阅读说明：本技术 一种弹性密封结构 (Elastic sealing structure ) 是由 赵亚飞 王旭东 贺耀 李炎军 胡海涛 徐鹏飞 于 2020-11-27 设计创作，主要内容包括：本申请一种弹性密封结构,所述弹性密封结构1为环形结构,弹性密封结构1设置在通气管5外侧、盖板3为环形平板结构,壳体4为环形结构,壳体4的内壁设置环形凹槽,盖板3与壳体4的环形凹槽形成环形空腔,所述环形空腔用于放置弹性密封结构1,通过螺钉2将盖板3固定在壳体4上,具体的：弹性密封结构1的截面形状包括至少两个腔体,弹性密封结构1的外部设置有至少两个凸台。(The utility model provides an elastic sealing structure, elastic sealing structure 1 is the loop configuration, and elastic sealing structure 1 sets up in 5 outsides of breather pipe, apron 3 is the annular flat structure, and casing 4 is the loop configuration, and casing 4's inner wall sets up the annular groove, and apron 3 forms the annular cavity with casing 4's annular groove, the annular cavity is used for placing elastic sealing structure 1, fixes apron 3 on casing 4 through screw 2, and is concrete: the cross-sectional shape of the elastic sealing structure 1 comprises at least two cavities, and at least two bosses are arranged outside the elastic sealing structure 1.)

1. The utility model provides an elastic sealing structure, a serial communication port, elastic sealing structure (1) is the loop configuration, and elastic sealing structure (1) sets up in breather pipe (5) outside, apron (3) is the annular flat structure, and casing (4) are the loop configuration, and the inner wall of casing (4) sets up the annular groove, and apron (3) and the annular groove of casing (4) form annular cavity, the annular cavity is used for placing elastic sealing structure (1), fixes apron (3) on casing (4) through screw (2), and is specific: the cross-sectional shape of the elastic sealing structure (1) comprises at least two cavities, and at least two bosses are arranged outside the elastic sealing structure (1).

2. The elastic sealing structure according to claim 1, characterized in that the cross-sectional shape of the individual cavities of the elastic sealing structure (1) comprises a circle, an ellipse, a heart, a star and a polygon.

3. Elastic sealing structure according to claim 1, characterized in that the elastic sealing structure (1) comprises an elastic sealing structure of uniform wall thickness, an elastic sealing structure of irregular wall thickness.

4. An elastic sealing structure according to claim 1, characterized in that the elastic sealing structure (1) comprises at least one inner support structure and an outer sealing structure, each inner support structure being of a different size, said at least one inner support structure being nested from small to large, the largest inner support being nested within the cavity of the outer sealing structure; a cavity is formed between the inner supporting structure and the outer sealing structure, and at least two elastic supporting structures are arranged in the cavity between the inner supporting structure and the outer sealing structure.

5. An elastic sealing structure according to claim 1, characterized in that the inner annular surface of the cavity of the elastic sealing structure (1) is provided with at least one vent hole.

6. The elastic sealing structure according to claim 1, characterized in that the elastic sealing structure (1) comprises an elastic sealing structure with closed cavities, an elastic sealing structure with open cavities and an elastic sealing structure with a combination of closed cavities and open cavities.

7. An elastic sealing structure according to claim 1, characterized in that at least two elastic sealing structures (1) are superimposed in axial direction to an annular cavity formed by the cover plate (3) and the annular groove of the housing (4).

8. An elastic sealing structure according to claim 1, characterized in that at least two elastic sealing structures (1) with different diameters are nested in the radial direction in an annular cavity formed by the cover plate (3) and the annular groove of the housing (4).

9. The elastic sealing structure according to claim 1, wherein if the cavities of the elastic sealing structure (1) are all closed cavities, an inert gas is provided inside the cavity of the elastic sealing structure (1), and the inert gas comprises argon gas and helium gas.

10. An elastic sealing structure according to claim 7 or 8, characterized in that at least one elastic support structure is arranged between a plurality of elastic sealing structures (1).

Technical Field

The invention belongs to the field of design of aero-engines, and relates to an elastic sealing structure.

Background

To ensure the reliability of the operation of the aircraft engine and its system, the internal sealing means must be reliable. The performance of the sealing device of the aircraft engine directly relates to the problems of aircraft flight safety, the service life of parts, maintenance frequency and the like. A good sealing arrangement is therefore of great importance for aircraft engines.

In current aeroengine, when high temperature high pressure gas got into each cavity through the air supply pipe on the casing, seal structure such as elastic seal or graphite gasket was adopted usually to seal between air supply pipe and cavity, thereby its principle is that seal structure receives axial pressure to produce radial expansion and then laminate the pipeline and seal. At present, most of sealing structures are axially pre-tightened, the structure is complex, the installation steps are complex, and the assembly efficiency is low. Meanwhile, the traditional sealing structure must be scrapped after being used once, repeated use for many times cannot be realized, a new sealing element must be replaced after the pipeline is disassembled, and the economic cost is very high.

Disclosure of Invention

The invention aims to provide an elastic sealing structure aiming at the defects of the prior art, which has reliable sealing performance and convenient installation and allows repeated use.

The utility model provides an elastic sealing structure, elastic sealing structure 1 is the loop configuration, and elastic sealing structure 1 sets up in 5 outsides of breather pipe, apron 3 is the annular flat structure, and casing 4 is the loop configuration, and casing 4's inner wall sets up the annular groove, and apron 3 forms the annular cavity with casing 4's annular groove, the annular cavity is used for placing elastic sealing structure 1, fixes apron 3 on casing 4 through screw 2, and is concrete: the cross-sectional shape of the elastic sealing structure 1 comprises at least two cavities, and at least two bosses are arranged outside the elastic sealing structure 1.

Specifically, the sectional shape of the single cavity of the elastic sealing structure 1 includes a circle, an ellipse, a heart, a star, and a polygon.

Specifically, the elastic sealing structure 1 comprises an elastic sealing structure with equal wall thickness and an elastic sealing structure with irregular wall thickness.

Specifically, the elastic sealing structure 1 comprises at least one internal supporting structure and an external sealing structure, the size of each internal supporting structure is different, the at least one internal supporting structure is nested from small to large in sequence, and the largest internal support is nested in a cavity of the external sealing structure; a cavity is formed between the inner supporting structure and the outer sealing structure, and at least two elastic supporting structures are arranged in the cavity between the inner supporting structure and the outer sealing structure.

Specifically, at least one vent hole is arranged on the inner ring surface of the cavity of the elastic sealing structure 1.

Specifically, the elastic sealing structure 1 comprises an elastic sealing structure with closed cavities, an elastic sealing structure with open cavities and an elastic sealing structure with combined closed cavities and open cavities.

Specifically, at least two elastic sealing structures 1 are superposed in the axial direction in an annular cavity formed by the cover plate 3 and the annular groove of the housing 4.

Specifically, at least two elastic sealing structures 1 with different diameters are nested and overlapped in the radial direction in an annular cavity formed by the cover plate 3 and an annular groove of the shell 4.

Specifically, if the cavity of the elastic sealing structure 1 is a closed cavity, an inert gas is arranged inside the cavity of the elastic sealing structure 1, and the inert gas includes argon and helium.

Specifically, at least one elastic support structure is arranged between the plurality of elastic sealing structures 1.

The elastic sealing structure 1 of the present invention mainly has the following four significant advantages:

firstly, because the cross-section has adopted multistage O shape cavity series connection structure, form between outside bulge loop 6 and the outside bulge loop 7, inside bulge loop 8 and the inside bulge loop 9 between and press the contained angle and form the linkage reaction with the appearance, consequently the sealed atress of single-stage is the condition on the large side can not appear, and the atress is more even with the deformation, and multistage sealed face laminating nature tends to unanimity, has avoided local stress too big, has improved sealed security.

Secondly, a first-stage O-shaped cavity is formed by the outer upper convex ring 6 and the outer lower convex ring 7, a second-stage O-shaped cavity is formed by the inner upper convex ring 8 and the inner lower convex ring 9, two-stage sealing is formed, and the sealing effect is enhanced.

Thirdly, in the normal operation process, when the pressure of the sealing gas of the aircraft engine rises, the gas enters the cavity 10 through the inner ring surface vent hole 11 to supplement the pressure, so that the self-sealing effect of the sealing ring by virtue of the environmental pressure is realized, and the sealing effect is further enhanced.

Fourthly, the elastic sealing structure of the invention also has the following characteristics: a fastening mode of interference fit is used; the section b adopts a multi-stage O-shaped cavity series structure, so that the elastic sealing structure 1 has higher elastic performance; c the silver plating on the inner upper convex ring 8 and the inner lower convex ring 9 play a role of buffering. Therefore, the pipe sealing structure can be conveniently assembled and disassembled, and the influence on the sealing performance is small when the pipe is pulled out and inserted into the sealing structure, so that the pipe sealing structure is convenient to install and can be repeatedly used.

The invention can be applied to the sealing parts of the joint parts of an oil return pipeline and a fuel pipeline of a bearing cavity of an aircraft engine, which need to pass through or be embedded into other components, allows for multiple plugging and unplugging, does not need to pre-tighten a nut during installation, does not need to disassemble other parts except the vent pipe 5 during disassembly, and has the advantages of simple structure, convenient installation, wide application range and the like.

The elastic sealing structure can seal the air-entraining cavity on the basis of not occupying too large structural space. The problems of complex sealing structure, poor reliability and the like of the bleed air flow path are solved, the replacement frequency of the sealing element is reduced, the use cost is directly reduced, and the economic benefit is improved. The invention has the advantages of high sealing performance, high reliability, convenient assembly and disassembly, low cost, small occupied space and simple structure, and has wide application prospect.

Compared with other sealing structures, the sealing performance, the assembly and disassembly convenience, the reliability and the like of the sealing structure are remarkably improved. The sealing safety is improved, and the sealing effect is enhanced. The self-sealing effect of the sealing ring by means of environmental pressure is realized. The installation is convenient, allows repetitious usage.

Therefore, the elastic sealing structure provided by the invention avoids the defects of the traditional sealing structure, improves the sealing performance and reliability, has repeatable practicability, directly reduces the use cost and greatly improves the economic benefit.

Drawings

FIG. 1 is a schematic view of the installation of a flexible seal arrangement of the present invention;

FIG. 2 is a schematic view of the construction of a flexible seal according to the present invention;

FIG. 3 is a schematic representation of a first derivative of the present invention;

FIG. 4 is a schematic representation of a second derivative of the present invention;

FIG. 5 is a schematic representation of a third derivative of the present invention;

FIG. 6 is a schematic representation of a fourth derivative of the present invention;

FIG. 7 is a schematic representation of a fifth derivative of the present invention.

FIG. 8 is a schematic representation of a sixth derivative of the present invention.

FIG. 9 is a schematic representation of a seventh derivative of the present invention.

Wherein, 1-elastic sealing structure, 2-screw, 3-cover plate, 4-shell, 5-vent pipe, 6-upper inner cavity, 7-lower inner cavity, 8-outer shell, 9-inner ring surface vent hole, 15-top inner cavity, 16-bottom inner cavity, and 17-middle inner cavity.

Detailed Description

The technical scheme of the elastic sealing structure is as follows:

the present invention will be described in further detail below by way of specific embodiments:

please refer to fig. 1, which is a schematic view illustrating an installation of an elastic sealing structure according to the present invention. The structure after installation comprises an elastic sealing structure (1) allowing repeated use for many times, a screw (2), a cover plate (3), a shell (4) and a vent pipe (5).

When the elastic sealing structure is installed, the elastic sealing structure (1) is firstly installed in the shell (4), and the elastic sealing structure (1) is generally assembled after being frozen due to interference fit. The second step is to cover the cover plate (3) on the top of the elastic sealing structure (1) by using the screw (2), wherein the cover plate (3) does not play a role in compressing and only plays a role in restraining the axial movement of the cover plate. Finally, the vent pipe (5) is inserted along the axis of the elastic sealing structure (1). The vent pipe (5) can be directly pulled out when needing to be pulled out, and other parts do not need to be disassembled.

Please refer to fig. 2, which is a specific structural diagram of an elastic sealing structure (1) according to the present invention, when assembling, due to the magnitude of interference of the boss mating surface of the outer housing, the elastic sealing structure is elastically deformed by a radial compressive force, so as to generate a large contact stress on the contact surface, and form a contact seal on the adjacent mating surface. When high-temperature and high-pressure gas is introduced into the vent pipe (5), the gas enters the cavity through the vent hole to supplement pressure, so that the self-sealing effect of the sealing ring by virtue of environmental pressure is realized, and the reliable work of the system is fully ensured.

Please refer to fig. 3, which is a schematic diagram of a first derivative of an elastic sealing structure according to the present invention, wherein the cross-sectional shape of the internal cavity is circular, elliptical, or polygonal.

Please refer to fig. 4, which is a schematic diagram of a second derivative of an elastic sealing structure according to the present invention, wherein the cross-sectional shape of the elastic sealing structure is a structure with a plurality of communicating cavities.

Please refer to fig. 5, which is a schematic diagram of a third derivative of an elastic sealing structure according to the present invention, wherein the elastic sealing structure is a nested structure of an inner supporting structure and an outer sealing structure.

Please refer to fig. 6, which is a schematic diagram of a fourth derivative of an elastic sealing structure according to the present invention, wherein the cross-sectional shape of the elastic sealing structure is two closed cavities.

Please refer to fig. 7, which is a schematic diagram of a fifth derivative of an elastic sealing structure according to the present invention, wherein two elastic sealing structures are stacked by a bellows spring, a plate spring, a coil spring, and a welding insert along an axial direction.

Please refer to fig. 8, which is a schematic diagram of a fifth derivative of an elastic sealing structure according to the present invention, wherein two elastic sealing structures with different diameters are respectively stacked by a bellows spring, a grinding plate spring, a coil spring, and a welding nest along a radial direction.

Please refer to fig. 9, which is a schematic diagram of a sixth derivative of an elastic sealing structure according to the present invention, showing a structure of a vent hole at different positions.

The sealing structure can effectively prevent air in the air cavity from leaking. The invention can be used for sealing the joint part of the ventilation pipeline which needs to pass through and be embedded into other components in the aircraft engine. The sealing device has the advantages of good sealing effect on the position which cannot be axially compressed for a sealing result, good sealing performance under the condition of repeated plugging and unplugging of the pipe, simple structure, convenience in installation, no leakage under the condition of repeated use, low use cost and high economic benefit.