Hydrofoil for water traffic tool
By using a modularly designed forewing and aftwing structure, combined with carbon fiber materials and three-dimensional weaving technology, the problems of large transport volume, heavy weight, low assembly efficiency, and high flight resistance of hydrofoils have been solved, resulting in enhanced structural stability and improved flight efficiency.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- ROYAL WATER FLYING (SHENZHEN) TECHNOLOGY CO LTD
- Filing Date
- 2025-04-29
- Publication Date
- 2026-04-21
AI Technical Summary
Existing hydrofoil designs suffer from problems such as large transport volume, heavy weight, low assembly efficiency, insufficient structural stability, and high sailing resistance.
The modular design of the forewing and aftwing structures, combined with carbon fiber materials and three-dimensional weaving technology, enables modular assembly of the forewing and aftwing through the cooperation of support components and fittings, thereby enhancing structural stability and reducing flight drag.
This has resulted in reduced transport volume, improved on-site assembly efficiency, enhanced structural stability, and reduced sailing resistance, thereby improving the hydrodynamic performance of high-speed vessels.
Smart Images

Figure CN224146109U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of hydrofoils, and in particular to a hydrofoil for water transportation vehicles. Background Technology
[0002] Water transport generally refers to vehicles that travel on water. There are various types of water transport, including ships, boats, rafts, and hydrofoils. Among them, hydrofoils are usually boats with hydrofoils that are submerged in water. When traveling at high speeds, the weight of the boat is entirely supported by the lift generated by the water on the hydrofoils, which makes the entire hull leave the water surface, reducing water resistance and thus achieving higher speeds.
[0003] Hydrofoils typically consist of a front wing and a rear wing. Existing front and rear wings usually have the following disadvantages: (1) They are assembled as a single unit on the hydrofoil boat, which increases the transport volume and affects the on-site assembly efficiency. They also have a large weight. Therefore, it is necessary to design the hydrofoil in a modular assembly manner to reduce the transport volume and improve the on-site assembly efficiency; (2) The structural stability is insufficient; (3) The sailing resistance is large. Utility Model Content
[0004] The purpose of this invention is to provide a hydrofoil for water transportation vehicles to solve the problems mentioned in the background art.
[0005] To achieve the above objectives, this utility model provides the following technical solution: a hydrofoil for water transportation vehicles, comprising:
[0006] A forewing structure, wherein a first support member is provided inside the forewing structure, and the forewing structure is U-shaped;
[0007] The rear wing structure is symmetrically arranged with adjacent rear wing structures. The rear wing structure is provided with a second support member inside. The rear wing structure is C-shaped. The leading edge and trailing edge of both the front wing structure and the rear wing structure are streamlined curves.
[0008] The first assembly is located on the forewing structure and is used to assemble and fix the forewing structure.
[0009] The second assembly is located on the rear wing structure and is used to assemble and fix the rear wing structure.
[0010] Preferably, the forewing structure includes:
[0011] The support portion, wherein the first support member is located at the top of the support portion;
[0012] A support portion, wherein the support portion is located on the side of the support portion;
[0013] The first arc-shaped portion, the supporting portion is connected to the supporting portion through the first arc-shaped portion;
[0014] The second arc-shaped portion is located at the top of the support portion, and the first fitting is located at the end of the second arc-shaped portion.
[0015] Preferably, the rear wing structure includes:
[0016] The receiving part, wherein the second support member is located at the top of the receiving part;
[0017] The connecting part is disposed at the top of the receiving part, and the second fitting is located at the end of the connecting part;
[0018] The third arc-shaped portion, wherein the connecting portion is connected to the receiving portion through the third arc-shaped portion;
[0019] The fourth arc-shaped portion is located on the side of the receiving portion.
[0020] Preferably, the first support member includes:
[0021] A support body, the support body being fixed to the top of the support portion, the top of the support body being provided with a fifth arc-shaped portion;
[0022] A wedge block, which is fixedly connected to the end of the fifth arc-shaped portion.
[0023] Preferably, the first assembly includes:
[0024] An assembly frame is fixedly connected to the end of the second arc-shaped portion, and the assembly frame has a first cavity inside;
[0025] Positioning holes are provided at the top and bottom of the assembly frame.
[0026] Preferably, the second assembly includes:
[0027] A connecting frame is fixedly connected to the end of the connecting part, and the connecting frame has a second cavity inside;
[0028] Mounting holes are provided at the top and bottom of the connecting frame.
[0029] Preferably, the second support member includes:
[0030] The carrier is fixedly connected to the top of the receiving part;
[0031] A wedge-shaped column is fixedly connected to the top of the support body.
[0032] The technical effects and advantages of this utility model are as follows:
[0033] This utility model utilizes the cooperation of a front wing structure, a rear wing structure, a first support member, a second support member, a first assembly member, and a second assembly member. The front wing structure and the rear wing structure are modularly designed. The first and second support members support the connection between the front wing structure and the rear wing structure. The first and second assembly members enable the front wing structure and the rear wing structure to be directly installed on the hydrofoil, which facilitates modular assembly design, reduces transportation volume, and improves on-site assembly efficiency. It is suitable for the hydrodynamic performance optimization requirements of high-speed ships. At the same time, by setting the first and second support members, it helps to enhance structural stability, improve navigation efficiency, reduce resistance, reduce wave impact, and has a simple structure that is easy to manufacture and maintain. Attached Figure Description
[0034] Figure 1 This is a schematic diagram of the overall structure of this utility model.
[0035] Figure 2 This is a schematic diagram of the front wing structure of this utility model.
[0036] Figure 3 This is a schematic diagram of the rear wing structure of this utility model.
[0037] In the diagram: 1. Forward wing structure; 11. Support part; 12. Supporting part; 13. First arc-shaped part; 14. Second arc-shaped part; 2. Rear wing structure; 21. Supporting part; 22. Connecting part; 23. Third arc-shaped part; 24. Fourth arc-shaped part; 3. First support member; 31. Support body; 32. Fifth arc-shaped part; 33. Wedge block; 4. First assembly; 41. Assembly frame; 42. First cavity; 43. Positioning hole; 5. Second assembly; 51. Connecting frame; 52. Second cavity; 53. Mounting hole; 6. Second support member; 61. Bearing body; 62. Wedge column. Detailed Implementation
[0038] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.
[0039] This utility model provides, for example Figure 1-3The hydrofoil shown is for a waterborne vehicle and includes a front wing structure 1, a rear wing structure 2, a first assembly 4, and a second assembly 5. The front wing structure 1, rear wing structure 2, first support member 3, first assembly 4, second assembly 5, and second support member 6 are integrally molded from carbon fiber material. The manufacturing method of the front wing structure 1, rear wing structure 2, first assembly 4, and second assembly 5 involves carbon fiber lay-up, vacuum sealing, and high-temperature curing in an autoclave. Internally, it incorporates two 30mm wide foamed reinforcing support beams, which are compositely molded using a foaming process and structural adhesive bonding. Innovatively, three-dimensional woven carbon fiber prepreg is used to fabricate the main load-bearing components. Through topology optimization design, an equal-strength structural distribution is achieved. This structure features high strength, light weight, and long service life. The front wing structure 1 has a first support member 3 inside, which facilitates connection with the hydrofoil and supports the connection of the front wing structure 1. The front wing structure 1 is U-shaped, and the adjacent rear wing structure 2 is symmetrically arranged. The rear wing structure 2... The internal structure is equipped with a second support member 6, which facilitates the support between the hydrofoil and the rear wing structure 2. The rear wing structure 2 is C-shaped. The first assembly 4 is located on the front wing structure 1 and is used to assemble and fix the front wing structure 1. The first assembly 4 and the second assembly 5 are directly plugged into the hydrofoil and locked with bolts, which facilitates disassembly, replacement and maintenance. The front wing structure 1 and the rear wing structure 2 adopt a modular design, which helps to reduce the transportation area and facilitates operation. The second assembly 5 is located on the rear wing structure 2 and is used to assemble and fix the rear wing structure 2. The front wing structure 1 and the rear wing structure 2 adopt an advanced hydrodynamic airfoil design. When sailing at a certain speed, it generates lift to reduce drag and turbulence. The streamlined curves of the leading and trailing edges reduce water flow separation and eddy generation. When the hydrofoil is cruising at high speed on calm sea surface, the improved hydrofoil is deployed to the maximum height and the angle of attack is adjusted to 5° to generate maximum lift. The hull is completely lifted off the water surface, the drag is significantly reduced and the sailing efficiency is improved by 20%.
[0040] Furthermore, the front wing structure 1 includes a support portion 11, a support portion 12, a first arc-shaped portion 13, and a second arc-shaped portion 14. The first support member 3 is located on the top of the support portion 11, the support portion 12 is located on the side of the support portion 11, the support portion 12 is connected to the support portion 12 through the first arc-shaped portion 13, the second arc-shaped portion 14 is located on the top of the support portion 12, and the first mounting part 4 is located at the end of the second arc-shaped portion 14.
[0041] Furthermore, the rear wing structure 2 includes a receiving part 21, a connecting part 22, a third arc-shaped part 23, and a fourth arc-shaped part 24. The second support member 6 is located on the top of the receiving part 21, the connecting part 22 is disposed on the top of the receiving part 21, the second fitting 5 is located at the end of the connecting part 22, the connecting part 22 is connected to the receiving part 21 through the third arc-shaped part 23, and the fourth arc-shaped part 24 is located on the side of the receiving part 21.
[0042] Specifically, the first support member 3 includes a support body 31 and a wedge block 33. The support body 31 is inserted into the bottom of the hydrofoil via the wedge block 33, which facilitates the support and reinforcement of the forewing structure 1 and the hydrofoil. The support body 31 is fixed to the top of the support part 11. The top of the support body 31 is provided with a fifth arc-shaped part 32, and the wedge block 33 is fixedly connected to the end of the fifth arc-shaped part 32.
[0043] Specifically, the first assembly 4 includes an assembly frame 41 and a positioning hole 43. The hydrofoil has a groove that matches the assembly frame 41. The positioning hole 43 facilitates connection with external bolts, thereby facilitating bolt installation and fixing of the forewing structure 1 to the hydrofoil, which is convenient for operation. The assembly frame 41 is fixedly connected to the end of the second arc-shaped part 14. The assembly frame 41 has a first cavity 42 inside. The positioning hole 43 is opened at the top and bottom of the assembly frame 41.
[0044] Specifically, the second assembly 5 includes a connecting frame 51 and mounting holes 53. The hydrofoil has a groove adapted to the connecting frame 51. The mounting holes 53 facilitate connection with external bolts, thereby facilitating the locking of the rear wing structure 2 to the hydrofoil and achieving assembly. The connecting frame 51 is fixedly connected to the end of the connecting part 22. The connecting frame 51 has a second cavity 52 inside. The mounting holes 53 are opened at the top and bottom of the connecting frame 51.
[0045] Specifically, the second support member 6 includes a carrier 61 and a wedge-shaped column 62. The carrier 61 is conducive to supporting the rear wing structure 2 and the hydrofoil. The wedge-shaped column 62 is conducive to being inserted into the hydrofoil to position the installation of the carrier 61. The carrier 61 is fixedly connected to the top of the receiving part 21, and the wedge-shaped column 62 is fixedly connected to the top of the carrier 61.
[0046] Finally, it should be noted that the above description is only a preferred embodiment of the present utility model and is not intended to limit the present utility model. Although the present utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions for some of the technical features. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present utility model should be included within the protection scope of the present utility model.
Claims
1. A hydrofoil for a watercraft, characterized in that, include: A forewing structure (1) is provided inside the forewing structure (1), and the forewing structure (1) is U-shaped; The rear wing structure (2) is symmetrically arranged with adjacent rear wing structures (2). The interior of the rear wing structure (2) is provided with a second support member (6). The rear wing structure (2) is C-shaped. The leading edge and trailing edge of the front wing structure and the rear wing structure are both streamlined curves. First assembly (4), the first assembly (4) is located on the forewing structure (1), the first assembly (4) is used to assemble and fix the forewing structure (1); The second assembly (5) is located on the rear wing structure (2) and is used to assemble and fix the rear wing structure (2).
2. A hydrofoil for a watercraft according to claim 1, wherein, The forewing structure (1) includes: Support (11), the first support member (3) is located on top of the support (11); The support portion (12) is located on the side of the support portion (11); The first arc-shaped portion (13) is connected to the support portion (12) through the first arc-shaped portion (13); The second arc-shaped portion (14) is located at the top of the support portion (12), and the first fitting (4) is located at the end of the second arc-shaped portion (14).
3. A hydrofoil for a watercraft according to claim 1, wherein The rear wing structure (2) includes: The receiving part (21) has the second support member (6) located on top of the receiving part (21); A connecting part (22) is provided on the top of the receiving part (21), and the second assembly (5) is located at the end of the connecting part (22); The third arc-shaped portion (23) is used to connect the connecting portion (22) to the receiving portion (21). The fourth arc-shaped part (24) is located on the side of the receiving part (21).
4. A hydrofoil for a watercraft according to claim 2, wherein The first support member (3) includes: A support body (31) is fixed to the top of the support part (11), and the top of the support body (31) is provided with a fifth arc-shaped part (32); A wedge block (33) is fixedly connected to the end of the fifth arc-shaped part (32).
5. A hydrofoil for a watercraft according to claim 2, wherein The first assembly (4) includes: Assembly frame (41), the assembly frame (41) is fixedly connected to the end of the second arc-shaped part (14), and the assembly frame (41) has a first cavity (42) inside; Positioning holes (43) are provided at the top and bottom of the assembly frame (41).
6. A hydrofoil for a watercraft according to claim 3, wherein The second assembly (5) includes: A connecting frame (51) is fixedly connected to the end of the connecting part (22), and a second cavity (52) is provided inside the connecting frame (51); Mounting holes (53) are provided at the top and bottom of the connecting frame (51).
7. A hydrofoil for a watercraft according to claim 3, wherein The second support member (6) includes: The carrier (61) is fixedly connected to the top of the receiving part (21); A wedge-shaped column (62) is fixedly connected to the top of the support body (61).