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Aircraft and ancillary materials. 2. ; Engine materials. Kokuki to sono shuhen zairyo. 2. ; Engine zairyo

Abstract

This paper summarizes materials for aircraft engines. Jet engines are the mainstream today, which are classified according to their operation process into a turbo jet engine, a turbo prop engine, a turbo shaft engine, and a turbo fan engine. Japan has produced 1543 engines in the past decade, almost all of which are supplied to the Defense Agency. Jet engines use mainly Ni-group heat-resistant alloys, titanium alloys and steels. Improvement of engine efficiency has caused turbine inlet temperatures to rise to 1400[degree]C to 1500[degree]C that give rise to grain boundary cracking. To prevent this, discussions are in progress on monocrystal blades replacing the conventional polycrystal precision casts. Intermetallic compounds including Al/Ti are expected especially of use as jet engine constructing materials from their high melting point and formability. Discussions are preceding on ceramics as to coating them intended of improving heat resistance. Composite materials have a problem of insufficient mechanical strength remaining unsolved. 8 figs., 5 tabs.
Publication Date:
Apr 05, 1993
Product Type:
Journal Article
Reference Number:
NEDO-93-950294; EDB-93-113640
Resource Relation:
Journal Name: Kino Zairyo; (Japan); Journal Volume: 13:5
Subject:
33 ADVANCED PROPULSION SYSTEMS; 36 MATERIALS SCIENCE; 32 ENERGY CONSERVATION, CONSUMPTION, AND UTILIZATION; BUILDING MATERIALS; HEAT RESISTING ALLOYS; STEELS; TITANIUM BASE ALLOYS; ENGINES; AIRCRAFT; TURBOFAN ENGINES; TURBOJET ENGINES; NICKEL BASE ALLOYS; CASTING; CERAMICS; COMPOSITE MATERIALS; CRACKS; GRAIN BOUNDARIES; INTAKE STRUCTURES; INTERMETALLIC COMPOUNDS; MONOCRYSTALS; NATIONAL DEFENSE; POLYCRYSTALS; TEMPERATURE DEPENDENCE; WAXES; ALLOYS; CRYSTALS; EQUIPMENT; FABRICATION; HEAT ENGINES; HEAT RESISTANT MATERIALS; INTERNAL COMBUSTION ENGINES; IRON ALLOYS; IRON BASE ALLOYS; MACHINERY; MATERIALS; MECHANICAL STRUCTURES; MICROSTRUCTURE; NICKEL ALLOYS; ORGANIC COMPOUNDS; OTHER ORGANIC COMPOUNDS; TITANIUM ALLOYS; TURBOMACHINERY; 330100* - Internal Combustion Engines; 360000 - Materials; 320201 - Energy Conservation, Consumption, & Utilization- Transportation- Air & Aerospace
OSTI ID:
6329823
Country of Origin:
Japan
Language:
Japanese
Other Identifying Numbers:
Journal ID: ISSN 0286-4835; CODEN: KIZAEP
Submitting Site:
NEDO
Size:
Pages: 34-42
Announcement Date:
Sep 15, 1993

Citation Formats

None. Aircraft and ancillary materials. 2. ; Engine materials. Kokuki to sono shuhen zairyo. 2. ; Engine zairyo. Japan: N. p., 1993. Web.
None. Aircraft and ancillary materials. 2. ; Engine materials. Kokuki to sono shuhen zairyo. 2. ; Engine zairyo. Japan.
None. 1993. "Aircraft and ancillary materials. 2. ; Engine materials. Kokuki to sono shuhen zairyo. 2. ; Engine zairyo." Japan.
@misc{etde_6329823,
title = {Aircraft and ancillary materials. 2. ; Engine materials. Kokuki to sono shuhen zairyo. 2. ; Engine zairyo}
author = {None}
abstractNote = {This paper summarizes materials for aircraft engines. Jet engines are the mainstream today, which are classified according to their operation process into a turbo jet engine, a turbo prop engine, a turbo shaft engine, and a turbo fan engine. Japan has produced 1543 engines in the past decade, almost all of which are supplied to the Defense Agency. Jet engines use mainly Ni-group heat-resistant alloys, titanium alloys and steels. Improvement of engine efficiency has caused turbine inlet temperatures to rise to 1400[degree]C to 1500[degree]C that give rise to grain boundary cracking. To prevent this, discussions are in progress on monocrystal blades replacing the conventional polycrystal precision casts. Intermetallic compounds including Al/Ti are expected especially of use as jet engine constructing materials from their high melting point and formability. Discussions are preceding on ceramics as to coating them intended of improving heat resistance. Composite materials have a problem of insufficient mechanical strength remaining unsolved. 8 figs., 5 tabs.}
journal = []
volume = {13:5}
journal type = {AC}
place = {Japan}
year = {1993}
month = {Apr}
}