|Table of Contents|

Design of fixture for processing turbine tray vanes in rocket engine(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2013年01期
Page:
65-71
Research Field:
工艺与材料
Publishing date:

Info

Title:
Design of fixture for processing turbine tray vanes in rocket engine
Author(s):
XU Jing; WANG Peng
Xi’an Space Engine Factory, Xi’an 710100, China
Keywords:
turbine tray vane;  vector computational method;  trigonometric function
PACS:
V431-34
DOI:
-
Abstract:
The design criteria of the fixture applied for processing the vanes of the turbine tray in rocket engine are introduced in this paper. The distinguishing basis and formula to calculate the fixture limit deviation with vector trigonometric function methods and VC software are offered. The fixture designed with the criteria can meet the design requirements for processing the vanes of turbine tray, and was checked up by hot test run of rocket engine.

References:

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Memo

Memo:
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Last Update: 1900-01-01