Supporting device of gas turbine

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...

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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

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