Push-pull integrated tool and rocket fairing fixture

Abstract

The utility model relates to the field of rocket assembling equipment, and provides a push-pull integrated tool which comprises a fixing base, a tension assembly and a thrust assembly, the fixing base is suitable for being arranged on a fairing fixture, and the tension assembly and the thrust assembly are independently arranged on the fixing base. The pulling force assembly is used for being connected with a butt joint hole in the fairing and pulling the fairing, and the pushing force assembly is used for being connected with the outer wall of the fairing in an abutting mode and pushing the fairing. According to the fairing, the pulling force assembly and the pushing force assembly are integrally arranged and work independently, frequent replacement between the pulling force assembly and the pushing force assembly is not needed when the half fairing of the fairing is pushed or pulled, and the efficiency of adjusting the shape and posture of the half fairing is improved. The utility model further provides a rocket fairing fixture.

Description

Technical Field

[0001] This application relates to the field of rocket assembly equipment, and in particular to a push-pull integrated tooling and a rocket fairing frame. Background Technology

[0002] During rocket assembly, the fairing halves need to be fixed onto the fairing frame first. To mate the two halves, various docking fixtures mounted on the fairing frame are used to fine-tune the shape and attitude of the halves, allowing them to be assembled. In existing technology, fine-tuning the shape and attitude of the halves involves pushing or pulling the mating joint, repeatedly until the halves meet the requirements for assembly with the other halves. Currently, pushing and pulling the mating joint is done using two different sets of docking fixtures, which share a common support. At the same time, the same part of the half-mask is either pulled or pushed. When it is necessary to pull, the docking fixture that pulls outward is used, and when it is necessary to push, the docking fixture that pushes inward is used. However, the pushing and pulling operations are often carried out alternately, and it is necessary to frequently change the docking fixture that pulls outward and the docking fixture that pushes inward. This constant switching is both time-consuming and laborious, which greatly affects the efficiency of adjusting the shape and posture of the half-mask.

[0003] Besides the aforementioned drawbacks, the docking fixture also has some significant shortcomings. The half-cover has docking holes; when pulling the half-cover outwards, the docking fixture needs to be connected to these holes. However, issues with positioning accuracy during hole machining, installation accuracy during fixture installation, significant deformation of the half-cover due to its large size, and deformation of the fairing frame greatly increase the difficulty of connecting the docking fixture to the docking holes. This severely impacts the docking efficiency, consequently affecting the efficiency of half-cover shape and attitude adjustment. Utility Model Content

[0004] To address the aforementioned problems, this application provides a push-pull integrated tooling and a rocket fairing frame, featuring ingenious design and simple structure. By integrating the pulling and thrusting components, which operate independently, this application eliminates the need for frequent switching between the pulling and thrusting components when pushing or pulling the fairing half, thus improving the efficiency of adjusting the half's shape and attitude. The technical solution adopted in this application is as follows:

[0005] A push-pull integrated tooling includes: a fixed base, a pulling component, and a pushing component. The fixed base is adapted to be mounted on a fairing frame. The pulling component and the pushing component are respectively and independently and adjacently mounted on the fixed base. The pulling component is used to connect with the docking hole on the fairing and pull the fairing. The pushing component is used to abut against the outer wall of the fairing and push the fairing.

[0006] By integrating the tension and thrust components and allowing them to operate independently, the efficiency of adjusting the shape and attitude of the fairing half is improved, eliminating the need for frequent switching between the tension and thrust components when pushing or pulling the fairing half.

[0007] In some embodiments, the fixed base is provided with an arc-shaped groove; the tension assembly includes a pull rod and a first limiting slider, the first limiting slider being disposed in the groove and slidable along the groove, the first limiting slider being adapted to the groove; the first limiting slider is provided with a first waist-shaped hole, the length direction of the first waist-shaped hole being the same as the height direction of the fairing frame, the width of the first waist-shaped hole being adapted to the diameter of the pull rod; the pull rod is disposed in the first waist-shaped hole, one end of the pull rod being adapted to abut against the edge of the first waist-shaped hole, and the other end being adapted to connect with a docking hole on the fairing; the pull rod is adapted to move along the length direction of the first waist-shaped hole.

[0008] By setting up a sliding groove, a first limiting slider, and a first waist-shaped hole, the pull rod can not only move around the fairing circumferentially within a certain range along the sliding groove, but also move along the first waist-shaped hole in the height direction of the fairing. This increases the range of the fairing outer wall that the pull rod end can radiate. When there is a large deviation between the pull rod end and the docking hole on the fairing, the pull rod can be docked with the docking hole by adjusting the position of the pull rod. This allows the pull rod to adapt to the large positional deviation between itself and the docking hole, ensuring the docking efficiency between the pull rod and the docking hole.

[0009] In some embodiments, the fixed base is further provided with a first receiving groove, which is located on one side of the slide groove and communicates with the slide groove; the tension assembly further includes a second limiting slider, which is slidably disposed in the first receiving groove, the sliding direction of the second limiting slider is the same as the height direction of the fairing frame, the second limiting slider is provided with a second waist-shaped hole, the length direction of the second waist-shaped hole is perpendicular to the sliding direction of the second limiting slider, and the width of the second waist-shaped hole is adapted to the diameter of the pull rod; the rod body of the pull rod is disposed in the first waist-shaped hole and the second waist-shaped hole.

[0010] By setting the first receiving groove, the second limiting slider, and the second waist-shaped hole, the range of motion of the pull rod is limited, so that the axis of the pull rod is always perpendicular to the axis of the fairing or fairing frame, which facilitates the connection between the pull rod and the docking hole on the fairing.

[0011] In some embodiments, a first screw and a second screw are screwed onto the fixed base. The ends of the first screw and the second screw are inserted into the first receiving groove. The ends of the first screw and the second screw respectively abut against both sides of the sliding direction of the second limiting slider to position the second limiting slider at a preset position.

[0012] By setting a first screw and a second screw, the second limiting slider is fixed using the first and second screws. By screwing the first and second screws together, the position of the second limiting slider can be adjusted. When the second limiting slider is fixed in the preset position, it can provide support for the pull rod, reducing the labor intensity required when the pull rod is connected to the mating hole, and improving the connection efficiency between the pull rod and the mating hole.

[0013] In some embodiments, the fixed base is provided with a second receiving groove; the thrust assembly includes a push rod, a push seat and a third limiting slider, the third limiting slider is disposed in the second receiving groove, the rod body of the push rod is screwed to the third limiting slider, one end of the push rod is rotatably connected to the push seat through a ball joint, and the side of the push seat away from the push rod is adapted to abut against the outer wall of the fairing.

[0014] The ball joint connects the push rod and the push seat, allowing the push seat to rotate omnidirectionally relative to the push rod. This enables the push seat to better contact and transmit force with the outer wall of the fairing, conforming to the curvature of the fairing.

[0015] In some embodiments, the third limiting slider is slidably disposed in the second receiving groove, and the sliding direction of the third limiting slider is the same as the height direction of the fairing frame.

[0016] By sliding the third limiting slider in the second receiving groove, the push rod can be translated along the height direction of the fairing within a certain range, thus increasing the range of the fairing outer wall that the push base can radiate.

[0017] In some embodiments, a third screw and a fourth screw are screwed onto the fixed base. The ends of the third screw and the fourth screw are inserted into the second receiving groove. The ends of the third screw and the fourth screw respectively abut against both sides of the sliding direction of the third limiting slider to position the third limiting slider at a preset position.

[0018] By setting a third screw and a fourth screw, the third limiting slider is fixed using the third screw and the position of the third limiting slider can be adjusted by screwing the third screw and the fourth screw. When the third limiting slider is fixed in the preset position, it can provide support for the push rod, reducing the labor intensity of the push seat abutting against the designated position on the outer wall of the fairing, and helping to improve the efficiency of adjusting the shape and attitude of the half fairing.

[0019] In some embodiments, the ball-and-socket connector includes a ball socket, a ball head, a ball bearing, and a locking nut; one of the ball socket and the ball head is located at the end of the push base near the push rod, and the other is located at the end of the push rod near the push base; the end of the push base or the push rod with the ball socket has a plurality of accommodating holes spaced circumferentially; the locking nut has a driving inclined surface, the diameter of the locking nut is not smaller than that of the ball head, and the locking nut is screwed onto the end of the push base or the push rod with the ball socket. At one end, the ball bearing is arranged in the receiving hole and located in the hole of the locking nut; when the locking nut is tightened, causing the driving inclined surface to press the ball bearing, the part of the ball bearing exposed in the receiving hole will press the ball head in the ball socket and restrict the ball head in the ball socket, so as to realize the hinge between the push seat and the push rod; when the locking nut is tightened, causing the driving inclined surface to move away from the ball bearing, the ball bearing will release the restriction on the ball head, so that the push seat and the push rod can be separated.

[0020] In some embodiments, a limiting member is provided at the end of the push base or the push rod where the ball socket is located. This limiting member is used to restrict the locking nut at the end of the push base or the push rod where the ball socket is located, thereby preventing the locking nut from falling off. By providing the limiting member, the locking nut can be prevented from falling off.

[0021] In some embodiments, the limiting member is a retaining ring, and the end of the push base or the push rod with the ball socket is provided with a retaining groove, and the retaining ring is engaged in the retaining groove.

[0022] In some embodiments, a turning handle is provided at the end of the push rod away from the push base. The turning handle improves the ease of turning the push rod.

[0023] On the other hand, this application provides a rocket fairing frame, including a frame body and the aforementioned push-pull integrated tooling, wherein the push-pull integrated tooling is installed on the frame body.

[0024] The push-pull integrated tooling and rocket fairing bracket provided in this application have at least one of the following beneficial effects:

[0025] 1. The push-pull integrated tooling provided in this application integrates the pulling component and the thrust component, and the two work independently of each other. This eliminates the need to frequently switch between the pulling component and the thrust component when pushing or pulling the fairing half, thereby improving the efficiency of adjusting the shape and attitude of the half.

[0026] 2. The push-pull integrated tooling provided in this application, by setting a sliding groove, a first limiting slider, and a first waist-shaped hole, enables the pull rod to not only move around the fairing circumferentially within a certain range along the sliding groove, but also to move along the fairing height direction along the first waist-shaped hole. This increases the range of the fairing outer wall that the pull rod end can radiate. When there is a large deviation between the pull rod end and the docking hole on the fairing, the pull rod can be docked with the docking hole by adjusting the position of the pull rod. This allows the pull rod to adapt to the large positional deviation between itself and the docking hole, ensuring the docking efficiency between the pull rod and the docking hole.

[0027] 3. The push-pull integrated tooling provided in this application restricts the range of motion of the pull rod by setting a first receiving groove, a second limiting slider and a second waist-shaped hole, so that the axis of the pull rod is always perpendicular to the axis of the fairing or fairing frame, which is conducive to the docking of the pull rod with the docking hole on the fairing.

[0028] 4. This application provides a push-pull integrated tooling, which uses a first screw and a second screw to fix a second limiting slider. By screwing the first screw and the second screw, the position of the second limiting slider can be adjusted. When the second limiting slider is fixed in a preset position, it can provide support for the pull rod, reducing the labor intensity required when the pull rod is connected to the mating hole, and improving the connection efficiency between the pull rod and the mating hole.

[0029] 5. The push-pull integrated tooling provided in this application uses a ball joint to connect the push rod and the push seat, so that the push seat can rotate omnidirectionally relative to the push rod, enabling the push seat to better contact and transmit force with the outer wall of the fairing in accordance with the curvature direction of the fairing outer wall.

[0030] 6. The push-pull integrated tooling provided in this application allows the push rod to be slidably disposed in the second receiving groove by the third limiting slider, so that the push rod can be translated along the height direction of the fairing within a certain range, thereby increasing the range of the fairing outer wall that the push base can radiate.

[0031] 7. This application provides a push-pull integrated tooling, which uses a third screw and a fourth screw to fix a third limiting slider. By screwing the third screw and the fourth screw, the position of the third limiting slider can be adjusted. When the third limiting slider is fixed in the preset position, it can provide support for the push rod, reducing the labor intensity of the push seat abutting against the designated position on the outer wall of the fairing, and improving the efficiency of adjusting the shape and attitude of the half-fairing.

[0032] 8. The push-pull integrated tooling provided in this application can prevent the locking nut from falling off by setting a limiting component.

[0033] 9. The push-pull integrated tooling provided in this application improves the convenience of turning the push rod by setting a turning handle. Attached Figure Description

[0034] The preferred embodiments will be described below in a clear and easy-to-understand manner, with reference to the accompanying drawings, to further explain the above-mentioned characteristics, technical features, advantages, and implementation methods of a push-pull integrated tooling and rocket fairing frame:

[0035] Figure 1 This is a schematic diagram of the push-pull integrated tooling installed on the fairing frame;

[0036] Figure 2 yes Figure 1 An enlarged view of part A in the embodiment;

[0037] Figure 3 This is a schematic diagram of the overall structure of an embodiment of the push-pull integrated tooling;

[0038] Figure 4 yes Figure 3 Another perspective on the embodiments;

[0039] Figure 5 yes Figure 3 Another perspective on the embodiments;

[0040] Figure 6 yes Figure 3 Top view of the embodiment;

[0041] Figure 7 yes Figure 3 Cross-sectional view of the embodiment;

[0042] Figure 8 This is a structural diagram of the tension component and the thrust component;

[0043] Figure 9 yes Figure 8 Another perspective on the embodiments;

[0044] Figure 10 This is a structural diagram of the push rod and push base;

[0045] Figure 11 yes Figure 10 Exploded view of the embodiment;

[0046] Figure 12 This is a structural schematic diagram of one embodiment of the fixing base;

[0047] Figure 13 yes Figure 12 Another perspective on the implementation.

[0048] Explanation of icon numbers:

[0049] 1. Fairing frame; 2. Push-pull integrated tooling; 3. Fixed seat; 4. Slide groove; 5. Pull rod; 6. First limiting slider; 7. First oblong hole; 8. First receiving groove; 9. Second limiting slider; 10. Second oblong hole; 11. First screw; 12. Second receiving groove; 13. Push rod; 14. Push seat; 15. Third limiting slider; 16. Third screw; 17. Fourth screw; 18. Ball socket; 19. Ball head; 20. Ball bearing; 21. Locking nut; 22. Receiving hole; 23. Limiting component; 24. Tightening handle; 25. Detailed Implementation

[0050] To more clearly illustrate the technical solutions in the embodiments of this application or the prior art, the specific implementation methods of this application will be described below with reference to the accompanying drawings. Obviously, the accompanying drawings described below are only some embodiments of this application. For those skilled in the art, other drawings and other implementation methods can be obtained based on these drawings without creative effort.

[0051] To keep the drawings concise, each drawing only schematically shows the parts relevant to this application, and they do not represent the actual structure of the product. Furthermore, for ease of understanding, in some drawings, only one of the components with the same structure or function is schematically shown, or only one is labeled. In this document, "one" not only means "only one," but can also mean "more than one."

[0052] It should also be further understood that the term “and / or” as used in this application specification and the appended claims means any combination of one or more of the associated listed items and all possible combinations, and includes such combinations.

[0053] In this document, it should be noted that, unless otherwise explicitly specified and limited, the terms "installation," "connection," and "linking" should be interpreted broadly. For example, they can refer to fixed connections, detachable connections, or integral connections; they can refer to mechanical connections or electrical connections; they can refer to direct connections or indirect connections through an intermediate medium; and they can refer to the internal connection between two components. Those skilled in the art can understand the specific meaning of the above terms in this application based on the specific circumstances.

[0054] Furthermore, in the description of this application, the terms "first," "second," etc., are used only to distinguish descriptions and should not be construed as indicating or implying relative importance.

[0055] refer to Figures 1-13This application provides a push-pull integrated tooling, including: a fixed base 3, a pulling component and a pushing component. The fixed base 3 is adapted to be mounted on the fairing frame 1. The pulling component and the pushing component are respectively and independently and adjacently mounted on the fixed base 3. The pulling component is used to connect with the docking hole on the fairing and pull the fairing. The pushing component is used to abut against the outer wall of the fairing and push the fairing.

[0056] Understandably, by integrating the tension and thrust components and allowing them to work independently, the efficiency of adjusting the shape and attitude of the fairing half is improved, eliminating the need for frequent switching between the tension and thrust components when pushing or pulling the fairing half.

[0057] refer to Figures 2-5 , Figures 7-13 In one embodiment, the fixed base 3 is provided with an arc-shaped groove 4; the tension assembly includes a pull rod 5 and a first limiting slider 6. The first limiting slider 6 is disposed in the groove 4 and can slide along the groove 4. The first limiting slider 6 is adapted to the groove 4; the first limiting slider 6 is provided with a first waist-shaped hole 7. The length direction of the first waist-shaped hole 7 is the same as the height direction of the fairing frame 1, and the width of the first waist-shaped hole 7 is adapted to the diameter of the pull rod 5; the rod of the pull rod 5 is disposed in the first waist-shaped hole 7. One end of the pull rod 5 is adapted to abut against the edge of the first waist-shaped hole 7, and the other end is adapted to connect with the docking hole on the fairing; the pull rod 5 is adapted to move in the first waist-shaped hole 7 along the length direction of the first waist-shaped hole 7.

[0058] It is easy to understand that by setting the slide groove 4, the first limiting slider 6, and the first waist-shaped hole 7, the pull rod 5 can not only move around the fairing circumferentially within a certain range along the slide groove 4, but also move along the first waist-shaped hole 7 in the height direction of the fairing. This increases the range of the fairing outer wall that the end of the pull rod 5 can radiate. When there is a large deviation between the end of the pull rod 5 and the docking hole on the fairing, the pull rod 5 can be docked with the docking hole by adjusting the position of the pull rod 5. This allows the pull rod 5 to adapt to the large positional deviation between itself and the docking hole, ensuring the docking efficiency of the pull rod 5 and the docking hole.

[0059] refer to Figures 2-5 , Figures 7-13In one embodiment, the fixed base 3 is further provided with a first receiving groove 8, which is located on one side of the slide groove 4 and communicates with the slide groove 4; the tension assembly also includes a second limiting slider 9, which is slidably disposed in the first receiving groove 8. The sliding direction of the second limiting slider 9 is the same as the height direction of the fairing frame 1. The second limiting slider 9 is provided with a second waist-shaped hole 10, the length direction of the second waist-shaped hole 10 is perpendicular to the sliding direction of the second limiting slider 9, and the width of the second waist-shaped hole 10 is adapted to the diameter of the rod body of the pull rod 5; the rod body of the pull rod 5 is disposed in the first waist-shaped hole 7 and the second waist-shaped hole 10.

[0060] It is worth noting that by setting the first receiving groove 8, the second limiting slider 9, and the second waist-shaped hole 10, the range of motion of the pull rod 5 is limited, so that the axis of the pull rod 5 is always perpendicular to the axis of the fairing or fairing frame 1, which is conducive to the connection between the pull rod 5 and the docking hole on the fairing.

[0061] refer to Figures 2-5 , Figures 7-13 In one embodiment, a first screw 11 and a second screw 12 are screwed onto the fixed base 3. The ends of the first screw 11 and the second screw 12 are inserted into the first receiving groove 8. The ends of the first screw 11 and the second screw 12 respectively abut against the two sides of the sliding direction of the second limiting slider 9 to position the second limiting slider 9 at a preset position.

[0062] Understandably, by setting the first screw 11 and the second screw 12, the second limiting slider 9 is fixed using the first screw 11 and the second screw 12. By turning the first screw 11 and the second screw 12, the position of the second limiting slider 9 can be adjusted. When the second limiting slider 9 is fixed in the preset position, it can provide support for the pull rod 5, reducing the labor intensity required when the pull rod 5 is connected to the docking hole, and improving the docking efficiency of the pull rod 5 and the docking hole.

[0063] refer to Figures 2-13 In one embodiment, the fixed base 3 is provided with a second receiving groove 13; the thrust assembly includes a push rod 14, a push seat 15, and a third limiting slider 16. The third limiting slider 16 is disposed in the second receiving groove 13. The rod body of the push rod 14 is screwed to the third limiting slider 16. One end of the push rod 14 is rotatably connected to the push seat 15 through a ball joint 19 and ball head 20. The side of the push seat 15 away from the push rod 14 is adapted to abut against the outer wall of the fairing. By using the ball joint 19 and ball head 20 to connect the push rod 14 and the push seat 15, the push seat 15 can rotate omnidirectionally relative to the push rod 14, enabling the push seat 15 to better abut against and transmit force to the outer wall of the fairing in accordance with the curvature direction of the outer wall.

[0064] refer to Figures 2-13In one embodiment, the third limiting slider 16 is slidably disposed in the second receiving groove 13, and the sliding direction of the third limiting slider 16 is the same as the height direction of the fairing frame 1. By slidably disposing the third limiting slider 16 in the second receiving groove 13, the push rod 14 can be translated along the height direction of the fairing within a certain range, thereby increasing the range of the outer wall of the fairing that the push base 15 can radiate.

[0065] refer to Figures 2-13 In one embodiment, a third screw 17 and a fourth screw 18 are screwed onto the fixed base 3. The ends of the third screw 17 and the fourth screw 18 are inserted into the second receiving groove 13. The ends of the third screw 17 and the fourth screw 18 respectively abut against the two sides of the sliding direction of the third limiting slider 16 to position the third limiting slider 16 at a preset position.

[0066] It is worth noting that by setting the third screw 17 and the fourth screw 18, the third limiting slider 16 is fixed using the third screw 17 and the fourth screw 18. By turning the third screw 17 and the fourth screw 18, the position of the third limiting slider 16 can be adjusted. When the third limiting slider 16 is fixed in the preset position, it can provide support for the push rod 14, reducing the labor intensity of the push seat 15 abutting against the designated position on the outer wall of the fairing, and helping to improve the efficiency of adjusting the shape and attitude of the half fairing.

[0067] refer to Figures 7-11 In one embodiment, the ball-and-socket connector includes a ball socket 19, a ball head 20, a ball bearing 21, and a locking nut 22. One of the ball socket 19 and the ball head 20 is located at the end of the push base 15 near the push rod 14, and the other is located at the end of the push rod 14 near the push base 15. The end of the push base 15 or push rod 14 with the ball socket 19 has a plurality of accommodating holes 23 spaced circumferentially. The locking nut 22 has a driving ramp inside, and the diameter of the hole in the locking nut 22 is not less than that of the ball head 20. The locking nut 22 is screwed onto the end of the push base 15 or push rod 14 with the ball socket 19. At one end of the ball socket 19, the ball 21 is arranged in the receiving hole 23 and located in the hole of the locking nut 22. When the locking nut 22 is tightened, the driving ramp presses the ball 21, and the part of the ball 21 exposed in the receiving hole 23 will press the ball head 20 in the ball socket 19 and restrict the ball head 20 in the ball socket 19, so as to realize the hinge between the push seat 15 and the push rod 14. When the locking nut 22 is tightened, the driving ramp moves away from the ball 21, and the ball 21 releases the restriction on the ball head 20, so that the push seat 15 and the push rod 14 can be separated.

[0068] refer to Figure 10 , Figure 11In one embodiment, a limiting member 24 is provided at the end of the push base 15 or push rod 14 where the ball socket 19 is located. The limiting member 24 is used to restrict the locking nut 22 to the end of the push base 15 or push rod 14 where the ball socket 19 is located, so as to prevent the locking nut 22 from falling off from the end of the push base 15 or push rod 14 where the ball socket 19 is located. By providing the limiting member 24, the locking nut 22 can be prevented from falling off.

[0069] refer to Figure 10 , Figure 11 In one embodiment, the limiting member 24 is a retaining ring, and the end of the push seat 15 or push rod 14 with the ball socket 19 is provided with a retaining groove, and the retaining ring is engaged in the retaining groove.

[0070] refer to Figure 5 , Figures 8-11 In one embodiment, the end of the push rod 14 away from the push base 15 is provided with a turning handle 25. By providing the turning handle 25, the convenience of turning the push rod 14 is improved.

[0071] On the other hand, reference Figure 1 This application provides a rocket fairing fixture, including a fixture body and the aforementioned push-pull integrated fixture 2, which is mounted on the fixture body. The specific structure of the push-pull integrated fixture 2 is as described in the aforementioned embodiment. Since this rocket fairing fixture adopts the technical solution of the aforementioned embodiment, it at least has the beneficial effects brought by the technical solution of the aforementioned embodiment, which will not be elaborated here.

[0072] It should be noted that the above embodiments can be freely combined as needed. The above are merely preferred embodiments of this application. It should be pointed out that for those skilled in the art, several improvements and modifications can be made without departing from the principles of this application, and these improvements and modifications should also be considered within the scope of protection of this application.

Claims

1. A push-pull integrated tooling characterized by, The utility model relates to a kind of integrated tool of push-pull, including: fixed seat, tension component and thrust component, the fixed seat is suitable for being arranged on fairing rack, the tension component and the thrust component are independently and adjacently arranged on the fixed seat respectively, the tension component is connected with the fairing on the interface hole and is pulled to the fairing, and the thrust component is abutted with the fairing outer wall and is pushed to the fairing.

2. The integrated tool of push-pull according to claim 1, wherein the fixed seat is provided with an arc-shaped sliding groove. The tension component includes a pull rod, a first limiting sliding block, the first limiting sliding block is arranged in the sliding groove and can slide along the sliding groove, and the first limiting sliding block is matched with the sliding groove. The first limiting sliding block is provided with a first waist-shaped hole, the length direction of the first waist-shaped hole is the same as the height direction of the fairing rack, the width of the first waist-shaped hole is matched with the diameter of the rod body of the pull rod, the rod body of the pull rod is arranged in the first waist-shaped hole, one end of the pull rod is matched with the edge of the first waist-shaped hole, and the other end is matched with the interface hole on the fairing. The pull rod is matched to move in the first waist-shaped hole along the length direction of the first waist-shaped hole.

3. The integrated tool of push-pull according to claim 2, wherein the fixed seat is further provided with a first accommodating groove, the first accommodating groove is located on one side of the sliding groove, and the first accommodating groove is communicated with the sliding groove. The tension component further includes a second limiting sliding block, the second limiting sliding block is arranged in the first accommodating groove and can slide, the slide direction of the second limiting sliding block is the same as the height direction of the fairing rack, the second limiting sliding block is provided with a second waist-shaped hole, the length direction of the second waist-shaped hole is perpendicular to the slide direction of the second limiting sliding block, and the width of the second waist-shaped hole is matched with the diameter of the rod body of the pull rod. The rod body of the pull rod is arranged in the first waist-shaped hole and the second waist-shaped hole.

4. The integrated tool of push-pull according to claim 3, wherein the fixed seat is further screwed with a first screw rod and a second screw rod, the ends of the first screw rod and the second screw rod are arranged in the first accommodating groove, and the ends of the first screw rod and the second screw rod are respectively matched with the two sides of the slide direction of the second limiting sliding block to position the second limiting sliding block at a predetermined position.

5. The integrated tool of push-pull according to any one of claims 1-4, wherein the fixed seat is provided with a second accommodating groove. The thrust component includes a push rod, a push seat and a third limiting sliding block, the third limiting sliding block is arranged in the second accommodating groove, the rod body of the push rod is screwed with the third limiting sliding block, one end of the push rod is rotatably connected with the push seat through a ball-and-socket joint pair, and the side, away from the push rod, of the push seat is matched with the fairing outer wall. The third limiting sliding block is arranged in the second accommodating groove and can slide, and the slide direction of the third limiting sliding block is the same as the height direction of the fairing rack. ​ 6. The push-pull integrated tooling of claim 5, wherein, ​ 7. The push-pull integrated tooling of claim 6, wherein, The third screw rod and the fourth screw rod are screwed on the fixing seat, the ends of the third screw rod and the fourth screw rod are inserted into the second accommodating groove, and the ends of the third screw rod and the fourth screw rod abut against two sides of the slidable direction of the third limiting sliding block, so that the third limiting sliding block is positioned at a preset position.

8. The push-pull integrated tooling of claim 7, wherein, The ball-and-socket joint comprises a ball socket, a ball head, a ball and a locking nut; one of the ball socket and the ball head is arranged at one end of the push rod close to the push seat, and the other is arranged at one end of the push seat close to the push rod; the end of the push seat or the push rod provided with the ball socket is circumferentially spaced apart and provided with a plurality of accommodating holes; the locking nut is internally provided with a driving slope, the hole diameter of the locking nut is not less than the ball head, the locking nut is screwed at the end of the push seat or the push rod provided with the ball socket, and the ball is arranged in the accommodating hole and located in the hole of the locking nut; when the locking nut is screwed, the driving slope extrudes the ball, the part of the ball exposed from the accommodating hole extrudes the ball head in the ball socket and limits the ball head in the ball socket, so that the push seat and the push rod are hinged; when the locking nut is screwed, the driving slope is away from the ball, the ball releases the limitation on the ball head, so that the push seat and the push rod can be separated.

9. The push-pull integrated tooling of claim 8, wherein, The end of the push seat or the push rod provided with the ball socket is provided with a limiting piece, the limiting piece is used for limiting the locking nut at the end of the push seat or the push rod provided with the ball socket, so as to prevent the locking nut from falling off from the end of the push seat or the push rod provided with the ball socket.

10. A rocket fairing jig, characterized by, The mold frame body and the push-pull integrated tool are included, and the push-pull integrated tool is mounted on the mold frame body.

Images