed on the main shaft of the translation control motor (1354) by a coupling.

6. A universal adjustment platform for transporting and assembling rocket engines according to claim 4 or claim 5, characterized in that: A number of omnidirectional balls (3) are evenly arranged at the bottom edge of the lower base plate (132); The bottom of the omnidirectional ball (3) is rolled on the top surface of the support base plate (121).

7. The rocket engine transfer and assembly integrated universal adjustment platform according to claim 4, characterized in that: An oil-free bushing (4) is provided at the connection between the connecting shaft (134) and the rotary lifting assembly (12).

8. The integrated universal adjustment platform for transporting and assembling rocket engines according to claim 1, characterized in that: The walking assembly (11) includes a walking seat (111), a walking drive wheel assembly (112), a walking driven wheel assembly (113), and a connecting member (114); The walking seat (111) is provided with a through groove (5); The driving wheel assembly (112) and the driven wheel assembly (113) are both disposed on the top surface of the walking seat (111), and the driving wheel assembly (112) and the driven wheel assembly (113) are connected by the connector (114); The wheel edges of the driving wheel assembly (112) and the driven wheel assembly (113) pass through the through groove (5) and extend out of the bottom surface of the walking seat (111); The rotary lifting assembly (12) includes a plurality of screw jacks (122), the bottom end of which is fixed on the traveling seat (111).

9. A universal adjustment platform for transporting and assembling rocket engines according to claim 8, characterized in that: The walking drive wheel assembly (112) includes a wheel (1121), a walking drive motor (1122), a steering motor (1123), a walking main gear (1124), a walking transmission gear (1125), a steering gear (1126), a transmission chain (1127), a crank (1128), a sector gear (1129), a steering drive gear (11210), and a connecting rod (11211); The wheel (1121) is connected to the travel transmission gear (1125) via the crank (1128), and the travel drive motor (1122) meshes with the travel transmission gear (1125) via the travel main gear (1124); The steering drive gear (11210) is fixed on the main shaft of the steering motor (1123), the transmission gear chain (1127) is connected between the steering drive gear (11210) and the steering gear (1126), and the steering gear (1126) meshes with the sector gear (1129); The sector tooth (1129) is connected to the crank (1128), and the steering drive gear (11210) drives the sector tooth (1129) to rotate and realizes the steering adjustment of the crank (1128); The two ends of the connecting rod (11211) are connected between the two cranks (1128), so that the two cranks (1128) turn synchronously.

10. The integrated universal adjustment platform for transporting and assembling rocket engines according to claim 1, characterized in that: The support leg structure (2) includes a large arm (21), a small arm (22), a lifting electric cylinder (23), and a telescopic electric cylinder (24); The forearm (22) is telescopically disposed in the telescopic cavities at both ends of the upper arm (21), and the telescopic electric cylinder (24) is fixed between the telescopic cavities of the forearm (22) and the upper arm (21); The rotary lifting assembly (12) includes a support base plate (121), the upper arm (21) is fixed on the support base plate (121), and the lifting electric cylinder (23) is fixed at the end of the lower arm (22) extending out of the support base plate (121) for lifting and adjusting the support base plate (121).

11. A universal adjustment platform for transporting and assembling rocket engines according to claim 10, characterized in that: A guide roller (6) is provided between the telescopic cavity of the forearm (22) and the upper arm (21); a foot pad (7) is fixed to the bottom surface of the end of the forearm (22) that extends out of the support base plate (121).

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