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FY 1999 project on the development of new industry support type international standards. Standardization of a method to evaluate the strength of aerospace use hi-tech composite materials; 1999 nendo shinki sangyo shiengata kokusai hyojun kaihatsu jigyo seika hokokusho. Koku uchuyo sentan fukugozai no kyodo hyoka hoho no hyojunka

Abstract

As to the evaluation method of the strength of aerospace use composite materials and the repair materials/repair parts, the R and D were conducted for international standardization. The FY 1999 results were summed up. Concerning the damage resistance of base structure, tests to give damages to three kinds of sandwich panels and tests on the strength of damaged parts were conducted, and it was confirmed that the foamed core was more easily damaged and less in strength lowering than the honeycomb core. Relating to damages of composite material parts which are caused by aircraft operation, surveys were carried out at Swissair, Japan Air Lines and Lufthansa German Airlines. In the investigational study of the repair method of composite material structures, it was found out that there were typical forms of repair: only one face plate, one face plate and core, and both face plates and core, and according to these, the analysis of strength should also be adopted. The survey of the repair method was also made at each airframe maker. In the study of the analysis method of strength at repair parts, it was confirmed that the finite element method was high in accuracy and can be adopted also  More>>
Authors:
"NONE"
Publication Date:
Mar 01, 2000
Product Type:
Technical Report
Report Number:
JP-NEDO-010015213
Resource Relation:
Other Information: PBD: Mar 2000
Subject:
36 MATERIALS SCIENCE; COMPOSITE MATERIALS; AIRCRAFT; YIELD STRENGTH; MEASURING METHODS; STANDARDIZATION; ISO; RETROFITTING; DAMAGE; HONEYCOMB STRUCTURES; FINITE ELEMENT METHOD
OSTI ID:
20175331
Research Organizations:
New Energy and Industrial Technology Development Organization, Tokyo (Japan)
Country of Origin:
Japan
Language:
Japanese
Other Identifying Numbers:
TRN: JN0140331
Availability:
Available to ETDE participating countries only(see www.etde.org); commercial reproduction prohibited; OSTI as DE20175331
Submitting Site:
NEDO
Size:
306 pages
Announcement Date:

Citation Formats

FY 1999 project on the development of new industry support type international standards. Standardization of a method to evaluate the strength of aerospace use hi-tech composite materials; 1999 nendo shinki sangyo shiengata kokusai hyojun kaihatsu jigyo seika hokokusho. Koku uchuyo sentan fukugozai no kyodo hyoka hoho no hyojunka. Japan: N. p., 2000. Web.
FY 1999 project on the development of new industry support type international standards. Standardization of a method to evaluate the strength of aerospace use hi-tech composite materials; 1999 nendo shinki sangyo shiengata kokusai hyojun kaihatsu jigyo seika hokokusho. Koku uchuyo sentan fukugozai no kyodo hyoka hoho no hyojunka. Japan.
2000. "FY 1999 project on the development of new industry support type international standards. Standardization of a method to evaluate the strength of aerospace use hi-tech composite materials; 1999 nendo shinki sangyo shiengata kokusai hyojun kaihatsu jigyo seika hokokusho. Koku uchuyo sentan fukugozai no kyodo hyoka hoho no hyojunka." Japan.
@misc{etde_20175331,
title = {FY 1999 project on the development of new industry support type international standards. Standardization of a method to evaluate the strength of aerospace use hi-tech composite materials; 1999 nendo shinki sangyo shiengata kokusai hyojun kaihatsu jigyo seika hokokusho. Koku uchuyo sentan fukugozai no kyodo hyoka hoho no hyojunka}
abstractNote = {As to the evaluation method of the strength of aerospace use composite materials and the repair materials/repair parts, the R and D were conducted for international standardization. The FY 1999 results were summed up. Concerning the damage resistance of base structure, tests to give damages to three kinds of sandwich panels and tests on the strength of damaged parts were conducted, and it was confirmed that the foamed core was more easily damaged and less in strength lowering than the honeycomb core. Relating to damages of composite material parts which are caused by aircraft operation, surveys were carried out at Swissair, Japan Air Lines and Lufthansa German Airlines. In the investigational study of the repair method of composite material structures, it was found out that there were typical forms of repair: only one face plate, one face plate and core, and both face plates and core, and according to these, the analysis of strength should also be adopted. The survey of the repair method was also made at each airframe maker. In the study of the analysis method of strength at repair parts, it was confirmed that the finite element method was high in accuracy and can be adopted also to complicated shapes, and that it was a method suitable for the actual analysis of repair strength. (NEDO)}
place = {Japan}
year = {2000}
month = {Mar}
}