A rocket secondary bundling mechanism

Abstract

The present invention provides a rocket auxiliary bundling mechanism. The rocket auxiliary bundling mechanism includes: a first support, a first adjusting wedge, a second adjusting wedge, and a second support; wherein, the first end face of the first support is fixedly connected to the core stage rocket, a first fixing plate and a second fixing plate are arranged on the second end face of the first support, and the first fixing plate and the second fixing plate are arranged opposite to each other; both the first adjusting wedge and the second adjusting wedge are slidably connected to the second end face of the first support and are both arranged between the first fixing plate and the second fixing plate; the first end face of the second support is fixedly connected to the booster, and a first sliding part and a second sliding part are arranged on the second end face of the second support; the first sliding part and the second sliding part are arranged opposite to each other on the second end face of the second support, and the first sliding part and the second sliding part are fixed between the first adjusting wedge and the second adjusting wedge. The solution of the present invention realizes the automatic adjustment of the displacement difference generated axially between the booster and the core stage rocket.

Description

Technical Field

[0001] The present invention relates to the technical field of rocket bundling, and particularly to a rocket secondary bundling mechanism. Background Art

[0002] The secondary bundling mechanism is used for connecting the rocket booster to the central part of the core stage rocket. Its main functions are not only to bear the additional torque generated by the booster on the core stage rocket, to adapt to the deviation of the core stage relative to the booster caused by the expansion of the engine during rocket flight, and to achieve the function of release and disconnection when the booster separates. The requirements for the secondary bundling mechanism are easy installation, the ability to supplement and adjust the deviation during flight, and rapid installation and release and disconnection. The traditional secondary bundling mechanism uses pyrotechnics for unlocking, which not only increases the weight of the rocket, but also reduces safety, and cannot adjust the displacement difference generated axially between the booster and the core stage rocket during flight. Summary of the Invention

[0003] The present invention provides a rocket secondary bundling mechanism, which solves the problems of the complex structure, low safety and inability to adjust the displacement difference generated axially between the booster and the core stage rocket during flight of the traditional secondary bundling mechanism.

[0004] To solve the above technical problems, the technical solution of the present invention is as follows:

[0005] An embodiment of the present invention provides a rocket secondary bundling mechanism, including:

[0006] A first support, a first adjusting wedge, a second adjusting wedge and a second support;

[0007] Wherein, the first end face of the first support is fixedly connected to the core stage rocket, and a first fixing plate and a second fixing plate are arranged on the second end face of the first support, and the first fixing plate and the second fixing plate are arranged oppositely;

[0008] Both the first adjusting wedge and the second adjusting wedge are slidably connected to the second end face of the first support, and are both arranged between the first fixing plate and the second fixing plate;

[0009] The first end face of the second support is fixedly connected to the booster, and a first sliding part and a second sliding part are arranged on the second end face of the second support;

[0010] The first end of the first sliding part and the first end of the second sliding part are both fixedly connected to the second end face of the second support, and are oppositely arranged on the second end face of the second support. The second end of the first sliding part and the second end of the second sliding part are both arranged between the first adjusting wedge and the second adjusting wedge;

[0011] The first fixing plate is provided with first bolt holes, and a first bolt passes through the first bolt holes to contact the first adjusting wedge block and push the first adjusting wedge block to press against the first sliding part;

[0012] The second fixing plate is provided with second bolt holes, and a second bolt passes through the second bolt holes to contact the second adjusting wedge block and push the second adjusting wedge block to press against the second sliding part.

[0013] Optionally, a dovetail groove is provided on the second end face of the first support, and the dovetail groove is arranged between the first fixing plate and the second fixing plate;

[0014] Both the first adjusting wedge block and the second adjusting wedge block are clamped on the dovetail groove and are slidably connected to the dovetail groove.

[0015] Optionally, the rocket secondary bundling mechanism further includes:

[0016] A first groove provided on the first fixing plate, at least one first through hole is provided in the first groove, and the first bolt hole is arranged in the first groove;

[0017] At least one second through hole provided on the first adjusting wedge block and corresponding to the first through hole;

[0018] At least one first guide rod, the first end of the first guide rod passes through the first through hole and the second through hole, and the second end of the first guide rod is fixed in the first groove;

[0019] A first cover plate, the first cover plate covers the first groove and is fixedly connected to the first groove;

[0020] A fifth through hole corresponding to the first bolt hole is provided on the first cover plate.

[0021] Optionally, the rocket secondary bundling mechanism further includes:

[0022] A second groove provided on the second fixing plate, at least one third through hole is provided in the second groove, and the second bolt hole is arranged in the second groove;

[0023] At least one fourth through hole provided on the second adjusting wedge block and corresponding to the third through hole;

[0024] At least one second guide rod, the first end of the second guide rod passes through the third through hole and the fourth through hole, and the second end of the second guide rod is fixed in the second groove;

[0025] A second cover plate, the second cover plate covers the second groove and is fixedly connected to the second groove;

[0026] A sixth through-hole corresponding to the second bolt hole is provided on the second cover plate.

[0027] Optionally, the first sliding portion includes: a first fixing block, a first movable block, a first limiting plate, at least one third guiding rod, and a first rectangular spring sleeved on the first end of the third guiding rod;

[0028] Wherein, the first end of the first fixing block is fixed on the second end face of the second support, and at least one first circular groove is provided on the end face of the second end of the first fixing block;

[0029] The first end of the third guiding rod is fixed in the first circular groove, and the second end of the third guiding rod is fixedly connected to the first limiting plate;

[0030] The first movable block is sleeved on the second end of the third guiding rod and is located between the first limiting plate and the first rectangular spring;

[0031] The first movable block is slidably connected to the third guiding rod, and the side surface of the first movable block is in contact connection with the first adjusting wedge block.

[0032] Optionally, the second sliding portion includes: a second fixing block, a second movable block, a second limiting plate, at least one fourth guiding rod, and a second rectangular spring sleeved on the first end of the fourth guiding rod;

[0033] Wherein, the first end of the second fixing block is fixed on the second end face of the second support, and at least one second circular groove is provided on the end face of the second end of the second fixing block;

[0034] The first end of the fourth guiding rod is fixed in the second circular groove, and the second end of the fourth guiding rod is fixedly connected to the second limiting plate;

[0035] The second movable block is sleeved on the second end of the fourth guiding rod and is located between the second limiting plate and the second rectangular spring;

[0036] The second movable block is slidably connected to the fourth guiding rod, and the side surface of the second movable block is in contact connection with the second adjusting wedge block.

[0037] Optionally, the contact surfaces of the first adjusting wedge block and the first sliding portion are both inclined surfaces;

[0038] The contact surfaces of the second adjusting wedge block and the second sliding portion are both inclined surfaces.

[0039] Optionally, the length of the end face of the first sliding part in contact with the first adjusting wedge is greater than the length of the end face of the first adjusting wedge in contact with the first sliding part;

[0040] The length of the end face of the second sliding part in contact with the second adjusting wedge is greater than the length of the end face of the second adjusting wedge in contact with the second sliding part.

[0041] Optionally, the first end face of the first support is an arc structure, and the first end face of the first support is fixedly connected to the core stage rocket through at least two third bolts.

[0042] Optionally, the first end face of the second support is an arc structure, and the first end face of the second support is fixedly connected to the booster through at least three fourth bolts.

[0043] The above solution of the present invention has at least the following beneficial effects:

[0044] The rocket auxiliary bundling mechanism of the present invention includes: a first support, a first adjusting wedge, a second adjusting wedge, and a second support; wherein, the first end face of the first support is fixedly connected to the core stage rocket, and a first fixing plate and a second fixing plate are arranged on the second end face of the first support, and the first fixing plate and the second fixing plate are arranged opposite to each other; both the first adjusting wedge and the second adjusting wedge are slidably connected to the second end face of the first support, and are both arranged between the first fixing plate and the second fixing plate; the first end face of the second support is fixedly connected to the booster, and a first sliding part and a second sliding part are arranged on the second end face of the second support; the first sliding part and the second sliding part are relatively arranged on the second end face of the second support, and the first sliding part and the second sliding part are fixed between the first adjusting wedge and the second adjusting wedge. The automatic adjustment function of the displacement difference generated axially between the booster and the core stage rocket during the flight process is realized. At the same time, the safety of the auxiliary bundling mechanism is improved, and it also has the advantages of simple structure, small mass, and convenient installation. Description of the Drawings

[0045] Figure 1 is a perspective view of the rocket auxiliary bundling mechanism of the present invention;

[0046] Figure 2 is an exploded structural schematic diagram of the rocket auxiliary bundling mechanism of the present invention;

[0047] Figure 3 is an assembly schematic diagram of the rocket auxiliary bundling mechanism of the present invention;

[0048] Figure 4 is a sectional view after assembly of the rocket auxiliary bundling mechanism of the present invention;

[0049] Figure 5 is a side view of the rocket auxiliary bundling mechanism of the present invention;

[0050] Figure 6 is a schematic structural view of the dovetail groove of the rocket auxiliary bundling mechanism of the present invention;

[0051] Figure 7 is a top view of the rocket auxiliary bundling mechanism of the present invention.

[0052] Explanation of reference numerals:

[0053] 1. First support; 11. First fixing plate; 111. First bolt; 12. Second fixing plate; 121. Second bolt; 13. Dovetail groove; 14. Third bolt; 21. First adjusting wedge; 211. First guide rod; 212. First cover plate; 22. Second adjusting wedge; 221. Second guide rod; 222. Second cover plate; 3. Second support; 31. Fourth bolt; 311. First fixing block; 312. First movable block; 313. First limiting plate; 314. Third guide rod; 315. First rectangular spring; 321. Second fixing block; 322. Second movable block; 323. Second limiting plate; 324. Fourth guide rod; 325. Second rectangular spring; 4. Core stage rocket; 5. Booster; 61. First hexagon socket head screw; 62. Second hexagon socket head screw; 7. Bundling link; 71. First screw; 72. Second screw; 81. First hexagon socket head shoulder screw; 82. Second hexagon socket head shoulder screw. Detailed implementation manners

[0054] Hereinafter, exemplary embodiments of the present disclosure will be described in more detail with reference to the drawings. Although the exemplary embodiments of the present disclosure are shown in the drawings, it should be understood that the present disclosure can be implemented in various forms and should not be limited by the embodiments set forth herein. On the contrary, these embodiments are provided so that the present disclosure can be more thoroughly understood and the scope of the present disclosure can be completely conveyed to those skilled in the art.

[0055] As Figures 1 to 6 shown, an embodiment of the present invention provides a rocket auxiliary bundling mechanism, including:

[0056] a first support 1, a first adjusting wedge 21, a second adjusting wedge 22, and a second support 3;

[0057] wherein, a first end face of the first support 1 is fixedly connected to a core stage rocket 4, a first fixing plate 11 and a second fixing plate 12 are arranged on a second end face of the first support 1, and the first fixing plate 11 and the second fixing plate 12 are arranged opposite to each other;

[0058] both the first adjusting wedge 21 and the second adjusting wedge 22 are slidably connected to the second end face of the first support 1, and are both arranged between the first fixing plate 11 and the second fixing plate 12;

[0059] The first end face of the second support 3 is fixedly connected to the booster 5, and a first sliding part and a second sliding part are provided on the second end face of the second support 3;

[0060] The first ends of the first sliding part and the second sliding part are both fixedly connected to the second end face of the second support 3 and are oppositely arranged on the second end face of the second support 3. The second ends of the first sliding part and the second sliding part are both arranged between the first adjusting wedge 21 and the second adjusting wedge 22;

[0061] The first fixing plate 11 is provided with a first bolt hole. The first bolt 111 passes through the first bolt hole and contacts the first adjusting wedge 21, and pushes the first adjusting wedge 21 to press the first sliding part;

[0062] The second fixing plate 12 is provided with a second bolt hole. The second bolt 121 passes through the second bolt hole and contacts the second adjusting wedge 22, and pushes the second adjusting wedge 22 to press the second sliding part.

[0063] In this embodiment, the first adjusting wedge 21 can extrude the first sliding part by adjusting the supply amount of the first bolt 111, and the second adjusting wedge 22 can extrude the second sliding part by adjusting the supply amount of the second bolt 121; after the first adjusting wedge 21 and the second adjusting wedge 22 clamp the first sliding part and the second sliding part through the first bolt 111 and the second bolt 121, under the action of the frictional force between the adjusting wedge and the sliding part, the fixed connection between the first support 1 and the second support 3 can be realized; meanwhile, during installation, the assembly error can also be adjusted by adjusting the positions of the sliding part and the adjusting wedge;

[0064] During the flight, when due to the vibration and moment of the core stage rocket engine, a displacement difference in the X-axis direction is generated between the core stage rocket 4 and the booster 5, the displacement difference generated by the vibration can be eliminated through the up and down relative sliding in the X-axis direction between the adjusting wedge and the sliding part, so as to realize the automatic adjustment function of the X-axis displacement difference during the flight; wherein, the X-axis direction is parallel to the direction of the core stage rocket 4, that is, the direction from the tail of the core stage rocket 4 to the head of the core stage rocket 4; the adjustment amount of the X-axis displacement difference is the difference between the length of the adjusting wedge and the length of the sliding part, that is Figure 5 the H in Figure 5 where X is the direction from the tail of the core stage rocket 4 to the head of the core stage rocket 4;

[0065] Meanwhile, since the adjusting wedge block and the sliding part are slidably connected, when the bundling link 7 is unlocked and released, under the self-weight of the booster 5, the sliding part can directly disengage from the clamping of the adjusting wedge block, enabling the sub-bundling mechanism to achieve the function of automatic disconnection.

[0066] As Figure 6 shown, in an optional embodiment of the present invention, a dovetail groove 13 is provided on the second end face of the first support 1, and the dovetail groove 13 is arranged between the first fixing plate 11 and the second fixing plate 12;

[0067] Both the first adjusting wedge block 21 and the second adjusting wedge block 22 are clamped on the dovetail groove 13 and are slidably connected to the dovetail groove 13. The first adjusting wedge block 21 and the second adjusting wedge block 22 can freely slide on the first support 1 through the dovetail groove 13.

[0068] In an optional embodiment of the present invention, the rocket sub-bundling mechanism further includes:

[0069] A first groove provided on the first fixing plate 11, at least one first through hole is provided in the first groove, and the first bolt hole is arranged in the first groove;

[0070] At least one second through hole provided on the first adjusting wedge block 21 and corresponding to the first through hole;

[0071] At least one first guide rod 211, the first end of the first guide rod 211 passes through the first through hole and the second through hole, and the second end of the first guide rod 211 is fixed in the first groove;

[0072] A first cover plate 212, the first cover plate 212 covers the first groove and is fixedly connected to the first groove;

[0073] A fifth through hole corresponding to the first bolt hole is provided on the first cover plate 212.

[0074] The rocket sub-bundling mechanism further includes:

[0075] A second groove provided on the second fixing plate 12, at least one third through hole is provided in the second groove, and the second bolt hole is arranged in the second groove;

[0076] At least one fourth through hole provided on the second adjusting wedge block 22 and corresponding to the third through hole;

[0077] At least one second guiding rod 221, the first end of the second guiding rod 221 passes through the third through hole and the fourth through hole, and the second end of the second guiding rod 221 is fixed in the second groove;

[0078] A second cover plate 222, the second cover plate 222 covers the second groove and is fixedly connected to the second groove;

[0079] The second cover plate 222 is provided with a sixth through hole corresponding to the second bolt hole.

[0080] In this embodiment, the first guiding rod 211 is used to support and guide the first adjusting wedge 21 to prevent the first adjusting wedge 21 from shifting during the sliding process; in a preferred solution, two first guiding rods 211 may be provided and are respectively located on both sides of the first bolt hole; the second guiding rod 221 is used to support and guide the second adjusting wedge 22 to prevent the second adjusting wedge 22 from shifting during the sliding process; in a preferred solution, two second guiding rods 221 may be provided and are respectively located on both sides of the second bolt hole; the first guiding rod 211 and the second guiding rod 221 are symmetrically arranged; the first cover plate 212 is used to fix the second end of the first guiding rod 211. During installation, the first cover plate 212 is fixed to the first groove by a first screw 71. The first bolt 111 passes through the fifth through hole and the first bolt hole and contacts the first adjusting wedge 21, and the first adjusting wedge 21 is pushed to slide in the direction of the second adjusting wedge 22 by adjusting the supply amount of the first bolt 111; the second cover plate 222 is used to fix the second end of the second guiding rod 221. During installation, the second cover plate 222 is fixed to the second groove by a second screw 72. The second bolt 121 passes through the sixth through hole and the second bolt hole and contacts the second adjusting wedge 22, and the second adjusting wedge 22 is pushed to slide in the direction of the first adjusting wedge 21 by adjusting the supply amount of the second bolt 121.

[0081] In an alternative embodiment of the present invention, the first sliding portion includes: a first fixed block 311, a first movable block 312, a first limiting plate 313, at least one third guiding rod 314, and a first rectangular spring 315 sleeved on the first end of the third guiding rod 314;

[0082] Wherein, the first end of the first fixed block 311 is fixed on the second end face of the second support 3, and at least one first circular groove is provided on the end face of the second end of the first fixed block 311;

[0083] The first end of the third guide rod 314 is fixed in the first circular groove, and the second end of the third guide rod 314 is fixedly connected to the first limiting plate 313;

[0084] The first movable block 312 is sleeved on the second end of the third guide rod 314 and is located between the first limiting plate 313 and the first rectangular spring 315;

[0085] The first movable block 312 is slidably connected to the third guide rod 314, and the side surface of the first movable block 312 is in contact connection with the first adjusting wedge 21.

[0086] In an optional embodiment of the present invention, the second sliding portion includes: a second fixed block 321, a second movable block 322, a second limiting plate 323, at least one fourth guide rod 324, and a second rectangular spring 325 sleeved on the first end of the fourth guide rod 324;

[0087] Wherein, the first end of the second fixed block 321 is fixed on the second end surface of the second support 3, and at least one second circular groove is provided on the end surface of the second end of the second fixed block 321;

[0088] The first end of the fourth guide rod 324 is fixed in the second circular groove, and the second end of the fourth guide rod 324 is fixedly connected to the second limiting plate 323;

[0089] The second movable block 322 is sleeved on the second end of the fourth guide rod 324 and is located between the second limiting plate 323 and the second rectangular spring 325;

[0090] The second movable block 322 is slidably connected to the fourth guide rod 324, and the side surface of the second movable block 322 is in contact connection with the second adjusting wedge 22.

[0091] In this embodiment, the first movable block 312 can slide on the third guide rod 314 by compressing the first rectangular spring 315; the second movable block 322 can slide on the fourth guide rod 324 by compressing the second rectangular spring 325; the first end of the third guide rod 314 is fixed in the first circular groove by at least one first hexagon socket head screw 61, and the second end of the third guide rod 314 is fixedly connected to the first limiting plate 313 by a first hexagon socket head shoulder screw 81; the first end of the fourth guide rod 324 is fixed in the second circular groove by at least one second hexagon socket head screw 62, and the second end of the fourth guide rod 324 is fixedly connected to the second limiting plate 323 by a second hexagon socket head shoulder screw 82; in a preferred solution, the number of the third guide rods 314 and the fourth guide rods 324 is 4 each.

[0092] In this embodiment, as Figure 7 shown, Figure 7 Y in represents the direction perpendicular to the booster 5 and the core stage rocket 4, that is, the direction in which the booster 5 approaches the core stage rocket 4; the structural design of the first sliding part and the second sliding part enables the rocket sub-bundling mechanism to have the function of automatically adjusting the displacement difference in the Y-axis direction (the Y-axis direction is the direction perpendicular to the booster 5 and the core stage rocket 4), that is, when the booster 5 approaches the core stage rocket 4, the first adjusting wedge 21 and the second adjusting wedge 22 will push the first movable block 312 and the second movable block 322, so that the first movable block 312 and the second movable block 322 compress the first rectangular spring 315 and the second rectangular spring 325, so that the first support 1 moves towards the second support 3, thereby eliminating the displacement difference generated when the booster 5 approaches the core stage rocket 4; similarly, when the booster 5 moves away from the core stage rocket 4, the compression amount of the first rectangular spring 315 and the second rectangular spring 325 can be restored by stretching, so as to eliminate the displacement difference generated when moving away; during installation, the first rectangular spring 315 and the second rectangular spring 325 need to be compressed to a certain extent to meet the stretching when the booster 5 moves away from the core stage rocket 4, and at the same time, after compression, the first rectangular spring 315 and the second rectangular spring 325 can also generate a pushing force during the separation of the booster 5 and the core stage rocket 4 to assist the separation of the booster 5.

[0093] In this embodiment, the adjustment amount of the displacement difference in the Y-axis direction is related to the heights of the first rectangular spring 315 and the second rectangular spring 325, that is, Figure 7 L in, so the adjustment amount of the displacement difference in the Y-axis direction can be set by selecting different specifications of the first rectangular spring 315 and the second rectangular spring 325.

[0094] In an alternative embodiment of the present invention, the contact surfaces of the first adjusting wedge block 21 and the first sliding part are both inclined surfaces;

[0095] The contact surfaces of the second adjusting wedge block 22 and the second sliding part are both inclined surfaces.

[0096] In an alternative embodiment of the present invention, the design that the length of the end face of the first sliding part in contact with the first adjusting wedge block 21 is greater than the length of the end face of the first adjusting wedge block 21 in contact with the first sliding part is to enable the first adjusting wedge block 21 to slide stably on the first sliding part, and at the same time increase the adjustment amount of the first adjusting wedge block 21 and the first sliding part in the X direction.

[0097] The design that the length of the end face of the second sliding part in contact with the second adjusting wedge block 22 is greater than the length of the end face of the second adjusting wedge block 22 in contact with the second sliding part is to enable the second adjusting wedge block 22 to slide stably on the second sliding part, and at the same time increase the adjustment amount of the second adjusting wedge block 22 and the second sliding part in the X direction.

[0098] In an alternative embodiment of the present invention, the first end face of the first support 1 is an arc structure. The first end face of the first support 1 is fixedly connected to the core stage rocket 4 through at least two third bolts 14. The arc structure design of the first end face of the first support 1 is to be able to connect more closely with the core stage rocket 4. The specific radian value of the arc structure on the first support 1 can be set according to the radian of the contact surface with the core stage rocket 4.

[0099] In an alternative embodiment of the present invention, the first end face of the second support 3 is an arc structure. The first end face of the second support 3 is fixedly connected to the booster 5 through at least three fourth bolts 31. The arc structure design of the first end face of the second support 3 is to be able to connect more closely with the booster 5. The specific radian value of the arc structure on the second support 3 can be set according to the radian of the contact surface with the booster 5.

[0100] The specific use process of the rocket secondary bundling mechanism described in this embodiment is as follows: First, fix the first fixing plate 11, the second fixing plate 12, the first adjusting wedge 21, and the second adjusting wedge 22 on the second end face of the first support 1 in sequence, and fixedly connect the first end face of the first support 1 with the core stage rocket 4. Then, fix the first sliding part and the second sliding part on the second end face of the second support 3, and fixedly connect the first end face of the second support 3 with the booster 5. Then, adjust the positions of the first sliding part and the second sliding part, and place the first sliding part and the second sliding part between the first adjusting wedge 21 and the second adjusting wedge 22. At the same time, compress the first rectangular spring 315 to a first preset value through the first movable block 312, and compress the second rectangular spring 325 to a second preset value through the second movable block 322. The first preset value is equal to the second preset value. Finally, push the first adjusting wedge 21 by rotating the first bolt 111. At the same time, push the second adjusting wedge 22 by rotating the second bolt 121, so that the first adjusting wedge 21 and the second adjusting wedge 22 clamp the first sliding part and the second sliding part.

[0101] During the flight, when the core stage rocket 4 and the booster 5 generate vibrations in the X-axis direction, the displacement difference generated by the vibration can be eliminated by the relative up-and-down sliding between the adjusting wedge and the sliding part. When the core stage rocket 4 and the booster 5 generate vibrations in the Y-axis direction, the displacement difference generated by the vibration in the Y-axis direction can be eliminated by compressing or releasing the spring. During the flight, when the booster 5 needs to separate from the core stage rocket 4, the bundling link 7 can be unlocked and released first. Then, under the self-gravity of the booster 5, the first sliding part and the second sliding part can directly break away from the clamping of the first adjusting wedge 21 and the second adjusting wedge 22, thereby realizing the automatic disconnection of the secondary bundling mechanism.

[0102] The rocket secondary bundling mechanism described in the present invention solves the problems of the traditional secondary bundling mechanism, such as complex structure, low safety, and inability to adjust the displacement difference generated axially between the booster and the core stage rocket during flight. It realizes the automatic adjustment function of the displacement difference generated axially between the booster and the core stage rocket during flight. At the same time, it improves the safety of the secondary bundling mechanism and also has the advantages of simple structure, small mass, and convenient installation.

[0103] The above is the preferred embodiment of the present invention. It should be noted that for those of ordinary skill in the art, without departing from the principle described in the present invention, several improvements and refinements can be made, and these improvements and refinements should also be regarded as the protection scope of the present invention.

Claims

1. A rocket secondary bundling mechanism, characterized in that, Including: A first support (1), a first adjusting wedge block (21), a second adjusting wedge block (22), and a second support (3); Wherein, a first end face of the first support (1) is fixedly connected to the core-stage rocket (4), a first fixing plate (11) and a second fixing plate (12) are arranged on a second end face of the first support (1), and the first fixing plate (11) and the second fixing plate (12) are arranged oppositely; Both the first adjusting wedge block (21) and the second adjusting wedge block (22) are slidably connected to the second end face of the first support (1), and are both arranged between the first fixing plate (11) and the second fixing plate (12); A first end face of the second support (3) is fixedly connected to the booster (5), and a first sliding part and a second sliding part are arranged on a second end face of the second support (3); A first end of the first sliding part and a first end of the second sliding part are both fixedly connected to the second end face of the second support (3), and are oppositely arranged on the second end face of the second support (3), and a second end of the first sliding part and a second end of the second sliding part are both arranged between the first adjusting wedge block (21) and the second adjusting wedge block (22); A first bolt hole is arranged on the first fixing plate (11), a first bolt (111) passes through the first bolt hole and contacts the first adjusting wedge block (21), and pushes the first adjusting wedge block (21) to press the first sliding part; A second bolt hole is arranged on the second fixing plate (12), a second bolt (121) passes through the second bolt hole and contacts the second adjusting wedge block (22), and pushes the second adjusting wedge block (22) to press the second sliding part.

2. The rocket secondary bundling mechanism according to claim 1, wherein A dovetail groove (13) is arranged on the second end face of the first support (1), and the dovetail groove (13) is arranged between the first fixing plate (11) and the second fixing plate (12); Both the first adjusting wedge block (21) and the second adjusting wedge block (22) are clamped on the dovetail groove (13), and are slidably connected to the dovetail groove (13).

3. The rocket secondary bundling mechanism according to claim 1, characterized in that, Further including: A first groove arranged on the first fixing plate (11), at least one first through hole is arranged in the first groove, and the first bolt hole is arranged in the first groove; At least one second through hole arranged on the first adjusting wedge block (21) and corresponding to the first through hole; At least one first guide rod (211), a first end of the first guide rod (211) passes through the first through hole and the second through hole, and a second end of the first guide rod (211) is fixed in the first groove; A first cover plate (212), the first cover plate (212) covers the first groove, and is fixedly connected to the first groove; A fifth through hole corresponding to the first bolt hole is arranged on the first cover plate (212).

4. The rocket secondary bundling mechanism according to claim 1, wherein Further including: A second groove arranged on the second fixing plate (12), at least one third through hole is arranged in the second groove, and the second bolt hole is arranged in the second groove; At least one fourth through-hole provided on the second adjusting wedge block (22) and corresponding to the third through-hole; At least one second guide rod (221), the first end of the second guide rod (221) passes through the third through-hole and the fourth through-hole, and the second end of the second guide rod (221) is fixed in the second groove; A second cover plate (222), the second cover plate (222) covers the second groove and is fixedly connected to the second groove; The second cover plate (222) is provided with a sixth through-hole corresponding to the second bolt hole.

5. The rocket secondary bundling mechanism according to claim 1, characterized in that, The first sliding part includes: a first fixing block (311), a first movable block (312), a first limiting plate (313), at least one third guide rod (314) and a first rectangular spring (315) sleeved on the first end of the third guide rod (314); Wherein, the first end of the first fixing block (311) is fixed on the second end face of the second support (3), and at least one first circular groove is provided on the end face of the second end of the first fixing block (311); The first end of the third guide rod (314) is fixed in the first circular groove, and the end of the second end of the third guide rod (314) is fixedly connected to the first limiting plate (313); The first movable block (312) is sleeved on the second end of the third guide rod (314) and is located between the first limiting plate (313) and the first rectangular spring (315); The first movable block (312) is slidably connected to the third guide rod (314), and the side surface of the first movable block (312) is in contact connection with the first adjusting wedge block (21).

6. The rocket secondary bundling mechanism according to claim 1, wherein The second sliding part includes: a second fixing block (321), a second movable block (322), a second limiting plate (323), at least one fourth guide rod (324) and a second rectangular spring (325) sleeved on the first end of the fourth guide rod (324); Wherein, the first end of the second fixing block (321) is fixed on the second end face of the second support (3), and at least one second circular groove is provided on the end face of the second end of the second fixing block (321); The first end of the fourth guide rod (324) is fixed in the second circular groove, and the end of the second end of the fourth guide rod (324) is fixedly connected to the second limiting plate (323); The second movable block (322) is sleeved on the second end of the fourth guide rod (324) and is located between the second limiting plate (323) and the second rectangular spring (325); The second movable block (322) is slidably connected to the fourth guide rod (324), and the side surface of the second movable block (322) is in contact connection with the second adjusting wedge block (22).

7. The rocket secondary bundling mechanism according to claim 1, characterized in that, The contact surfaces of the first adjusting wedge block (21) and the first sliding part are all inclined surfaces; The contact surfaces of the second adjusting wedge block (22) and the second sliding part are all inclined surfaces.

8. The rocket secondary bundling mechanism according to claim 1, characterized in that The length of the end face of the first sliding part in contact with the first adjusting wedge block (21) is greater than the length of the end face of the first adjusting wedge block (21) in contact with the first sliding part; The length of the end face of the second sliding part in contact with the second adjusting wedge block (22) is greater than the length of the end face of the second adjusting wedge block (22) in contact with the second sliding part.

9. The rocket secondary bundling mechanism according to claim 1, characterized in that, The first end face of the first support (1) is an arc structure, and the first end face of the first support (1) is fixedly connected to the core stage rocket (4) through at least two third bolts (14).

10. The rocket secondary bundling mechanism according to claim 1, characterized in that, The first end face of the second support (3) is an arc structure, and the first end face of the second support (3) is fixedly connected to the booster (5) through at least three fourth bolts (31).

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