CN220434870U - Exhaust muffler installation assembly of aeroengine - Google Patents

Exhaust muffler installation assembly of aeroengine Download PDF

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Publication number
CN220434870U
CN220434870U CN202321976443.5U CN202321976443U CN220434870U CN 220434870 U CN220434870 U CN 220434870U CN 202321976443 U CN202321976443 U CN 202321976443U CN 220434870 U CN220434870 U CN 220434870U
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CN
China
Prior art keywords
exhaust
muffler
exhaust muffler
supporting plate
joint
Prior art date
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Active
Application number
CN202321976443.5U
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Chinese (zh)
Inventor
邓江
尹俊杰
何强
黄杰
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Chongqing Zongshen Aviation Engine Manufacturing Co ltd
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Chongqing Zongshen Aviation Engine Manufacturing Co ltd
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Priority to CN202321976443.5U priority Critical patent/CN220434870U/en
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Publication of CN220434870U publication Critical patent/CN220434870U/en
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Abstract

The utility model discloses an exhaust muffler mounting assembly of an aeroengine, which comprises an exhaust muffler, an exhaust elbow communicated with the exhaust muffler and a mounting bracket, wherein a connecting part is arranged on the mounting bracket, and the connecting part is attached to the exhaust muffler through a belt type hoop. The problem that the reliability is relatively poor caused by the fact that an exhaust muffler installation assembly of an aeroengine is easy to fall off in the prior art is solved.

Description

Exhaust muffler installation assembly of aeroengine
Technical Field
The utility model relates to an exhaust system of an aeroengine, in particular to an exhaust muffler installation assembly of the aeroengine.
Background
The existing exhaust muffler of the aeroengine is generally installed in a hanging mode, as shown in fig. 1, the exhaust muffler a is hung through four exhaust bent pipes b, two tension springs c are arranged between each exhaust bent pipe b and the exhaust muffler a, and two ends of each tension spring c are respectively connected with the exhaust muffler a and the exhaust bent pipe b through two spring hooks d, so that elastic connection is formed between the exhaust muffler and the exhaust bent pipe. Thus, the whole exhaust muffler needs eight tension springs and sixteen spring hooks to be installed, and when one tension spring or one spring hook is broken, the whole exhaust muffler is unstable to be installed, so that the exhaust muffler is easy to drop, and the reliability is poor.
Disclosure of Invention
The utility model aims to provide an exhaust muffler mounting assembly of an aeroengine, which is used for solving the problem that the reliability is poor due to the fact that the exhaust muffler mounting assembly of the aeroengine is easy to fall off in the prior art.
In order to achieve the above purpose, the basic scheme of the utility model provides an exhaust muffler installation assembly of an aeroengine, which comprises an exhaust muffler, an exhaust elbow communicated with the exhaust muffler and an installation support, wherein a connecting part is arranged on the installation support, and the connecting part is attached to the exhaust muffler through a belt type hoop.
The beneficial effect of this basic scheme lies in: by adopting the arrangement, the exhaust muffler is connected with the mounting bracket through the belt type hoop, and the belt type hoop has certain elasticity, so that the exhaust muffler is in non-rigid connection with the mounting bracket, thereby reducing vibration transmission between the exhaust muffler and the mounting bracket, further improving the stability and fatigue durability of the mounting bracket under the vibration effect, and enhancing the reliability of the exhaust muffler mounting assembly.
Further, the mounting bracket is provided with a first supporting plate vertical to the axial direction of the exhaust muffler and a second supporting plate parallel to the axial direction of the exhaust muffler, and connecting holes are formed in the first supporting plate and the second supporting plate. By adopting the arrangement, the first support plate and the second support plate are utilized to resist the actions in two directions perpendicular to each other, so that the structural stability of the mounting bracket is enhanced, and the reliability of the exhaust muffler mounting assembly is further improved.
Further, a bending part is arranged between the connecting hole and the connecting part on the first supporting plate. By adopting the arrangement, the toughness of the first supporting plate is improved by utilizing the bending part, so that the vibration resistance of the mounting bracket is further improved, and the reliability of the exhaust muffler mounting assembly is further enhanced.
Further, the exhaust muffler is connected with the exhaust elbow through a joint assembly, the joint assembly comprises a muffler joint connected to the exhaust muffler, an exhaust pipe outer sleeve and an exhaust pipe inner sleeve connected to the end part of the exhaust elbow, and a containing cavity for plugging the muffler joint is arranged between the exhaust pipe outer sleeve and the exhaust pipe inner sleeve. By adopting the arrangement, the connection between the new exhaust muffler and the exhaust elbow is realized through the plug-in fit of the muffler joint between the exhaust pipe outer sleeve and the exhaust pipe inner sleeve, so that the connection operation is simpler, the assembly tolerance between the exhaust elbow and the exhaust muffler can be effectively overcome, and the processing difficulty is reduced.
Further, the outer sleeve and the inner sleeve are respectively provided with a waveform part for interference fit with the muffler joint. By adopting the arrangement, the sealing effect between the outer sleeve and the inner sleeve of the exhaust pipe and the muffler joint is realized by utilizing the line contact and interference fit between the wavy part and the muffler joint, thereby enhancing the connection tightness.
Drawings
FIG. 1 is a schematic illustration of a prior art exhaust muffler mounting assembly;
FIG. 2 is a schematic view of an embodiment of an exhaust muffler mounting assembly for an aircraft engine according to the present utility model;
FIG. 3 is a right side view of FIG. 2;
fig. 4 is a schematic diagram of the connection of an exhaust muffler to an exhaust elbow.
Detailed Description
The following is a further detailed description of the embodiments:
reference numerals in the drawings of the specification include: the exhaust muffler 1, the anchor bolt 21, the steel belt 22, the first supporting plate 31, the second supporting plate 32, the connecting part 33, the bending part 311, the muffler joint 4, the exhaust pipe outer sleeve 5, the exhaust pipe inner sleeve 6 and the exhaust elbow 7.
An embodiment is substantially as shown in figures 2 to 4: an exhaust muffler installation assembly of an aeroengine comprises an exhaust muffler 1 and an exhaust elbow 7 communicated with the exhaust muffler 1, wherein an installation bracket is arranged on the exhaust muffler 1. In this embodiment, the mounting bracket is provided with a connection portion 33, and the connection portion 33 is attached to the exhaust muffler 1 through a band-type anchor ear. In this embodiment, the band type anchor ear is composed of a steel band 22 and anchor ear bolts 21 for adjusting the distance between both ends of the steel band 22. The mounting bracket is provided with a first supporting plate 31 perpendicular to the axial direction of the exhaust muffler 1 and a second supporting plate 32 parallel to the axial direction of the exhaust muffler 1, and connecting holes are formed in the first supporting plate 31 and the second supporting plate 32, so that the central lines of the two connecting holes are perpendicular to each other, and the mounting bracket can restrict the axial direction and the radial direction of the exhaust muffler 1. A bending portion 311 is disposed between the connecting hole and the connecting portion 33 on the first supporting plate 31, and in this embodiment, the bending portion 311 is disposed near the connecting hole on the first supporting plate 31.
In this embodiment, the exhaust muffler 1 and the exhaust elbow 7 are connected by a joint assembly. The joint assembly comprises a muffler joint 4 connected to the exhaust muffler 1, an exhaust pipe outer sleeve 5 and an exhaust pipe inner sleeve 6 connected to the end part of an exhaust elbow 7, and a containing cavity for plugging the muffler joint 4 is arranged between the exhaust pipe outer sleeve 5 and the exhaust pipe inner sleeve 6. The exhaust pipe outer sleeve 5 and the exhaust pipe inner sleeve 6 are provided with wave-shaped parts for interference fit with the muffler joint 4.
The specific implementation process is as follows:
when the exhaust muffler is used, the exhaust muffler 1 is connected with the mounting bracket through the belt type hoop, and then the mounting bracket is connected with the engine, so that the exhaust muffler 1 is fixed on the engine. Finally, the muffler joint 4 is inserted between the exhaust pipe outer sleeve 5 and the exhaust pipe inner sleeve 6, so that the exhaust muffler 1 is connected with the exhaust elbow 7. During specific assembly operation, a certain amount of high-temperature-resistant sealant is smeared on the surface of the muffler joint 4, so that the sealing effect is improved.
The foregoing is merely exemplary embodiments of the present utility model, and specific structures and features that are well known in the art are not described in detail herein. It should be noted that modifications and improvements can be made by those skilled in the art without departing from the structure of the present utility model, and these should also be considered as the scope of the present utility model, which does not affect the effect of the implementation of the present utility model and the utility of the patent.

Claims (4)

1. The utility model provides an aeroengine's exhaust silencer installation assembly, includes exhaust silencer and the exhaust return bend that communicates with exhaust silencer, its characterized in that: the mounting bracket is provided with a connecting part, and the connecting part is attached to the exhaust muffler through a belt type hoop;
the mounting bracket is provided with a first supporting plate vertical to the axial direction of the exhaust muffler and a second supporting plate parallel to the axial direction of the exhaust muffler, and connecting holes are formed in the first supporting plate and the second supporting plate.
2. An aircraft engine exhaust muffler mounting assembly according to claim 1, wherein: and a bending part is arranged between the connecting hole and the connecting part on the first supporting plate.
3. An aircraft engine exhaust muffler mounting assembly according to claim 1 or 2, wherein: the exhaust muffler is connected with the exhaust elbow through a joint assembly, the joint assembly comprises a muffler joint connected to the exhaust muffler, an exhaust pipe outer sleeve and an exhaust pipe inner sleeve connected to the end part of the exhaust elbow, and a containing cavity for plugging the muffler joint is arranged between the exhaust pipe outer sleeve and the exhaust pipe inner sleeve.
4. An aircraft engine exhaust muffler mounting assembly according to claim 3, wherein: the outer sleeve and the inner sleeve of the exhaust pipe are respectively provided with a waveform part which is in interference fit with the muffler joint.
CN202321976443.5U 2023-07-26 2023-07-26 Exhaust muffler installation assembly of aeroengine Active CN220434870U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202321976443.5U CN220434870U (en) 2023-07-26 2023-07-26 Exhaust muffler installation assembly of aeroengine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202321976443.5U CN220434870U (en) 2023-07-26 2023-07-26 Exhaust muffler installation assembly of aeroengine

Publications (1)

Publication Number Publication Date
CN220434870U true CN220434870U (en) 2024-02-02

Family

ID=89697618

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202321976443.5U Active CN220434870U (en) 2023-07-26 2023-07-26 Exhaust muffler installation assembly of aeroengine

Country Status (1)

Country Link
CN (1) CN220434870U (en)

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