A high seal turbine casing seal sleeve

CN224849900UActive Publication Date: 2026-10-13WUXI DESKY POWER TECH CO LTD
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Patent Information

Application Number
CN202522659647.1
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-12-16
Publication Date
2026-10-13
Estimated Expiration
2035-12-16

AI Technical Summary

Technical Problem

[0004]本实用新型的目的在于提供一种高密封涡轮壳密封套,以解决现有技术中密封外衬套内部结构强度较差,易过度形变损坏影响密封效果的问题

Benefits of technology

本实用新型利用密封外衬套内设有的内撑加强件,内撑加强件和限位凸起均为合金件,增加了密封外衬套内部的结构强度,防止密封外衬套过度形变损坏影响密封效果。

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model discloses a kind of high sealing turbine shell sealing sleeve, including sealing outer bush and inner bush, sealing outer bush is equipped with inner support reinforcement in, the inner support reinforcement is equipped with limit protrusion in, inner bush includes the inner core sleeve of being equipped with, the first sealing ring and second sealing ring are equipped with in the inner core sleeve two sides, clamping groove is formed between inner core sleeve, first sealing ring and second sealing ring, and inner bush is clamped in the inner and outer wall of sealing outer bush by clamping groove, the utility model is equipped with the inner support reinforcement in sealing outer bush, increase the structural strength inside sealing outer bush, prevent sealing outer bush excessive deformation influence sealing effect, and inner bush is clamped in the inner and outer wall of sealing outer bush by clamping groove, utilize inner bush can be sealed to the inner wall of the connecting gap between turbine shell and shell cover, it is favorable to improve the sealing property of turbine shell and shell cover installation fixation.
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Description

Technical Field

[0001] This utility model relates to the field of sealing sleeve technology, specifically a high-sealing turbine housing sealing sleeve. Background Technology

[0002] A turbine is a fan in a car or airplane engine that uses exhaust gases to blow fuel vapor into the engine, thereby improving engine performance. A turbine is a rotating power machine that converts the energy of a flowing working fluid into mechanical work. It is one of the main components of aircraft engines, gas turbines, and steam turbines. A sealing sleeve is needed during the installation and fixing of the turbine housing and cover to improve the stability and sealing of the housing installation.

[0003] A prior art patent application (application number 202423223730.6) describes a high-stability, leak-proof turbine housing sealing sleeve. The sleeve includes a sealing body comprising a first outer half-ring and a first inner half-ring. A second outer half-ring is inserted into one end of the first outer half-ring. Both the first and second outer half-rings contain a first reinforcing member, with a first insertion plate at one end and a first insertion groove at the other. The sealing sleeve's internal structure has high strength, strong resistance to compression, and good sealing performance, thus extending its service life. Furthermore, when the sealing sleeve is severely damaged locally, only the semi-circular sealing sleeve needs to be replaced, improving resource utilization and facilitating energy conservation. However, the internal structure of the outer sealing sleeve is relatively weak and prone to excessive deformation, affecting the sealing effect. Utility Model Content

[0004] The purpose of this utility model is to provide a high-sealing turbine housing sealing sleeve to solve the problem that the internal structure of the sealing outer bushing in the prior art is of poor strength and is easily damaged by excessive deformation, which affects the sealing effect.

[0005] To achieve the above objectives, this utility model provides the following technical solution: a high-sealing turbine housing sealing sleeve, comprising an outer sealing bushing and an inner bushing, wherein the outer sealing bushing is provided with an inner support reinforcement member, and the inner side of the inner support reinforcement member is provided with a limiting protrusion; the inner bushing includes an inner core sleeve, and the inner core sleeve is provided with a first sealing ring and a second sealing ring on both sides; a snap-fit ​​groove is formed between the inner core sleeve, the first sealing ring and the second sealing ring, and the inner bushing is snap-fitted to the inner and outer walls of the outer sealing bushing through the snap-fit ​​groove.

[0006] Furthermore, the inner core sleeve, the first sealing ring, and the second sealing ring are integrally formed, and all three are elastic rubber structures.

[0007] Furthermore, the snap-fit ​​groove is configured as an arc-shaped groove, and the width of the snap-fit ​​groove is equal to the thickness of the sealing outer bushing.

[0008] Furthermore, the inner core sleeve has a limiting hole on its side wall, and the limiting hole is engaged with the limiting protrusion.

[0009] Furthermore, both the inner support reinforcement and the limiting protrusion are alloy parts, and multiple limiting protrusions are arranged in a ring array on the inner wall of the inner support reinforcement.

[0010] Furthermore, the sealing outer bushing has positioning holes inside, and multiple positioning holes are provided at equal angles.

[0011] Compared with the prior art, the beneficial effects of this utility model are: This utility model utilizes an internal support reinforcement inside the sealing outer bushing. Both the internal support reinforcement and the limiting protrusion are alloy parts, which increases the structural strength inside the sealing outer bushing and prevents excessive deformation of the sealing outer bushing from affecting the sealing effect.

[0012] This utility model utilizes a first sealing ring and a second sealing ring provided on both sides of the inner core sleeve. A snap-fit ​​groove is formed between the inner core sleeve, the first sealing ring, and the second sealing ring. The inner liner is snapped onto the inner and outer walls of the sealing outer liner through the snap-fit ​​groove. The inner liner can seal the inner wall of the connection gap between the turbine housing and the housing cover, which helps to improve the sealing performance of the turbine housing and housing cover installation and fixation.

[0013] This utility model utilizes a limiting protrusion on the inner side of the inner support reinforcement and a limiting hole on the side wall of the inner core sleeve. The limiting hole and the limiting protrusion are interlocked, which facilitates the improvement of the stability of the inner core sleeve on the outer wall of the sealing outer bushing. Moreover, the inner bushing can be removed when not in use, which improves the flexibility of bushing use. Attached Figure Description

[0014] The accompanying drawings are provided to further illustrate the present invention and form part of the specification. They are used together with the embodiments of the present invention to explain the present invention, but do not constitute a limitation thereof. In the drawings: Figure 1 This is a schematic diagram of the overall structure of this utility model; Figure 2 This is a schematic diagram of the inner liner structure of this utility model; Figure 3 This is a schematic diagram of the sealing outer bushing structure of this utility model.

[0015] In the diagram: 1. Sealing outer bushing; 2. Positioning hole; 3. Inner core sleeve; 4. First sealing ring; 5. Second sealing ring; 6. Limiting hole; 7. Snap-fit ​​groove; 8. Inner support reinforcement; 9. Limiting protrusion. Detailed Implementation

[0016] 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.

[0017] Please see Figure 1 , Figure 2 , Figure 3 In this embodiment of the present invention, a high-sealing turbine housing sealing sleeve includes an outer sealing sleeve 1 and an inner sleeve. The outer sealing sleeve 1 has positioning holes 2 inside, and multiple positioning holes 2 are provided at equal angles. The outer sealing sleeve 1 has an inner support reinforcement 8 inside, which increases the structural strength inside the outer sealing sleeve 1 and prevents excessive deformation of the outer sealing sleeve 1 from affecting the sealing effect. The inner support reinforcement 8 has a limiting protrusion 9 on its inner side, and multiple limiting protrusions 9 are arranged in a ring array on the inner wall of the inner support reinforcement 8. The inner sleeve includes an inner core sleeve 3, and a first sealing ring 4 and a second sealing ring 5 are provided on both sides of the inner core sleeve 3. A snap-fit ​​groove 7 is formed between the inner core sleeve 3, the first sealing ring 4 and the second sealing ring 5, and the inner sleeve is snapped onto the inner and outer walls of the outer sealing sleeve 1 through the snap-fit ​​groove 7. The snap-fit ​​groove 7 is set as an arc groove, and the width of the snap-fit ​​groove 7 is equal to the thickness of the outer sealing sleeve 1, so that the inner sleeve can seal the inner wall of the connection gap between the turbine housing and the housing cover, which is beneficial to improving the sealing performance of the turbine housing and the housing cover installation and fixation.

[0018] like Figure 1 and Figure 2 As shown, the inner core sleeve 3, the first sealing ring 4, and the second sealing ring 5 are also integrally formed, and the inner core sleeve 3, the first sealing ring 4, and the second sealing ring 5 are all elastic rubber structures, which makes it easy to fit the inner liner on the outer wall of the sealing outer liner 1.

[0019] like Figure 2 and Figure 3 As shown, in order to improve the stability of the inner core sleeve 3 fitted on the outer wall of the sealing outer bushing 1, a limiting hole 6 is also provided on the side wall of the inner core sleeve 3, and the limiting hole 6 is inserted and matched with the limiting protrusion 9. The inner support reinforcement 8 and the limiting protrusion 9 are both alloy parts, which facilitates the improvement of the stability of the inner core sleeve 3 fitted on the outer wall of the sealing outer bushing 1. Moreover, the inner bushing can be removed when not in use, which improves the flexibility of bushing use.

[0020] The working principle and usage process of this utility model are as follows: In use, the inner support reinforcement 8 is provided inside the sealing outer bushing 1. The inner support reinforcement 8 is made of alloy, which increases the structural strength inside the sealing outer bushing 1 and prevents the sealing outer bushing 1 from being damaged by excessive deformation, thus affecting the sealing effect. Moreover, the inner bushing is snapped into the inner and outer walls of the sealing outer bushing 1 through the snap-fit ​​groove 7. The inner bushing can seal the inner wall of the connection gap between the turbine housing and the housing cover, which is beneficial to improving the sealing performance of the turbine housing and housing cover installation and fixation.

[0021] Finally, it should be noted that the above description is merely a preferred embodiment of this utility model and is not intended to limit the utility model. Although the 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 this utility model should be included within the protection scope of this utility model.

Claims

1. A high-sealing turbine housing sealing sleeve, comprising an outer sealing bushing (1) and an inner bushing, characterized in that: The sealing outer bushing (1) is provided with an inner support reinforcement (8), and the inner support reinforcement (8) is provided with a limiting protrusion (9) on the inner side. The inner bushing includes an inner core sleeve (3), and the inner core sleeve (3) is provided with a first sealing ring (4) and a second sealing ring (5) on both sides. A snap-fit ​​groove (7) is formed between the inner core sleeve (3), the first sealing ring (4) and the second sealing ring (5), and the inner bushing is snapped onto the inner and outer walls of the sealing outer bushing (1) through the snap-fit ​​groove (7).

2. The high-sealing turbine housing sealing sleeve according to claim 1, characterized in that: The inner core sleeve (3), the first sealing ring (4), and the second sealing ring (5) are integrally formed, and the inner core sleeve (3), the first sealing ring (4), and the second sealing ring (5) are all elastic rubber structures.

3. The high-sealing turbine housing sealing sleeve according to claim 2, characterized in that: The snap-fit ​​groove (7) is configured as an arc-shaped groove, and the width of the snap-fit ​​groove (7) is equal to the thickness of the sealing outer bushing (1).

4. The high-sealing turbine housing sealing sleeve according to claim 2, characterized in that: The inner core sleeve (3) has a limiting hole (6) on its side wall, and the limiting hole (6) is engaged with the limiting protrusion (9).

5. The high-sealing turbine housing sealing sleeve according to claim 1, characterized in that: Both the inner support reinforcement (8) and the limiting protrusion (9) are alloy parts, and the limiting protrusion (9) is arranged in a ring array on the inner wall of the inner support reinforcement (8).

6. The high-sealing turbine housing sealing sleeve according to claim 1, characterized in that: The sealing outer bushing (1) has a positioning hole (2) inside, and the positioning hole (2) has multiple holes at equal angles.

Citation Information

Patent Citations

  • High-stability oil-leakage-resistant turbine shell sealing sleeve

    CN223469307U