Structure of offshore suspended rocket launch platform

Abstract

The present invention relates to the technical field of launching platforms, and discloses an offshore suspended rocket launching platform structure, comprising a hull assembly, a flip assembly, a floating assembly, a loading assembly and a launching assembly, wherein the flip assembly is symmetrically hinged on both sides of the hull assembly, the floating assembly is connected to the flip assembly through a stabilizing assembly, the loading assembly is symmetrically placed on the top of the hull assembly, and the launching assembly is installed in the middle of the hull assembly; a first flip frame is installed on the floating assembly, a second flip frame is rotatably connected to the middle of the first flip frame, a third flip frame is rotatably connected to the middle of the second flip frame, a propeller is installed in the middle of the third flip frame, and a plurality of propellers are distributed and installed on the first flip frame at four corners, thereby solving the problems of poor stability of the existing offshore suspended rocket launching platform due to the fluctuation of sea water and unadjustable launching angle in the prior art.

Description

Technical Field

[0001] The patent of this invention relates to the technical field of launch platforms, specifically, to the structure of an offshore suspended rocket launch platform. Background Art

[0002] The Chinese patent with publication number CN115200407B discloses an offshore suspended rocket launch platform, a rocket launch device and a launch method, which belongs to the field of rocket offshore launch. An offshore suspended rocket launch platform includes a deflector, a support and a walking track; the deflector is a wave-shaped structure, the deflector includes a pressure tank inside, and the pressure tank is connected to the "U"-shaped part of the deflector through a liquid flow channel; a rocket launch device includes an offshore suspended rocket launch platform and a launch ship, a launch platform and a walking trolley; the offshore suspended rocket launch platform is connected to the launch ship, and the launch platform is arranged on the walking trolley, and the rocket can be transported to the offshore suspended rocket launch platform for launch by the transportation of the walking trolley. The present invention can improve the convenience of rocket offshore launch, improve the efficiency of offshore rocket launch, and has low production, use and maintenance costs.

[0003] A Chinese patent with publication number CN106197146B discloses a rocket launch platform with adjustable rocket model and attitude, which belongs to the technical field of rocket launch devices, and includes a launch frame, a moving platform, a support platform, a fixed platform, support legs, and first to ninth branches; wherein the first, second and third branches are evenly distributed on the launch frame; the fourth and fifth branches are respectively connected between the launch frame and the support platform, and form a space closed loop mechanism with the launch frame and the support platform; the sixth branch is connected between the support platform and the moving platform; the seventh, eighth and ninth branches are respectively connected between the moving and fixed platforms, and form a space closed loop mechanism with the moving and fixed platforms; three support legs are evenly distributed on the bottom of the fixed platform, one end of each support leg is fastened to the fixed platform by bolts, and the other end is fastened to the launch ground by ground nails; the present invention has the characteristics of compact structure, strong adaptability to working conditions, flexible attitude adjustment, relatively simple control, etc., and can realize the launch of rockets of different models.

[0004] However, the existing offshore suspended rocket launch platform has poor stability due to the fluctuation of sea water and the launch angle cannot be adjusted. Summary of the invention

[0005] The purpose of the present invention is to provide an offshore suspended rocket launching platform structure, aiming to solve the problem in the prior art that the existing offshore suspended rocket launching platform has poor stability due to the fluctuation of sea water and the launching angle cannot be adjusted.

[0006] The present invention is implemented as follows: the offshore suspended rocket launch platform structure includes a hull assembly, a flip assembly, a floating assembly, a loading assembly and a launching assembly, wherein the flip assembly is symmetrically hinged on both sides of the hull assembly, the floating assembly is connected to the flip assembly through a stabilizing assembly, the loading assembly is symmetrically placed on the top of the hull assembly, and the launching assembly is installed in the middle of the hull assembly;

[0007] A first turning frame is installed on the floating assembly, a second turning frame is rotatably connected to the middle of the first turning frame, a third turning frame is rotatably connected to the middle of the second turning frame, a propeller is installed in the middle of the third turning frame, and a plurality of propellers are installed on the first turning frame in four corners.

[0008] The hull assembly includes a rocket bay and a launch pad, wherein the rocket bay is symmetrically arranged on both sides of the launch pad, and a plurality of rockets are loaded in the middle of the rocket bay. The flip assembly includes a flip cylinder, a flip plate and a flip hinge, wherein the flip hinge is symmetrically rotatably connected to both sides of the rocket bay, and both sides of the flip plate are hinged to the flip hinge, and the flip cylinder is hinged in the middle of the rocket bay, and the telescopic end of the flip cylinder is hinged to the flip plate.

[0009] The floating assembly also includes a floating plate, and the floating plate is connected to the flip plate through a stabilizing assembly. The stabilizing assembly includes a stabilizing support plate, an adjusting screw, a stabilizing seat, a stabilizing connecting rod, a stabilizer and a stabilizing hinge rod. The stabilizing support plate is fixedly connected to one side of the flip plate, and the stabilizing support plate is hinged to the stabilizing seat. An adjusting screw is threadedly connected to the hinge between the stabilizing support plate and the stabilizing seat. The stabilizing connecting rod is symmetrically placed in the middle of the stabilizing seat, and both ends of the stabilizing hinge rod are hinged to the non-hinged end of the stabilizing connecting rod. Both ends of the stabilizer are respectively hinged to two stabilizing connecting rods distributed up and down on the same side.

[0010] The launching assembly comprises a launching base, a launching bracket, a first slide rail, a first screw block, a first screw rod, a first slide rod, a transverse slide rod, a second screw rod and a driving motor. The launching base is mounted on the top of the launching platform, the launching bracket is symmetrically placed on the top of the launching base, the first slide rail is fixedly connected to one side of the launching bracket, the first screw block is driven by the first screw rod to slide on the first slide rail, a first slide rod is mounted on the top of the first screw block, the transverse slide rod is slidably connected to the first slide rod, the driving motor is mounted on one side of the first screw block, the second screw rod is drivingly connected to the driving motor, and the second screw drives the transverse slide rod to slide.

[0011] The launching assembly also includes an angle turntable, a turntable hinge, a driving block, a third screw and a rocket bracket. The angle turntable is installed on the top of the launching base. The turntable hinge is hinged to the driving block. The driving block drives the third screw to rotate. The rocket bracket is connected to the third screw in a driving manner.

[0012] The launching assembly also includes a launching chamber, a launching signal block and a launching induction block. The launching chamber is installed on the top of the rocket support, the launching signal block is placed on the launching chamber, and the launching induction blocks are placed on both sides of the launching chamber.

[0013] The feeding assembly includes a feeding seat, a feeding cylinder, a feeding hinge rod, a feeding buffer rod, a feeding rack and a feeding push rod. The feeding seat is slidably connected to the top of the rocket compartment, the feeding rack is hinged to the top of the feeding seat, the two ends of the feeding hinge rod are respectively hinged to the feeding seat and the middle of the feeding rack, the feeding cylinder is hinged on the feeding seat, the telescopic end of the feeding cylinder is hinged to the middle of the feeding hinge rod, the feeding buffer rod is placed in the middle of the feeding seat, and the feeding push rods are symmetrically installed in the middle of the feeding rack.

[0014] A clamping block is installed in the middle of the loading frame. The clamping block includes a clamping frame, a clamping push rod and a clamping sleeve. The clamping push rod is slidably connected to the middle of the clamping frame, and the clamping sleeve is placed on the top of the clamping frame.

[0015] A plurality of flow rate monitoring blocks are installed at the bottom of the floating assembly, and the flow rate monitoring blocks monitor the floating of the sea surface, control the rotation speed and direction of the propeller, and reduce the influence of the floating of the sea surface.

[0016] The clamping block is detachably mounted on the loading rack, and the clamping block further comprises a clamping ring, which is mounted on the top of the clamping sleeve.

[0017] Compared with the prior art, the present invention has the following beneficial effects:

[0018] The present invention launches rockets at sea, utilizing the vast space and stability of the ocean, and reducing dependence on land facilities. In addition, this modular design allows the platform to be quickly adjusted and reconfigured according to different launch requirements, reducing dependence on land facilities and reducing construction and maintenance costs. The floating component is connected to the flip component through a stabilizing component, providing additional stability. The setting of the propeller helps to control the direction and position of the platform so that it can remain stable on the sea surface. The rotating connection design of the first flip frame, the second flip frame and the third flip frame, combined with the four-corner distribution of the propeller, can form a stable support structure on the sea surface to effectively resist the impact of waves. The design of the propeller allows the platform to adjust its position and control its direction as needed, improving the maneuverability and flexibility of the platform. When encountering sudden sea conditions, the propeller can quickly adjust the speed and direction, allowing the platform to respond quickly and remain stable. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] Figure 1 It is a structural schematic diagram of the offshore suspended rocket launching platform of the present invention;

[0020] Figure 2It is a schematic structural diagram of a hull assembly in an offshore suspended rocket launching platform of the present invention;

[0021] Figure 3 yes Figure 2 A partial enlarged view of the middle A area;

[0022] Figure 4 It is a structural schematic diagram of a launch assembly in an offshore suspended rocket launch platform of the present invention;

[0023] Figure 5 It is a structural schematic diagram of a loading assembly in an offshore suspended rocket launching platform of the present invention;

[0024] Figure 6 It is a schematic diagram of the structure of the clamping block in the offshore suspended rocket launching platform of the present invention;

[0025] Figure 7 It is a schematic structural diagram of a stabilizing assembly in an offshore suspended rocket launching platform of the present invention;

[0026] Reference numerals:

[0027] 1. Hull assembly; 2. Flip assembly; 3. Floating assembly; 4. Rocket chamber; 5. Loading assembly; 6. Launch assembly; 7. Launch platform; 8. Flip cylinder; 9. Flip plate; 10. Floating plate; 11. Stable assembly; 12. Stable support plate; 13. Adjusting screw; 14. Stable seat; 15. Stable connecting rod; 16. Stabilizer; 17. Stable hinge rod; 18. Propeller; 19. First flip frame; 20. Flip hinge rod; 21. Second flip frame; 22. Third flip frame; 23. Launch base; 24. Launch bracket; 25. First slide rail; 2 6. First screw block; 27. First screw rod; 28. First slide rod; 29. ​​Second screw rod; 30. Drive motor; 31. Angle turntable; 32. Turntable hinge seat; 33. Drive block; 34. Third screw rod; 35. Rocket bracket; 36. Launch chamber; 37. Transmitting signal block; 38. Transmitting induction block; 39. Loading seat; 40. Loading cylinder; 41. Loading hinge rod; 42. Loading buffer rod; 43. Loading rack; 44. Loading push rod; 45. Clamping block; 46. Clamping rack; 47. Clamping push rod; 48. Clamping sleeve; 49. Clamping ring. DETAILED DESCRIPTION

[0028] In order to make the purpose, technical solution and advantages of the present invention more clearly understood, the present invention is further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are only used to explain the present invention and are not intended to limit the present invention.

[0029] The implementation of the present invention is described in detail below in conjunction with specific embodiments.

[0030] like Figure 1-3 As shown, the present invention provides a structure of an offshore suspended rocket launching platform, comprising a hull assembly 1, a flip assembly 2, a floating assembly 3, a loading assembly 5 and a launching assembly 6, wherein the flip assembly 2 is symmetrically hinged on both sides of the hull assembly 1, the floating assembly 3 is connected to the flip assembly 2 through a stabilizing assembly 11, the loading assembly 5 is symmetrically placed on the top of the hull assembly 1, and the launching assembly 6 is installed in the middle of the hull assembly 1;

[0031] A first turning frame 19 is installed on the floating assembly 3, the middle part of the first turning frame 19 is rotatably connected to the second turning frame 21, the middle part of the second turning frame 21 is rotatably connected to the third turning frame 22, the middle part of the third turning frame 22 is installed with a propeller 18, and multiple propellers 18 are installed on the first turning frame 19 at four corners.

[0032] The present invention launches rockets at sea, utilizing the vast space and stability of the ocean, and reducing dependence on land facilities. In addition, this modular design allows the platform to be quickly adjusted and reconfigured according to different launch requirements, reducing dependence on land facilities and reducing construction and maintenance costs. The floating component 3 is connected to the flip component 2 through the stabilizing component 11, providing additional stability. The setting of the propeller helps to control the direction and position of the platform so that it can remain stable on the sea surface. The rotating connection design of the first flip frame 19, the second flip frame 21 and the third flip frame 22, combined with the four-corner distribution of the propeller 18, can form a stable support structure on the sea surface to effectively resist the impact of waves. The design of the propeller 18 allows the platform to adjust its position and control its direction as needed, thereby improving the maneuverability and flexibility of the platform. When encountering sudden sea conditions, the propeller 18 can quickly adjust the speed and direction, allowing the platform to respond quickly and remain stable.

[0033] The hull assembly 1 includes a rocket bay 4 and a launch platform 7. The rocket bay 4 is symmetrically placed on both sides of the launch platform 7. A plurality of rockets are loaded in the middle of the rocket bay 4. The flip assembly 2 includes a flip cylinder 8, a flip plate 9 and a flip hinge 20. The flip hinge 20 is symmetrically rotatably connected to both sides of the rocket bay 4. Both sides of the flip plate 9 are hinged to the flip hinge 20. The flip cylinder 8 is hinged to the middle of the rocket bay 4. The telescopic end of the flip cylinder 8 is hinged to the flip plate 9.

[0034] The flip assembly 2 controls the use position of the floating assembly 3. After the floating assembly 3 is lowered, the navigation speed of the hull assembly 1 can be accelerated. When the hull assembly 1 reaches the designated position for launch, the floating force can be offset or reduced according to the floating conditions of the sea surface, thereby optimizing the storage and launch process of the rocket. The rocket chamber 4 is symmetrically placed on both sides of the launch platform 7. This symmetrical layout helps to maintain the balance of the hull assembly 1 and provides sufficient space to load multiple rockets.

[0035] The floating assembly 3 also includes a floating plate 10, which is connected to the flip plate 9 through a stabilizing assembly 11. The stabilizing assembly 11 includes a stabilizing support plate 12, an adjusting screw 13, a stabilizing seat 14, a stabilizing connecting rod 15, a stabilizer 16 and a stabilizing hinge 17. The stabilizing support plate 12 is fixedly connected to one side of the flip plate 9, and the stabilizing support plate 12 is hinged to the stabilizing seat 14. The adjusting screw 13 is threadedly connected to the hinge between the stabilizing support plate 12 and the stabilizing seat 14. The stabilizing connecting rod 15 is symmetrically placed in the middle of the stabilizing seat 14. Both ends of the stabilizing hinge 17 are hinged to the non-hinged end of the stabilizing connecting rod 15, and both ends of the stabilizer 16 are respectively hinged to two stabilizing connecting rods 15 distributed up and down on the same side.

[0036] The design of the floating assembly 3, including the floating plate 10 and the stabilizing assembly 11, is to ensure that the platform can remain stable on rough seas. The complex mechanical structure of the stabilizing assembly, such as the stabilizing support plate 12, the adjusting screw 13, the stabilizing seat 14, the stabilizing link 15, the stabilizer 16 and the stabilizing hinge 17, are all designed to improve the stability of the platform. The multi-link and hinged design of the stabilizing assembly 11 can maintain the stability of the floating assembly under the impact of waves and reduce the adverse effects on rocket launches. The adjusting screw 13 allows the operator to adjust the tension of the stabilizing assembly according to changes in sea conditions to adapt to different sea surface conditions. The design of the stabilizer 16 can provide mechanical buffering when waves impact, absorb and reduce wave energy, and protect the platform structure.

[0037] The launching assembly 6 includes a launching base 23, a launching bracket 24, a first slide rail 25, a first screw block 26, a first screw rod 27, a first slide rod 28, a transverse slider, a second screw rod 29 and a driving motor 30. The launching base 23 is installed on the top of the launching platform 7, the launching bracket 24 is symmetrically placed on the top of the launching base 23, the first slide rail 25 is fixed to one side of the launching bracket 24, the first screw block 26 is driven by the first screw rod 27 to slide on the first slide rail 25, a first slide rod 28 is installed on the top of the first screw block 26, the transverse slider is slidably connected to the first slide rod 28, the driving motor 30 is installed on one side of the first screw block 26, the second screw rod 29 is transmission-connected to the driving motor 30, and the second screw rod 29 drives the transverse slider to slide.

[0038] The launching assembly 6 also includes an angle turntable 31, a turntable hinge 32, a driving block 33, a third screw 34 and a rocket bracket 35. The angle turntable 31 is installed on the top of the launching base 23. The turntable hinge 32 is hinged to the driving block 33. The driving block 33 drives the third screw 34 to rotate. The rocket bracket 35 is connected to the third screw 34 by transmission.

[0039] The launching assembly 6 also includes a launching chamber 36 , a launching signal block 37 and a launching sensing block 38 . The launching chamber 36 is installed on the top of the rocket bracket 35 , the launching signal block 37 is placed on the launching chamber 36 , and the launching sensing block 38 is placed on both sides of the launching chamber 36 .

[0040] The design of the first slide rail 25 and the first screw block 26, in conjunction with the drive motor 30, can achieve precise control of the rocket launch position, which is crucial to ensuring the accuracy of the launch trajectory. The automated design of the launch assembly 6 reduces the possibility of human error and improves the reliability of the launch process. The adjustable design of the launch assembly 6 allows for quick adjustment of the launch angle and direction to accommodate different launch requirements.

[0041] The loading assembly 5 includes a loading seat 39, a loading cylinder 40, a loading hinge rod 41, a loading buffer rod 42, a loading rack 43 and a loading push rod 44. The loading seat 39 is slidably connected to the top of the rocket chamber 4, the loading rack 43 is hinged to the top of the loading seat 39, the two ends of the loading hinge rod 41 are respectively hinged to the loading seat 39 and the middle of the loading rack 43, the loading cylinder 40 is hinged on the loading seat 39, the telescopic end of the loading cylinder 40 is hinged to the middle of the loading hinge rod 41, the loading buffer rod 42 is placed in the middle of the loading seat 39, and the loading push rod 44 is symmetrically installed in the middle of the loading rack 43.

[0042] A clamping block 45 is installed in the middle of the loading frame 43. The clamping block 45 includes a clamping frame 46, a clamping push rod 47 and a clamping sleeve 48. The clamping push rod 47 is slidably connected to the middle of the clamping frame 46, and the clamping sleeve 48 is placed on the top of the clamping frame 46.

[0043] A plurality of flow rate monitoring blocks are installed at the bottom of the floating component 3. The flow rate monitoring blocks monitor the floating of the sea surface, control the rotation speed and direction of the propeller 18, and reduce the impact of the floating of the sea surface. The flow rate monitoring block can monitor the speed and direction of the ocean current in real time and provide important environmental data for the platform. According to the data provided by the flow rate monitoring block, the platform can dynamically adjust the working state of the propeller 18 to adapt to the changing sea conditions. By adjusting the propeller, the platform can maintain a relatively stable position and posture, and rocket launches can be carried out even in harsh marine environments. The flow rate monitoring block can also predict the upcoming severe sea conditions and take measures in advance, such as adjusting the launch plan or strengthening the fixation of the platform to avoid potential risks during the launch process.

[0044] The clamping block 45 is detachably mounted on the loading rack 43, and the clamping block 45 also includes a clamping ring 49, which is mounted on the top of the clamping sleeve 48. The design of the clamping block 45 can provide a stable fixation when the rocket is loaded onto the loading rack 43, ensuring that the rocket will not move or tilt during transportation and launch preparation. The detachable design of the clamping block 45 allows it to be adjusted or replaced according to different types of rockets, providing a high degree of flexibility. The design of the clamping push rod 47 and the clamping sleeve 48 allows the rocket to be quickly fixed or released, speeding up the loading process. The design of the clamping ring 49 provides additional protection for the rocket to prevent accidental falling off or sliding during the movement of the rocket.

[0045] The same or similar numbers in the drawings of this embodiment correspond to the same or similar parts; in the description of the present invention, it should be understood that if the terms "upper", "lower", "left", "right" and the like indicate directions or positional relationships based on the directions or positional relationships shown in the drawings, it is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific direction, be constructed and operated in a specific direction. Therefore, the terms describing the positional relationship in the drawings are only used for illustrative purposes and cannot be understood as limitations on this patent. For ordinary technicians in this field, the specific meanings of the above terms can be understood according to specific circumstances.

[0046] As shown in the drawings, a preferred embodiment of the present invention is provided.

[0047] The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. Any modifications, equivalent substitutions and improvements made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. The offshore suspended rocket launching platform structure is characterized by: The invention comprises a hull component (1), a turnover component (2), a floating component (3), a loading component (5) and a launching component (6), wherein the turnover component (2) is symmetrically hinged on both sides of the hull component (1), the floating component (3) is connected to the turnover component (2) via a stabilizing component (11), the loading component (5) is symmetrically arranged on the top of the hull component (1), and the launching component (6) is installed in the middle of the hull component (1); A first turning frame (19) is mounted on the floating assembly (3); a second turning frame (21) is rotatably connected to the middle of the first turning frame (19); a third turning frame (22) is rotatably connected to the middle of the second turning frame (21); a propeller (18) is mounted on the middle of the third turning frame (22); and a plurality of propellers (18) are mounted on the first turning frame (19) in a distributed manner at four corners. The hull assembly (1) comprises a rocket chamber (4) and a launch platform (7), wherein the rocket chamber (4) is symmetrically arranged on both sides of the launch platform (7), and a plurality of rockets are loaded in the middle of the rocket chamber (4); the flip assembly (2) comprises a flip cylinder (8), a flip plate (9) and a flip hinge rod (20), wherein the flip hinge rod (20) is symmetrically rotatably connected to both sides of the rocket chamber (4), both sides of the flip plate (9) are hinged to the flip hinge rod (20), the flip cylinder (8) is hinged to the middle of the rocket chamber (4), and the telescopic end of the flip cylinder (8) is hinged to the flip plate (9); The floating assembly (3) further comprises a floating plate (10), wherein the floating plate (10) is connected to the flip plate (9) via a stabilizing assembly (11), wherein the stabilizing assembly (11) comprises a stabilizing support plate (12), an adjusting screw (13), a stabilizing seat (14), a stabilizing connecting rod (15), a stabilizer (16) and a stabilizing hinge rod (17), wherein the stabilizing support plate (12) is fixedly connected to one side of the flip plate (9), wherein the stabilizing support plate (12) is hinged to the stabilizing seat (14), wherein the adjusting screw (13) is threadedly connected to the hinged portion between the stabilizing support plate (12) and the stabilizing seat (14), wherein the stabilizing connecting rod (15) is symmetrically arranged in the middle of the stabilizing seat (14), wherein both ends of the stabilizing hinge rod (17) are hinged to the non-hinged end of the stabilizing connecting rod (15), and wherein both ends of the stabilizer (16) are respectively hinged to two stabilizing connecting rods (15) distributed up and down on the same side.

2. The offshore suspended rocket launching platform structure according to claim 1 is characterized in that: The launching assembly (6) comprises a launching base (23), a launching bracket (24), a first slide rail (25), a first screw block (26), a first screw rod (27), a first slide rod (28), a transverse slide block, a second screw rod (29) and a driving motor (30); the launching base (23) is mounted on the top of the launching platform (7); the launching bracket (24) is symmetrically arranged on the top of the launching base (23); the first slide rail (25) is fixed to one side of the launching bracket (24); the first screw block (26) is driven by the first screw rod (27) to slide on the first slide rail (25); a first slide rod (28) is mounted on the top of the first screw block (26); the transverse slide block is slidably connected to the first slide rod (28); the driving motor (30) is mounted on one side of the first screw block (26); the second screw rod (29) is drivingly connected to the driving motor (30); the second screw rod (29) drives the transverse slide block to slide.

3. The offshore suspended rocket launching platform structure according to claim 2 is characterized in that: The launching assembly (6) further comprises an angle turntable (31), a turntable hinge seat (32), a driving block (33), a third screw rod (34) and a rocket bracket (35); the angle turntable (31) is mounted on the top of the launching base (23); the turntable hinge seat (32) is hingedly connected to the driving block (33); the driving block (33) drives the third screw rod (34) to rotate; and the rocket bracket (35) is drivingly connected to the third screw rod (34).

4. The offshore suspended rocket launching platform structure according to claim 3 is characterized in that: The launching assembly (6) further comprises a launching chamber (36), a launching signal block (37) and a launching induction block (38); the launching chamber (36) is mounted on the top of the rocket support (35); the launching signal block (37) is placed on the launching chamber (36); and the launching induction blocks (38) are placed on both sides of the launching chamber (36).

5. The offshore suspended rocket launching platform structure according to claim 4 is characterized in that: The feeding assembly (5) comprises a feeding seat (39), a feeding cylinder (40), a feeding hinge rod (41), a feeding buffer rod (42), a feeding frame (43) and a feeding push rod (44); the feeding seat (39) is slidably connected to the top of the rocket chamber (4); the feeding frame (43) is hinged to the top of the feeding seat (39); the two ends of the feeding hinge rod (41) are respectively hinged to the feeding seat (39) and the middle of the feeding frame (43); the feeding cylinder (40) is hinged to the feeding seat (39); the telescopic end of the feeding cylinder (40) is hinged to the middle of the feeding hinge rod (41); the feeding buffer rod (42) is placed in the middle of the feeding seat (39); and the feeding push rod (44) is symmetrically installed in the middle of the feeding frame (43).

6. The offshore suspended rocket launching platform structure according to claim 5 is characterized in that: A clamping block (45) is installed in the middle of the loading frame (43), and the clamping block (45) comprises a clamping frame (46), a clamping push rod (47) and a clamping sleeve (48). The clamping push rod (47) is slidably connected to the middle of the clamping frame (46), and the clamping sleeve (48) is placed on the top of the clamping frame (46).

7. The offshore suspended rocket launching platform structure according to claim 6 is characterized in that: A plurality of flow rate monitoring blocks are installed at the bottom of the floating assembly (3), and the flow rate monitoring blocks monitor the floating of the sea surface, control the rotation speed and direction of the propeller (18), and reduce the influence of the floating of the sea surface.

8. The offshore suspended rocket launching platform structure according to claim 7 is characterized in that: The clamping block (45) is detachably mounted on the loading rack (43), and the clamping block (45) further comprises a clamping ring (49), wherein the clamping ring (49) is mounted on the top of the clamping sleeve (48).

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