Supporting device of gas turbine

A gas turbine and supporting device technology, which is applied to gas turbine devices, jet propulsion devices, mechanical equipment, etc., can solve the problems of low reliability and impact resistance, and achieve the effects of simple structure, easy operation, and improved impact resistance

Inactive Publication Date: 2016-06-01
AECC SHENYANG ENGINE RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is to provide a support device for a gas turbine to solve the problem of low reliability and impact resistance of the current support device for a gas turbine

Method used

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  • Supporting device of gas turbine
  • Supporting device of gas turbine
  • Supporting device of gas turbine

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Embodiment Construction

[0019] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the invention. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention. Embodiments of the present invention will be described in detail b...

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Abstract

The invention relates to a supporting device of a gas turbine. The supporting device comprises an installation base, main supporting legs, main supporting adapter coupling supports, auxiliary supporting legs, auxiliary supporting bases and an anti-deflection device; the installation base is placed in a manner of being parallel to the ground, the upper face is an installation face, the lower face is a supporting face, and the supporting face of the installation base is in contact with the ground; one ends of the two main supporting legs are vertically installed on the installation face of the installation base and are fixedly connected with the installation face through bolts, the other ends of the main supporting legs are fixedly provided with the main supporting adapter coupling supports, and the two auxiliary supporting bases are further installed on the installation face of the installation base; the auxiliary supporting legs are installed on the auxiliary supporting bases and hinged to the auxiliary supporting bases through spherical hinges; and a rectangle is formed by the main supporting legs and the auxiliary supporting legs, and the anti-deflection device is arranged in the middle position of a connecting line of the two auxiliary supporting legs and fixedly connected with the installation base. By means of the supporting device of the gas turbine, the requirement for reliability can be met, the shock resistance is improved, and the supporting device has the beneficial effects of being simple in structure, easy and convenient to operate and the like.

Description

technical field [0001] The invention belongs to the technical field of gas turbines, and in particular relates to a gas turbine supporting device. Background technique [0002] The gas turbine is an internal combustion power machine that uses continuous flowing gas as the working medium to drive the impeller to rotate at high speed, and converts the energy of the fuel into useful work. It is a rotary impeller heat engine. However, the gas turbine requires not only the design of the main body, but also the design of the support device. In the design of gas turbine support system, many factors need to be considered, such as reliability, economy and impact resistance. The main engine of the industrial gas turbine is installed on the platform through the base, and the load is transmitted to the platform through the main and auxiliary supporting legs. In order to ensure that the stress level and vibration level of the gas turbine are within the allowable range, the support syst...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02C7/20F01D25/28
CPCF02C7/20F01D25/28
Inventor 李孝堂杨晓玲高松刘常青赵祥敏李彬韩永军姚明舟张东林徐鑫马凤柯郑健
Owner AECC SHENYANG ENGINE RES INST
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