Communication pipeline with protective structure for aviation

By adopting the design of protective sleeve, threaded splicing structure and elastic support pad on the connecting pipe of aircraft engine, the problems of poor protection effect and incompatible connection are solved, and efficient protection and convenient replacement and adjustment are achieved.

CN223460094UActive Publication Date: 2025-10-21LUOYANG HANGHUI MASCH CO LTD
View PDF 1 Cites 0 Cited by

Patent Information

Application Number
CN202422959948.1
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-12-03
Publication Date
2025-10-21
Estimated Expiration
2034-12-03

AI Technical Summary

Technical Problem

Existing aviation engine connecting pipes have poor protection effect and poor connection adaptability, making them inconvenient to use.

Method used

The connecting pipe is installed on the inner wall of the protective casing, and the double-layer sealing connection is achieved by using threaded splicing grooves and threaded splicing blocks. The elastic support pads and support sleeves are combined for internal and external support. The connecting pipe can be bent and adjusted, and fast disassembly and assembly can be achieved through high-speed bolts and installation sleeves.

Benefits of technology

It achieves effective protection for the connecting pipelines, improves the adaptability and ease of use of the connection, and facilitates quick replacement and adjustment.

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure CN223460094U_ABST
    Figure CN223460094U_ABST
Patent Text Reader

Abstract

The communicating pipeline with the protective structure for aviation comprises a protective sleeve, sealing buckling grooves are formed in the inner wall and the outer wall of the edge of one end of a threaded splicing groove, a fixed supporting pipe is fixedly connected to the inner wall of an installation inserting block, and a supporting cushion block is fixedly connected to the inner wall of the fixed supporting pipe; and a supporting sleeve block is mounted on the outer wall of the protective sleeve in a wrapping manner. According to the communicating pipeline with the protective structure for aviation, the communicating pipeline can be sleeved, supported and protected through the supporting sleeve block, the protective sleeve and the supporting cushion block, impact damage is avoided, the protective effect is good, the connecting position of the protective sleeve can be bent and adjusted through the connecting pipe, adaptability is good, and the communicating pipeline is convenient to use. The connecting pipe is connected with the supporting cushion block, rapid rotating splicing installation is carried out through the threaded splicing groove and the threaded splicing block, the connecting pipe, the threaded splicing groove and the threaded splicing block are conveniently and rapidly disassembled and assembled through the installation sleeve block and the high-speed bolt, and the supporting cushion block can be rapidly positioned, disassembled and assembled through the installation insertion groove and the installation insertion block and is convenient to replace.
Need to check novelty before this filing date? Find Prior Art

Description

TECHNICAL FIELD

[0001] The utility model relates to the technical field of communication pipeline for aviation, specifically to a communication pipeline for aviation with protective structure. BACKGROUND

[0002] The pipeline of an aero-engine is generally connected with accessories such as fuel system and oil system, and transmits medium such as fuel and oil. Especially for the oil system, the pipeline medium oil will flow through rotating parts such as gears and bearings. The abrasion of related rotating parts in the process of meshing or rolling and impurities remaining in the accessory shell during machining form the excess of the fuel system and oil system, which may cause nozzle blockage and damage to rotating parts, and thus affect the safe use of the engine.

[0003] The existing CN117552867A self-cleaning pipeline for an aero-engine can solve the problems of low filtering efficiency caused by traditional oil filters and medium pressure reduction caused thereby, and is suitable for various military and civil aero-engines. However, the existing device has poor protection effect, poor connection adaptability and inconvenient use, and thus a communication pipeline for aviation with protective structure is needed to solve the above problems. SUMMARY

[0004] The utility model aims at providing a communication pipeline for aviation with protective structure to solve the problems of poor protection effect, poor connection adaptability and inconvenient use mentioned in the background.

[0005] To achieve the above-mentioned purpose, the utility model provides the following technical scheme: a communication pipeline for aviation with protective structure, comprising a protective sleeve, a communication pipeline is installed on the inner wall of the protective sleeve, mounting sleeve blocks are installed on both ends of the protective sleeve in a sleeved manner, high-speed bolts are inserted and installed on the outer wall edge of the mounting sleeve blocks, a connecting pipe is fixedly connected to the edge of one end of the mounting sleeve block, a rotating ring is installed in communication on one end of the connecting pipe, a threaded splicing groove is rotatably installed on the rotating ring at one end of the protective sleeve, a threaded splicing block is rotatably installed on the rotating ring at the other end of the protective sleeve, a sealing buckle is fixedly connected to the inner and outer walls of the edge of one end of the threaded splicing block, the sealing buckle is inserted and installed in the sealing buckle groove, the sealing buckle groove is arranged on the inner and outer walls of the edge of one end of the threaded splicing groove, an installation insertion groove is arranged on the inner wall of the protective sleeve, an installation insertion block is inserted and installed in the inner wall of the installation insertion groove, a fixed support pipe is fixedly connected to the inner wall of the installation insertion block, a support pad block is fixedly connected to the inner wall of the fixed support pipe, and a support sleeve block is wrapped and installed on the outer wall of the protective sleeve.

[0006] Preferably, the protective sleeve and the communication pipeline are inserted and installed in a sleeved manner, and the communication pipeline is wrapped and supported by the protective sleeve through the support pad block, the support pad block is of an elastic structure, and the support sleeve block is made of rubber.

[0007] Preferably, the protective sleeve is spirally spliced and installed between the threaded splicing grooves and the threaded splicing blocks, and the threaded splicing grooves are connected to the threaded splicing blocks in double-layer sealing through the sealing buckle grooves and the sealing buckle blocks.

[0008] Preferably, the protective sleeve is spirally spliced and installed between the threaded splicing grooves and the threaded splicing blocks, and the threaded splicing grooves are connected to the threaded splicing blocks in double-layer sealing through the sealing buckle grooves and the sealing buckle blocks.

[0009] Preferably, the protective sleeve is spirally spliced and installed between the threaded splicing grooves and the threaded splicing blocks, and the threaded splicing grooves are connected to the threaded splicing blocks in double-layer sealing through the sealing buckle grooves and the sealing buckle blocks.

[0010] Preferably, the protective sleeve is spirally spliced and installed between the threaded splicing grooves and the threaded splicing blocks, and the threaded splicing grooves are connected to the threaded splicing blocks in double-layer sealing through the sealing buckle grooves and the sealing buckle blocks.

[0011] Compared with the prior art, the beneficial effects of the utility model are that the communication pipeline with the protective structure for aviation can be supported and protected by the supporting sleeve block, the protective sleeve and the supporting pad block, impact damage is avoided, the protection effect is good, the connection of the protective sleeve can be bent and adjusted through the connecting pipe, the adaptability is good, the threaded splicing groove and the threaded splicing block are quickly and rotatably spliced and installed, the connecting pipe, the threaded splicing groove and the threaded splicing block are conveniently and quickly disassembled through the mounting sleeve block and the high-speed bolt, and the supporting pad block can be quickly positioned, disassembled and replaced through the mounting slot and the mounting block. BRIEF DESCRIPTION OF DRAWINGS

[0012] Figure 1 It is a front view of the communication pipeline with the protective structure for aviation.

[0013] Figure 2 It is a front view of the communication pipeline with the protective structure for aviation.

[0014] Figure 3 It is a front view of the communication pipeline with the protective structure for aviation.

[0015] Figure 4 It is a front view of the communication pipeline with the protective structure for aviation. Figure 2 It is an enlarged view of A in the communication pipeline with the protective structure for aviation.

[0016] Figure 5 It is an enlarged view of A in the communication pipeline with the protective structure for aviation. Figure 2 It is an enlarged view of B in the communication pipeline with the protective structure for aviation.

[0017] Figure 6 It is an enlarged view of C in the communication pipeline with the protective structure for aviation. Figure 2 It is an enlarged view of C in the communication pipeline with the protective structure for aviation.

[0018] Figure 7 The utility model provides a kind of communication pipeline for aviation with protective structure Figure 3 The enlarged view of D in the middle.

[0019] In the drawing: 1, protective sleeve, 2, connecting pipe, 3, threaded splicing groove, 4, communication pipeline, 5, supporting cushion block, 6, mounting sleeve block, 7, high-speed bolt, 8, rotating ring, 9, sealing buckle groove, 10, sealing buckle block, 11, threaded splicing block, 12, mounting slot, 13, supporting sleeve block, 14, fixed support pipe, 15, mounting plug. DETAILED DESCRIPTION

[0020] The technical solutions in the embodiments of the utility model will be clearly and completely described below with reference to the drawings in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, rather than all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by those skilled in the art without creative labor fall within the scope of protection of the utility model.

[0021] Please refer to Figures 1-7 The utility model provides a kind of technical scheme: a kind of communication pipeline for aviation with protective structure, including protective sleeve 1, connecting pipe 2, threaded splicing groove 3, communication pipeline 4, supporting cushion block 5, mounting sleeve block 6, high-speed bolt 7, rotating ring 8, sealing buckle groove 9, sealing buckle block 10, threaded splicing block 11, mounting slot 12, supporting sleeve block 13, fixed support pipe 14 and mounting plug 15, communication pipeline 4 is installed in the inner wall of protective sleeve 1, protective sleeve 1 and communication pipeline 4 are inserted into each other and are installed, and communication pipeline 4 is wrapped and supported by supporting cushion block 5 and protective sleeve 1, supporting cushion block 5 is elastic structure, supporting sleeve block 13 is rubber material, so that protective sleeve 1 is conveniently supported and protected inside and outside by supporting sleeve block 13 and supporting cushion block 5.

[0022] Protective sleeve 1 is installed by threaded splicing groove 3 and threaded splicing block 11 between the screw joint, and threaded splicing groove 3 is connected by sealing buckle groove 9, sealing buckle block 10 and threaded splicing block 11 Double-sealed, so that protective sleeve 1 is quickly rotated and spliced and installed, and double-sealing treatment can be carried out, protective sleeve 1 is installed by connecting pipe 2 between the bending communication, and connecting pipe 2 is spring pipe structure, so that the connecting part of protective sleeve 1 can be bent and adjusted, and the installation adaptability is good.

[0023] The installation sleeve block 6 is sleeved and mounted at both ends of the protective sleeve 1, high-speed bolts 7 are inserted and mounted at the outer wall edges of the installation sleeve block 6, a connecting pipe 2 is fixedly connected at one end of the installation sleeve block 6, and a rotating ring 8 is communicated and mounted at one end of the connecting pipe 2; the connecting pipe 2, the threaded splicing groove 3 and the threaded splicing block 11 are inserted and locked and spliced and mounted at one end of the protective sleeve 1 through the installation sleeve block 6 and the high-speed bolts 7, so that the connecting pipe 2, the threaded splicing groove 3 and the threaded splicing block 11 are conveniently and independently disassembled and assembled for quick replacement.

[0024] The threaded splicing groove 3 is rotatably mounted on the rotating ring 8 at one end of the protective sleeve 1, the threaded splicing block 11 is rotatably mounted on the rotating ring 8 at the other end of the protective sleeve 1, the sealing buckle block 10 is fixedly connected at the inner and outer walls of one end edge of the threaded splicing block 11, the sealing buckle block 10 is inserted and mounted in the sealing buckle groove 9, the sealing buckle groove 9 is formed in the inner and outer walls of one end edge of the threaded splicing groove 3, the installation insertion groove 12 is formed in the inner wall of the protective sleeve 1, the installation insertion block 15 is inserted and mounted in the inner wall of the installation insertion groove 12, the fixed support pipe 14 is fixedly connected to the inner wall of the installation insertion block 15, the support pad block 5 is fixedly connected to the inner wall of the fixed support pipe 14, the support pad block 5 is positioned, inserted and spliced and mounted in the protective sleeve 1 through the installation insertion groove 12 and the installation insertion block 15, so that the support pad block 5 is conveniently inserted and disassembled, and the protective sleeve 1 is conveniently used, and the support sleeve block 13 is wrapped and mounted on the outer wall of the protective sleeve 1.

[0025] Working principle: when the device is used, the protective sleeve 1 of the device is sleeved on the outer wall of the communication pipeline 4, the threaded splicing groove 3 and the threaded splicing block 11 are rotatably spliced and mounted at the connection through the rotating ring 8, the double-layer sealing is buckled through the sealing buckle groove 9 and the sealing buckle block 10, when the connection is bent, the bending adjustment can be realized through the connecting pipe 2, when the device is used, the inner and outer supports and buffers of the communication pipeline 4 can be realized through the support pad block 5 and the support sleeve block 13, when the connecting pipe 2, the splicing groove 3 and the threaded splicing block 11 are damaged and need to be replaced, the quick insertion and locking disassembly and assembly replacement can be realized through the installation sleeve block 6 and the high-speed bolts 7, when the support pad block 5 needs to be adapted to different communication pipelines 4, the positioning, insertion and splicing installation can be realized through the installation insertion groove 12, the installation insertion block 15 and the protective sleeve 1, the adaptation, replacement and adjustment can be realized, which is the use process of the communication pipeline with the protective structure for aviation.

[0026] Although the utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art can modify the technical solutions recorded in the foregoing embodiments or replace part of the technical features equivalently, any modification, equivalent replacement, improvement, etc. within the spirit and principle of the utility model should be included in the protection scope of the utility model.

Claims

1. A communication pipeline with a protective structure for aviation, comprising a protective sleeve (1), a communication pipeline (4) is installed on the inner wall of the protective sleeve (1), characterized in that: The protective sleeve (1) is provided with a mounting sleeve block (6) at both ends, and high-speed bolts (7) are inserted and mounted on the outer wall edge of the mounting sleeve block (6). One end of the mounting sleeve block (6) is fixedly connected with a connecting pipe (2), and one end of the connecting pipe (2) is communicatedly provided with a rotating ring (8). A threaded splicing groove (3) is rotatably mounted on the rotating ring (8) at one end of the protective sleeve (1), and a threaded splicing block (11) is rotatably mounted on the rotating ring (8) at the other end of the protective sleeve (1). The threaded splicing block (11) is fixedly connected with a sealing buckle block (10) on the inner and outer walls of the edge of one end, and the sealing buckle block (10) is inserted and mounted with a sealing buckle groove (9). The sealing buckle groove (9) is provided on the inner and outer walls of the edge of one end of the threaded splicing groove (3). An installation slot (12) is provided on the inner wall of the protective sleeve (1), and an installation plug (15) is inserted and mounted on the inner wall of the installation slot (12). The installation plug (15) is fixedly connected with a fixed support pipe (14) on the inner wall, and the fixed support pipe (14) is fixedly connected with a support pad block (5) on the inner wall. The protective sleeve (1) is wrapped with a support sleeve block (13).

2. A communication line for an aircraft with a protective structure according to claim 1, characterized in that: The protective sleeve (1) is inserted and mounted with the communication pipeline (4), and the communication pipeline (4) is wrapped and supported with the protective sleeve (1) through the support pad block (5). The support pad block (5) is of elastic structure, and the support sleeve block (13) is of rubber material.

3. A communication line for an aircraft with a protective structure according to claim 2, characterized in that: The protective sleeve (1) is spirally spliced between the threaded splicing groove (3) and the threaded splicing block (11), and the threaded splicing groove (3) is double-sealed connected with the threaded splicing block (11) through the sealing buckle groove (9) and the sealing buckle block (10).

4. A communication line with a protective structure for an aircraft according to claim 3, characterized in that: The protective sleeve (1) is bent and communicated between the connecting pipes (2), and the connecting pipe (2) is of spring pipe structure.

5. A communication line with a protective structure for an aircraft according to claim 4, characterized in that: The connecting pipe (2), the threaded splicing groove (3) and the threaded splicing block (11) are inserted and locked and spliced with one end of the protective sleeve (1) through the mounting sleeve block (6) and the high-speed bolt (7).

6. A communication line with a protective structure for an aircraft according to claim 5, characterized in that: The support pad block (5) is positioned, inserted and spliced with the protective sleeve (1) through the installation slot (12) and the installation plug (15).

Citation Information

Patent Citations

  • Self-cleaning pipeline of aero-engine

    CN117552867A