Water-entry separable umbrella cabin

By designing a water-separable parachute compartment, and utilizing an axial-flow rotor assembly and a screw-in structure to achieve mechanical separation of the compartment body and the bottom plate, the problems of complex structure and poor reliability in existing technologies are solved, and rapid and reliable separation of the parachute and the object is achieved.

CN115743555BActive Publication Date: 2025-11-28XIANGYANG HONGWEI AIRCRAFT
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Patent Information

Application Number
CN202211463437.X
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2022-11-22
Publication Date
2025-11-28
Estimated Expiration
2042-11-22

AI Technical Summary

Technical Problem

In existing technologies, the parachute separation mechanism of airdropped equipment after entering the water has a complex structure, requires a large number of electronic components, and has poor reliability.

Method used

Design a parachute cabin that can separate upon entering water. Utilize an axial flow rotor assembly to generate relative rotation between the cabin body and the bottom plate after entering the water due to the impact of water force. The separation is achieved through a screw-on structure. The density of the cabin body and the bottom plate is less than that of water to facilitate buoyancy.

Benefits of technology

It achieves fast and reliable separation of objects using a purely mechanical method, avoiding the use of electronic components and improving reliability.

✦ Generated by Eureka AI based on patent content.

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Abstract

The application discloses a water-entering separable umbrella cabin, which comprises a cabin body, a cabin bottom plate, a screw joint structure and an axial flow runner assembly, wherein the cabin body is fixedly connected with the canopy rope of a parachute, the cabin bottom plate is fixedly connected with an air-dropped heavy object, the screw joint structure is fixedly arranged between the cabin body and the cabin bottom plate, and the cabin body is screwed with the cabin bottom plate through the screw joint structure; the axial flow runner assembly is fixedly arranged on the cabin body or the cabin bottom plate, and the rotation center axis of the axial flow runner assembly is coincident with the axial direction of the cabin body or the cabin bottom plate. When the air-dropped heavy object enters water at a high speed, the axial flow runner assembly is impacted by water force to make the screwed cabin body and cabin bottom plate relatively rotate, so that the cabin body and the cabin bottom plate are rapidly released from the screwed state, the cabin bottom plate continuously falls under the action of inertia, and the cabin body and the cabin bottom plate are rapidly separated, so that the object-parachute separation is realized. The separation mode is a pure mechanical separation, and the reliability is high.
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Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of parachute pod, and particularly relates to a water-entering separation type parachute pod. BACKGROUND

[0002] In general, parachutes do not require forced separation from the ground, but there are some special cases, such as when deploying detection equipment in the ocean or lake for exploration or investigation, the equipment is air-dropped by a flying object in the air, and needs to be separated from the parachute as soon as possible after entering the water to facilitate underwater deployment of the equipment.

[0003] Application No. 201811538241.6 discloses a parachute separation mechanism for air-dropped equipment after entering the water, which has a complex structure and needs to use more electronic devices, and has poor reliability. SUMMARY

[0004] The present application aims to overcome the above technical deficiencies and provide a water-entering separation type parachute pod to solve the technical problems of the parachute separation mechanism for air-dropped equipment after entering the water in the prior art, which has a complex structure, needs to use more electronic devices, and has poor reliability.

[0005] To achieve the above technical purpose, the technical scheme of the present application provides a water-entering separation type parachute pod, which comprises a pod body, a pod bottom plate, a threaded structure and an axial flow runner assembly, the pod body is fixedly connected with the parachute rope of a parachute, the pod bottom plate is fixedly connected with an air-dropped weight, the threaded structure is fixedly arranged between the pod body and the pod bottom plate, and the pod body is threadedly connected with the pod bottom plate through the threaded structure; the axial flow runner assembly is fixedly arranged on the pod body or the pod bottom plate, and the rotational center axis of the axial flow runner assembly coincides with the axial direction of the pod body or the pod bottom plate.

[0006] After the axial flow runner assembly enters the water, it is subjected to hydraulic impact to cause relative rotation between the pod body and the pod bottom plate, so that the pod body and the pod bottom plate are separated from the threaded connection state.

[0007] Further, the threaded structure comprises a plurality of clamping grooves fixedly arranged at the bottom of the pod body and a plurality of protrusions fixedly arranged on the pod bottom plate and corresponding to the clamping grooves, and the protrusions are movably inserted into the corresponding clamping grooves.

[0008] Further, the threaded structure comprises an internal thread formed in the inner wall of the bottom of the pod body and an external thread formed on the top outer side of the pod bottom plate.

[0009] Further, the axial flow runner assembly comprises a plurality of blades, and the plurality of blades are distributed on the outer side of the pod body or the pod bottom plate in the circumferential direction.

[0010] Further, a plurality of the blades are fixedly arranged on the outer sidewall of the cabin body in a circumferential direction, and the blades are wing plates which are inclined to a vertical plane and fixedly arranged on the outer sidewall of the cabin body.

[0011] Further, the angle between the wing plate and the vertical plane is 5-10 degrees.

[0012] Further, the blades are plastic blades or wooden blades.

[0013] Further, the water-enterable separation umbrella cabin further comprises a plurality of umbrella connecting supports fixedly arranged on the inner wall of the top of the cabin body, for fixedly connecting with the umbrella rope of the parachute; the umbrella connecting support comprises two oppositely arranged supporting seats and a fixing rod fixedly connected between the two supporting seats.

[0014] Further, the density of the cabin body and the cabin bottom plate is less than the density of water.

[0015] Further, the cabin body and the cabin bottom plate are respectively a plastic cabin body and a plastic cabin bottom plate.

[0016] Compared with the prior art, the beneficial effects of the present application include:

[0017] When the water-enterable separation umbrella cabin is used to air-drop a heavy object into water at a high speed, the axial flow type runner assembly is subjected to hydraulic impact to cause the relative rotation between the screwed cabin body and the cabin bottom plate, so that the cabin body and the cabin bottom plate are quickly released from the screwed state, and the cabin bottom plate continuously falls under the action of inertia while the cabin body is decelerated by the parachute, so that the two are quickly separated, thereby realizing the separation of the object and the parachute, and the separation mode is a pure mechanical separation, and the reliability is high. BRIEF DESCRIPTION OF DRAWINGS

[0018] Figure 1 is a structural schematic view of a water-enterable separation umbrella cabin provided by the present application;

[0019] Figure 2 is a structural schematic view of a cabin body in an embodiment of the present application;

[0020] Figure 3 is a structural schematic view of a cabin bottom plate in an embodiment of the present application. DETAILED DESCRIPTION

[0021] In order to make the purpose, technical scheme and advantages of the present application more clear, the present application is further described in detail below in combination with the drawings and embodiments. It should be understood that the specific embodiments described herein are only used to explain the present application, and are not used to limit the present application.

[0022] The present application provides a water-enterable separation umbrella cabin, the structure of which is as shown in Figure 1As shown in the drawings, the water-enterable separation parachute cabin comprises a cabin body 1, a cabin bottom plate 2, a screw joint structure 3 and an axial flow runner assembly 4. The cabin body 1 is fixedly connected with the canopy rope of a parachute, the cabin bottom plate 2 is fixedly connected with an air-dropped heavy object, the screw joint structure 3 is fixedly arranged between the cabin body 1 and the cabin bottom plate 2, and the cabin body 1 is screwed with the cabin bottom plate 2 through the screw joint structure 3. The axial flow runner assembly 4 is fixedly arranged on the cabin body 1 or the cabin bottom plate 2, and the rotation center axis of the axial flow runner assembly 4 coincides with the axial direction of the cabin body and the cabin bottom plate.

[0023] After the axial flow runner assembly 4 enters water, the cabin body 1 and the cabin bottom plate 2 are relatively rotated due to water impact, so that the cabin body 1 and the cabin bottom plate 2 are separated from the screw joint state.

[0024] When the air-dropped heavy object enters water at a high speed, the axial flow runner assembly 4 is impacted by water to make the cabin body 1 and the cabin bottom plate 2 relatively rotate, so that the cabin body 1 and the cabin bottom plate 2 are quickly separated from the screw joint state, and the cabin bottom plate 2 continuously falls under the action of inertia while the cabin body 1 is slowed down by the parachute, so that the cabin body 1 and the cabin bottom plate 2 are quickly separated, thereby realizing the separation of the object and the parachute. The separation mode is a pure mechanical separation, and the reliability is high.

[0025] As shown in Figure 2 and Figure 3 respectively are the structural schematic diagrams of the cabin body and the cabin bottom plate in the embodiment of the present application. As a preferred embodiment, the screw joint structure 3 comprises a plurality of clamping grooves 31 fixedly arranged at the bottom of the cabin body 1 and a plurality of protrusions 32 fixedly arranged on the cabin bottom plate 2 and corresponding to the clamping grooves 31, and the protrusions 32 are movably inserted into the corresponding clamping grooves 31. Specifically, in order to facilitate the processing and production, the clamping grooves 31 are integrally formed with the cabin body 1, and the protrusions 32 are integrally formed with the cabin bottom plate 2.

[0026] It can be understood that when the cabin body 1 and the cabin bottom plate 2 relatively rotate, the protrusions 32 can be separated from the corresponding clamping grooves 31 to release the constraint, so that the cabin body 1 and the cabin bottom plate 2 are quickly separated.

[0027] It should be noted that the screw joint structure 3 is provided with the clamping grooves 31 and the protrusions 32 only as a preferred embodiment in this embodiment, and in other embodiments, the screw joint structure 3 can also comprise an internal thread formed in the inner wall of the bottom of the cabin body 1 and an external thread formed on the top outer side of the cabin bottom plate 2, and the internal thread can be engaged with the external thread. When the cabin body 1 and the cabin bottom plate 2 relatively rotate, the internal thread and the external thread are disengaged from the engagement state, so that the cabin body 1 and the cabin bottom plate 2 are separated.

[0028] Please continue to refer to Figure 2 As a preferred embodiment, the axial flow runner assembly 4 comprises a plurality of blades 40 which are circumferentially distributed on the outside of the cabin body 1 or the cabin floor. As a specific embodiment, the blades 40 are plastic blades or wooden blades, which can reduce the weight of the umbrella cabin.

[0029] It can be understood that the circumferential distribution of the blades 40 on the outside of the cabin body 1 or the cabin floor 2 can maximize the torque received by the cabin body 1 or the cabin floor 2 when the axial flow runner assembly 4 rotates, so that the cabin body 1 and the cabin floor 2 can be quickly separated in the shortest time.

[0030] In this embodiment, a plurality of blades 40 are circumferentially and uniformly fixed on the outer side wall of the cabin body 1. Specifically, the blades 40 are wing plates inclined to the vertical plane and fixed on the outer side wall of the cabin body 1.

[0031] As a preferred embodiment, considering that the wing plate will be subjected to a certain force when falling in the air and entering the water, in order to avoid the airflow force on the wing plate being too large in the air and causing the cabin body 1 and the cabin floor 2 to separate in the air, the angle between the wing plate and the vertical plane is 5°-10°, and the number of wing plates is 16.

[0032] As a preferred embodiment, the water-entering separable umbrella cabin further comprises a plurality of umbrella connecting supports 5 fixedly arranged on the inner wall of the top of the cabin body 1, for fixedly connecting with the parachute rope of the parachute; the umbrella connecting support 5 comprises two oppositely arranged supporting seats 51 and a fixed rod 52 fixedly connected between the two supporting seats 51.

[0033] As a preferred embodiment, the density of the cabin body 1 and the cabin floor 2 is less than the density of water. Specifically, the cabin body 1 and the cabin floor 2 are plastic cabin body and plastic cabin floor, respectively.

[0034] It can be understood that the density of the cabin body 1 and the cabin floor 2 is less than the density of water, which can make the cabin body 1 and the cabin floor 2 float in water, so as to facilitate the search for the air-dropped heavy object falling into the water.

[0035] In order to facilitate the understanding of the present application, the following will be combined with Figures 1-3 The working principle of the present scheme will be described in detail:

[0036] When the parachute cabin enters water at a faster speed, the axial flow runner assembly 4 is subjected to a water impact torque at the moment of entering water, which is transmitted to the cabin body 1 to drive the cabin body 1 to rotate, while the cabin bottom plate 2 only has a falling speed under the action of inertia, the water impact torque overcomes the friction between the clamping groove 31 and the protruding block 32, so that the clamping groove 31 rotates relative to the protruding block 32 (that is, the cabin body 1 rotates relative to the cabin bottom plate 2) to make the protruding block 32 be released from the corresponding clamping groove 31, at this time, the cabin bottom plate 2 continues to fall due to inertia, while the cabin body 1 is slowed down by the parachute, so that the cabin body 1 and the cabin bottom plate 2 are separated, that is, the object-parachute separation is realized.

[0037] The water-entering separable parachute cabin has the following beneficial effects:

[0038] When the parachute cabin enters water at a faster speed, the axial flow runner assembly 4 is subjected to a water impact torque at the moment of entering water, which is transmitted to the cabin body 1 to drive the cabin body 1 to rotate, while the cabin bottom plate 2 only has a falling speed under the action of inertia, the water impact torque overcomes the friction between the clamping groove 31 and the protruding block 32, so that the clamping groove 31 rotates relative to the protruding block 32 (that is, the cabin body 1 rotates relative to the cabin bottom plate 2) to make the protruding block 32 be released from the corresponding clamping groove 31, at this time, the cabin bottom plate 2 continues to fall due to inertia, while the cabin body 1 is slowed down by the parachute, so that the cabin body 1 and the cabin bottom plate 2 are separated, that is, the object-parachute separation is realized.

[0039] The specific embodiments of the application described above do not constitute a limitation on the scope of protection of the application. Any various other corresponding changes and modifications made according to the technical concept of the application shall be included in the scope of protection of the claims of the application.

Claims

1. A water-landable pod, characterized in that, The application relates to a parachute cabin assembly, which comprises a cabin body, a cabin bottom plate, a screw joint structure and an axial flow runner assembly. The axial flow runner assembly is impacted by water to make the cabin body and the cabin bottom plate relatively rotate and separate from the screw joint state. The screw joint structure comprises a plurality of clamping grooves fixedly arranged on the bottom of the cabin body and a plurality of protrusions fixedly arranged on the cabin bottom plate and corresponding to the clamping grooves. The axial flow runner assembly comprises a plurality of blades, and the blades are circumferentially distributed on the outer side of the cabin body or the cabin bottom plate. The blades are circumferentially and uniformly fixedly arranged on the outer side wall of the cabin body, and the blades are wing plates which are inclined to the vertical plane and fixedly arranged on the outer side wall of the cabin body.

2. A water-entry separable umbrella pod according to claim 1, wherein, The screw joint structure comprises an inner thread formed on the inner wall of the bottom of the cabin body and an outer thread formed on the top outer side of the cabin bottom plate.

3. A water-entry separable umbrella pod according to claim 1, wherein, The angle between the wing plate and the vertical plane is 5-10 degrees.

4. A water-entry separable umbrella pod according to claim 1, wherein, The blades are plastic blades or wooden blades.

5. A water-entry separable umbrella pod according to claim 1, wherein, The parachute cabin assembly further comprises a plurality of parachute connecting supports fixedly arranged on the inner wall of the top of the cabin body and used for being fixedly connected with the parachute ropes, and the parachute connecting supports comprise two oppositely arranged supporting seats and a fixing rod fixedly connected between the two supporting seats.

6. A water-entry separable umbrella pod according to claim 1, wherein, The density of the cabin body and the cabin bottom plate is less than the density of water.

7. A water-entry separable umbrella pod according to claim 1, wherein, The cabin body and the cabin bottom plate are plastic cabin bodies and plastic cabin bottom plates respectively.

Citation Information

Patent Citations

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    CN109398653B

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    CN204124371U

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