Carrying platform

Abstract

The utility model discloses a carrying platform. The device comprises a front cabin, the front cabin comprises a head section and a column section, and the column section is arranged at the bottom of the head section; a forward booster is mounted in the head section; a releasable device is mounted in the column section; the rear cabin is arranged at the bottom of the column section and connected with the column section; a test control system is arranged in the rear cabin and used for monitoring the environment where the carrying platform is located in real time. A charging engine is installed in the rear cabin and used for providing floating power for the carrying platform. And a reverse booster is also mounted in the rear cabin. The carrying platform floats up underwater through power provided by a charging engine, and equipment installed in the column section can leave the column section to be disintegrated and released after water is discharged. According to the carrying platform, the problem that cross-medium transportation cannot be achieved due to the fact that the self weight of cross-medium equipment is too large due to sealing and pressure bearing is solved.

Description

Technical Field

[0001] This utility model relates to the field of cross-medium transport platform technology, and more specifically, to a cross-medium underwater transport platform. Background Technology

[0002] Currently, water-to-air cross-medium products mainly include cross-medium aircraft and various cross-medium military equipment. These products typically achieve underwater sealing and pressure resistance through their structural design, resulting in significant weight and placing high demands on power and flight capabilities. Conventional transport platforms often struggle to transport such heavy equipment across media. Existing technologies for aerial separation of equipment and transport platforms employ two methods: hot separation and cold separation. Hot separation involves the front end of the transport platform detaching after aerial separation conditions are met, ejecting the equipment. While this method offers the advantage of controllable separation, the ejection process places high demands on the equipment's shock absorption, heat insulation, and fire resistance. Cold separation involves the front end of the transport platform detaching after aerial separation conditions are met, with the equipment sliding off the platform without power. This process is time-consuming and occurs in an uncontrolled state.

[0003] There are currently no effective solutions to the problems of high requirements for vibration reduction, heat insulation and fire prevention in existing technologies for thermal separation, as well as the long separation time and uncontrolled separation process in cold separation. Utility Model Content

[0004] This utility model provides a transport platform to solve the problems in the prior art where hot separation has high requirements for equipment in terms of shock absorption, heat insulation and fire prevention, and cold separation has a long separation time and is in an uncontrolled state during separation.

[0005] To achieve the above objectives, this utility model provides a transport platform, comprising: a front compartment, which includes a nose section and a column section, the column section being located at the bottom of the nose section; a forward booster installed within the nose section; and a releasable device installed within the column section; a rear compartment, located at the bottom of and connected to the column section; a test and control system installed within the rear compartment for real-time monitoring of the environment in which the transport platform is located; a propellant-loading engine installed within the rear compartment for providing upward propulsion for the transport platform; and a reverse booster also installed within the rear compartment.

[0006] Optionally, a heat insulation layer is provided inside the head section to isolate the internal cavity of the head section into a double-layer nested structure.

[0007] Optionally, the positive booster is installed between the front inner wall of the head section and the heat insulation layer.

[0008] Optionally, the head segment has an oval structure.

[0009] Optionally, a cutting separator is provided at the top and bottom of the column segment, respectively, for separating the head segment from the column segment and separating the column segment from the rear compartment.

[0010] Optionally, the reverse booster is located inside the top of the aft compartment; the test control system is located inside the middle of the aft compartment; and the propellant loading engine is located inside the tail of the aft compartment.

[0011] Optionally, wing panels are evenly distributed on the outer rear of the aft compartment.

[0012] Optionally, the rear section of the aft compartment has a conical structure.

[0013] Optionally, the front compartment is mounted on top of the rear compartment by screws.

[0014] Optionally, a sealing ring is provided between the front compartment and the rear compartment.

[0015] The beneficial effects of this utility model are:

[0016] This utility model provides a transport platform comprising: a front compartment, which includes a head section and a column section, the column section being located at the bottom of the head section; a forward booster installed within the head section; and releasable equipment installed within the column section; a rear compartment, located at the bottom of and connected to the column section; a test and control system installed within the rear compartment for real-time monitoring of the environment in which the transport platform is located; a propellant-loading engine installed within the rear compartment for providing buoyancy power to the transport platform; and a reverse booster also installed within the rear compartment. This transport platform ascends from underwater using power provided by the propellant-loading engine, and the equipment installed within the column section can be disassembled and released after surfacing. The transport platform achieves separation via the propellant-loading engine, featuring short separation time, controllable separation, and low requirements for shock absorption, heat insulation, and fire prevention. This transport platform solves the problem of cross-medium equipment being unable to be transported across media due to excessive weight from sealing and pressure bearing zones. Attached Figure Description

[0017] Figure 1 This is a schematic diagram of the structure of the transport platform provided in this embodiment of the utility model;

[0018] Figure 2 This is a schematic diagram of the front cabin structure provided in an embodiment of the present invention;

[0019] Figure 3 This is a schematic diagram of the head section structure provided in an embodiment of the present invention;

[0020] Figure 4 This is a schematic diagram of the column segment provided in an embodiment of the present invention;

[0021] Figure 5 This is a structural schematic diagram of the rear compartment provided in an embodiment of the present utility model.

[0022] Symbol explanation:

[0023] Forward compartment-1, rear compartment-2, nose section-11, column section-12, heat insulation layer-111, forward booster-112, cutting separator-121, equipment-122, test control system-21, propellant engine-22, reverse booster-23, wing panel-24. Detailed Implementation

[0024] To make the objectives, technical solutions, and advantages of this utility model clearer, the present utility model will be further described in detail below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of this utility model, and not all embodiments. Based on the embodiments of this utility model, all other embodiments obtained by those skilled in the art without creative effort are within the protection scope of this utility model.

[0025] Currently, water-to-air cross-medium products mainly include cross-medium aircraft and various cross-medium military equipment. These products typically achieve underwater sealing and pressure resistance through their structural design, resulting in significant weight and placing high demands on power and flight capabilities. Conventional transport platforms often struggle to transport such heavy equipment across media. Existing technologies for aerial separation of equipment and transport platforms employ two methods: hot separation and cold separation. Hot separation involves the front end of the transport platform detaching after aerial separation conditions are met, ejecting the equipment. While this method offers the advantage of controllable separation, the ejection process places high demands on the equipment's shock absorption, heat insulation, and fire resistance. Cold separation involves the front end of the transport platform detaching after aerial separation conditions are met, with the equipment sliding off the platform without power. This process is time-consuming and occurs in an uncontrolled state.

[0026] Therefore, this utility model provides an underwater transport platform that can accommodate and carry various cross-medium devices 122. The platform enables water-to-air cross-medium transport, solving the problem that cross-medium devices 122 cannot be transported across media due to excessive weight of their seals and pressure bearings. Furthermore, the platform has low requirements for shock absorption, heat insulation, and fire prevention of the equipment, and the separation time is short and the separation is controllable.

[0027] Figure 1 This is a schematic diagram of the structure of the transport platform provided in this embodiment of the utility model, as shown below. Figure 1 As shown, the launch platform includes:

[0028] Front cabin 1, Figure 2 This is a structural schematic diagram of the front compartment 1 provided in an embodiment of this utility model, as shown below. Figure 2As shown, the front compartment 1 includes: a head section 11 and a column section 12, wherein the column section 12 is located at the bottom of the head section 11;

[0029] Figure 3 This is a schematic diagram of the structure of the head segment 11 provided in this embodiment of the utility model, as shown below. Figure 3 As shown, the head section 11 is an oval structure with a curve; a positive booster 112 is installed inside the head section 11;

[0030] Furthermore, a heat insulation layer 111 is provided within the head section 11 to isolate the internal cavity of the head section 11 into a double-layer nested structure. The forward booster 112 is installed between the front inner wall of the head section 11 and the heat insulation layer 111, and both the front of the head section 11 and the heat insulation layer 111 have curved structures. In a specific embodiment of this utility model, two forward boosters 112 are provided. When the forward booster 112 is working, it can cause the carrier platform to move upward with a small force.

[0031] Figure 4 This is a structural schematic diagram of the column segment 12 provided in an embodiment of this utility model, as shown below. Figure 4 As shown, the column segment 12 is a cylindrical structure with a hollow interior and a releasable device 122 installed inside. A cutting separator 121 is provided at the top of the column segment 12 to separate the head segment 11 from the column segment 12. A cutting separator 121 is provided at the bottom of the column segment 12 to separate the column segment 12 from the component connected to the bottom.

[0032] Rear cabin 2, Figure 5 This is a structural schematic diagram of the rear compartment 2 provided in an embodiment of this utility model, as shown below. Figure 5 As shown, the rear cabin 2 is located at the bottom of the column section 12 and connected to it;

[0033] Specifically, the front compartment 1 (the column segment 12 of the front compartment 1) is mounted on the top of the rear compartment 2 with screws. Furthermore, a sealing ring is provided between the front compartment 1 and the rear compartment 2 to provide a seal.

[0034] A test control system 21 is installed in the rear compartment 2 to monitor the environment of the transport platform in real time and control the timing of the transport platform's actions; a grenades engine 22 is installed in the rear compartment 2 to provide the transport platform with the power to float upwards; a reverse booster 23 is also installed in the rear compartment 2, which can push the cut rear compartment 2 downwards when it is working.

[0035] Specifically, the reverse booster 23 is located inside the top of the aft compartment 2; the test control system 21 is located inside the middle of the aft compartment 2; and the propellant-loading engine 22 is located inside the tail of the aft compartment 2. The tail of the aft compartment 2 has a conical structure, and winglets 24 are evenly distributed on the outer side of the tail of the aft compartment 2.

[0036] The working principle of this utility model is explained below through a specific embodiment:

[0037] After the launch platform exits the vertical tube, the test control system 21 located in the aft compartment 2 collects and judges its environmental information. Once the specified conditions are met, the test control system 21 issues an ignition signal to start the propellant loading engine 22 in the aft compartment 2. The propellant loading engine 22 ignites to provide thrust, pushing the launch platform out of the water before shutting down. When the test control system 21 detects the entry of air, it sends a positive thrust signal to the forward booster 112 in the head section 11 of the front compartment 1. The forward booster 112 starts working, giving the launch platform a slight upward force. Shortly after, the test control system 21 issues a separation signal to the cutting separator 121, which cuts and separates the launch platform into three parts: the head section 11, the column section 12, and the aft compartment 2. Simultaneously, the test control system 21 issues a reverse booster 23 to perform a reverse thrust, accelerating the cut aft compartment 2 downwards and releasing the equipment 122 inside the column section 12.

[0038] Currently, products that separate cold and heat require high levels of ballistic control and thermal insulation, resulting in high costs. However, the transport platform of this invention can withstand high pressure at great depths, does not have pressure-bearing and sealing requirements for internal equipment, and does not suffer from the problems associated with cold and heat separation.

[0039] The beneficial effects of this utility model are:

[0040] This utility model provides a transport platform, comprising: a front compartment 1, which includes a head section 11 and a column section 12, the column section 12 being located at the bottom of the head section 11; a forward booster 112 installed within the head section 11; and a releasable device 122 installed within the column section 12; a rear compartment 2, located at the bottom of and connected to the column section 12; a test and control system 21 installed within the rear compartment 2 for real-time monitoring of the environment in which the transport platform is located; a propellant-loading engine 22 installed within the rear compartment 2 for providing buoyancy power to the transport platform; and a reverse booster 23 also installed within the rear compartment 2. The transport platform rises from underwater using power provided by the propellant-loading engine 22, and the device 122 installed within the column section 12 can be disassembled and released after surfacing. The transport platform achieves separation through the loading engine 22, which has the characteristics of short separation time and controllable separation, and does not have high requirements for shock absorption, heat insulation and fire prevention. The transport platform solves the problem that the cross-medium equipment 122 cannot be transported across media due to the excessive weight of the seal and pressure belt.

[0041] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of this utility model, and not to limit it. Although this utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art should understand that modifications can still be made to the technical solutions described in the foregoing embodiments, or equivalent substitutions can be made to some of the technical features. Such modifications or substitutions do not cause the essence of the corresponding technical solutions to deviate from the spirit and scope of the technical solutions of the embodiments of this utility model.

Claims

1. A carrier platform characterized by, The utility model relates to a carrying platform, which comprises: a front cabin, which comprises a head section and a column section arranged at the bottom of the head section; a forward booster is arranged in the head section; a releasable device is arranged in the column section; a rear cabin arranged at the bottom of the column section and connected with the column section; a test control system is arranged in the rear cabin for monitoring the environment in which the carrying platform is located in real time; a charge engine is arranged in the rear cabin for providing power for the carrying platform to float upwards; and a reverse booster is arranged in the rear cabin.

2. The carrying platform according to claim 1, wherein: a heat insulation layer is arranged in the head section for isolating the internal cavity of the head section into a double-layer nested structure.

3. The carrying platform according to claim 2, wherein: the forward booster is arranged between the front inner wall of the head section and the heat insulation layer.

4. The carrying platform according to claim 2, wherein: the head section is in an oval structure.

5. The carrying platform according to claim 1, wherein: cutting separators are arranged at the top and bottom of the column section respectively for separating the head section from the column section and separating the column section from the rear cabin.

6. The carrying platform according to claim 1, wherein: the reverse booster is arranged at the top of the rear cabin; the test control system is arranged in the middle of the rear cabin; and the charge engine is arranged at the tail of the rear cabin.

7. The carrying platform according to claim 6, wherein: wing plates are uniformly distributed at the tail of the rear cabin.

8. The carrying platform according to claim 7, wherein: the tail of the rear cabin is in a conical structure.

9. The carrying platform according to claim 1, wherein: the front cabin is arranged at the top of the rear cabin by means of screws.

10. The carrying platform according to claim 1, wherein: a sealing ring is arranged between the front cabin and the rear cabin.

Images