Accession Number : AD0860362
Title : Selected Problems from Technical Analysis of Combustion Chamber Deficiencies of Aviation Engines,
Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH
Personal Author(s) : Andruszkiewicz, St. ; Sikorski, M.
Report Date : 03 APR 1969
Pagination or Media Count : 16
Abstract : Fundamental problems encountered in combustion chambers and flame tubes of jet engines are discussed. It is recommended that the tightening force on combustion chamber flange bolts should not exceed 0.4 plus or minus 0.025 kgm. Fragment visual inspection of combustion chamber liners is recommended to prevent serious damage. A magnifying glass with a magnifying power of 5, the use of defectoscopy, and the use of ultrasound are recommended for inspections. Cracks found in flame tubes should be properly welded to increase their lifetime. (Author)
Descriptors : (*JET ENGINES, COMBUSTION CHAMBERS), (*COMBUSTION CHAMBERS, FAILURE(MECHANICS)), RUPTURE, FRACTURE(MECHANICS), NOZZLE THROATS, CRACKS, CRACK PROPAGATION, DEFECTS(MATERIALS), FATIGUE(MECHANICS), DEFORMATION, AVIATION SAFETY, POLAND.
Subject Categories : Mechanics
Combustion and Ignition
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE