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Dynamic seal structure of wheel-disc transverse teeth of gas turbine

A dynamic sealing structure, gas turbine technology, applied in the direction of machines/engines, mechanical equipment, engine components, etc., can solve the problems of unreliable fasteners, complex structures, difficult installation, etc., to ensure reliability and safety, and facilitate The effect of disassembly and replacement, easy processing and assembly

Active Publication Date: 2015-04-22
DONGFANG TURBINE CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In order to solve the problems of complex structure, difficult installation and unreliability of fasteners of traditional sealing components, the present invention provides a dynamic sealing structure

Method used

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  • Dynamic seal structure of wheel-disc transverse teeth of gas turbine
  • Dynamic seal structure of wheel-disc transverse teeth of gas turbine
  • Dynamic seal structure of wheel-disc transverse teeth of gas turbine

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Embodiment Construction

[0015] Such as Figure 2-5 As shown, the present invention is a dynamic sealing structure of gas turbine disc end face teeth. The two connecting wheels 1-1 and 1-2 each add a ring-shaped boss on the inner side of the meshing part of the end face teeth 2. A pair of circumferential grooves 6-1 and 6-2 are correspondingly provided on the end faces of the opposite circular bosses of the discs 1-1 and 1-2, and the circumferential grooves 6-1 and 6-2 are similar to O-ring structures sealing groove.

[0016] The gas turbine disc end face gear moving sealing part of the present invention is a ring of sealing plates whose two ends are respectively inserted in the opposite circumferential grooves 6-1 and 6-2. The sealing plate is composed of several arc-shaped sealing plates 7, each end of the sealing plate 7 is provided with an L-shaped pinch plate 8 inwardly or outwardly, and the corresponding positions of the circumferential grooves 6-1 and 6-2 Bayonet 9 is provided.

[0017] The...

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Abstract

The invention provides a dynamic seal structure of wheel-disc transverse teeth of a gas turbine. A circle of ring-shaped boss is arranged at the inner side of the meshing part of end teeth of each matching wheel disc, and a pair of circumferential grooves are formed in an opposite end face. The dynamic seal structure is a circle of seal plate of which two ends are respectively inserted into the opposite circumferential grooves. The seal plate is composed of a plurality of segments of arc-shaped seal plates, L-shaped pinch plates are arranged inward or outward at two ends of each segment of seal plate, and bayonets are arranged on corresponding positions of the circumferential grooves. The seal structure has the characteristics of simple structure and convenience in processing and assembly, and only the circumferential grooves matched with the seal plate are formed in a rotor. The centrifugal force role of the seal plate is applied, so that the seal plate achieves a seal effect along with the increasing of the rotation speed of the rotor. After a unit stops, the clinging force between the seal plate and the rotor disappears, and the seal plate is conveniently disassembled and replaced. The structure adopts a design thought without fasteners, the reliability and the safety of the seal structure are ensured well, and the dynamic seal structure is easy for large-scale promotion and use.

Description

technical field [0001] The invention relates to high-speed rotating equipment such as gas turbines and steam turbines, in particular to a dynamic sealing structure for the end teeth of the gas turbine disc. Background technique [0002] Such as figure 1 , 2 As shown, the connection mode of the turbine disk of the gas turbine is mostly that the impeller 1-1 and the impeller 1-2 are butted through the end face teeth 2, and then axially tightened by the tie rod 3 to form a turbine rotor. In the assembly structure of the face teeth of the gas turbine, when the impeller 1-1 and the end face teeth 2 of the impeller 1-2 are mated, there is an assembly gap between the impeller dedendum 4 and the impeller addendum 5, so that the outside of the end face tooth 2 and its disc The inner chamber communicates directly through this assembly gap. If the gas parameters of the inner chamber of the wheel disc are different from those of the outer gas parameters of the face gear 2, gas leakag...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F01D11/00
Inventor 祁乃斌孙伟方宇艾松袁永强黄果赵卫军周洪宇陶健赵仕志陈丽华
Owner DONGFANG TURBINE CO LTD