Packing-off piece installation device of turbine stator blades and use method of packing-off piece installation device

A turbine stator and installation device technology, which is applied to stators, leakage prevention, engine components, etc., can solve the problems that the interference fit between the positioning pin and the turbine casing is difficult to disassemble, and the sealing sheet is difficult to install, etc., so as to shorten the assembly cycle and facilitate the installation. , the effect of easy assembly

Active Publication Date: 2016-02-03
SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Since the gap between the two blades is smaller than the width of the sealing piece, and at the same time, the interference fit between the positioning pin and the turbine casing is difficult to disassemble, making it difficult

Method used

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  • Packing-off piece installation device of turbine stator blades and use method of packing-off piece installation device
  • Packing-off piece installation device of turbine stator blades and use method of packing-off piece installation device
  • Packing-off piece installation device of turbine stator blades and use method of packing-off piece installation device

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Example Embodiment

[0026] Such as Figure 1~6 As shown, a turbine stator blade sealing piece installation device includes a mounting plate 1, a mounting edge 7, a backing plate 11, a screw 1, a counterweight 6, a limit block 10, a screw 2, a fixing bolt 12, and a nut. The mounting plate 1 is a semicircular plate with two end plates and an auxiliary plate at the top of the arc. The semicircular plate is provided with a mounting hole 2 and a round hole 3. The distance between the mounting holes 2 and the working state The distance between the end holes of the two turbine stator blades 22 is the same, the end plate and the auxiliary plate are provided with lifting holes 4; the counterweight 6 is fixedly installed on the end plate, and the limit block 10 It is installed on the end plate through the second screw; the mounting edge 7 is semi-circular, and the second mounting hole 8 and the screw hole 9 are set thereon; the first screw is inserted into the round hole 3 and screwed into the screw hole 9 ...

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Abstract

The invention relates to a device, in particular to a packing-off piece installation device of turbine stator blades and a use method of the packing-off piece installation device. According to the technical scheme, the packing-off piece installation device comprises an installation plate, an installation edge, first screws, balancing weights, limiting blocks, second screws, fixing bolts and nuts; the installation plate is a semicircular plate and is provided with two end plates and an auxiliary plate on the top of the arc; first installation holes are formed in the semicircular plate, the interval of the first installation holes is the same as the interval of end holes of the two turbine stator blades, and hoisting holes are formed in the end plates and the auxiliary plate; the balancing weights are fixedly arranged on the end plates, and the limiting blocks are arranged on the end plates through the second screws; the installation edge is in a semicircular shape and provided with second installation holes; the installation plate and the installation edge are connected together through the first screws, and the positions of the first installation holes correspond to the positions of the second installation holes; and the fixing bolts and the nuts are used for fixing the turbine stator blades. By means of the packing-off piece installation device, installation of packing-off pieces is achieved under the condition that positioning pins of the turbine stator blades are not decomposed.

Description

technical field [0001] The invention relates to a device, in particular to a turbine stator vane sealing piece installation device and a usage method thereof. Background technique [0002] In the gas turbine structure, the installation of sealing sheets between the turbine stator blades is an important means to ensure the efficiency of the gas turbine. There is an existing gas turbine turbine structure, the casing of which is a horizontal split structure, the stator blades are positioned circumferentially by positioning pins, axially positioned by retaining rings, radially positioned by outer ring blocks, and fixed by inner ring blocks on the stator blade. During the machining process of the turbine case, the outer ring block and the inner ring block need to be installed on the casing to combine and process the honeycomb size. Therefore, the positioning pins and the stator blades need to be installed in place first. After combined processing, the inner and outer ring blocks...

Claims

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Application Information

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IPC IPC(8): F01D25/28F01D9/02F01D11/00
Inventor 孙晓超李景波任加峰
Owner SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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