1-20 of 108 Search Results for

jet engine blades

Follow your search
Access your saved searches in your account

Would you like to receive an alert when new items match your search?
Close Modal
Sort by
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1980) 29 (9): Sn-10.
Published: 01 September 1980
... and recycled into new uses any number of times. Among its many uses are fusible mandrels for electroforming, proof casting in foundries, low-temperature solder, holding jet engine blades for machining and dies for wax patterns for investment casting. This datasheet provides information on composition, physical...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1980) 29 (11): Bi-20.
Published: 01 November 1980
... jet engine blades for machining and broaching, support for bending tubing and extrusions and seals for annealing and nitriding furnaces. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on casting, forming, heat...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1980) 29 (5): Bi-17.
Published: 01 May 1980
... and recycled into new uses any number of times. Its many uses include holding jet engine blades for machining, foundry patterns and fusible elements in safety devices. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1959) 8 (3): Co-17.
Published: 01 March 1959
... HAYNES Alloy No. 36 is a cobalt-base alloy having excellent strength at temperatures up to 1800 deg. F. It is the cast modification of wrought HAYNES Alloy No. 25 and has been used successfully in jet engine blading and nozzle vanes. This datasheet provides information on composition, physical...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1984) 33 (2): Bi-35.
Published: 01 February 1984
...- i2Sn can be used to anchor many types of parts and components (such as jet-engine blades and buckets) for machining and grinding. Common practice is to set several blades in the alloy within an iron form and machine all of them simultaneously. This alloy expands rapidly after solidification to give...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1960) 9 (2): TS-90.
Published: 01 February 1960
... a temperature above 700┬░F. Cool slowly in furnace or insulating material. Parts should be given a fuh anneal afta welding. General Characteristics: JET FORGE is a chromium, molybdenum, vanadium 9 pe hot work tool steed particukuly adapted for the orgiog of jet engine blades and otha high temperature and high...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1979) 28 (9): Bi-13.
Published: 01 September 1979
... to 15 hours age hardening (depending on application) before placing in operation, The shrinkage/growth characteristics of Cerrolow-136 alloy are given in Table 2. Anchoring of Parts: Cerrolow-136 alloy can be used to anchor many types of parts and components (such as jet-engine blades and buckets...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1983) 32 (6): Bi-31.
Published: 01 June 1983
... pigs. Applications: lndalloy 147 is suitable for anchoring or holding jet engine blades and many other parts and components for machining and lor grinding; internal and external support for bending tubing and extrusions; anchoring inserts and parts in ceramics or plastics; foundry uses such as nests...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1981) 30 (1): Bi-21.
Published: 01 January 1981
... on application) before placing in operation. Anchoring for Machining: Cerrolow-147 alloy can be used to support jet-engine blades for machining and broaching. The final machin- ing, which involves several contour cuts, requires posi- tive supporting of the thin sections that are involved. Many other machining...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1984) 33 (11): Bi-38.
Published: 01 November 1984
... before it solidifies, and (5) Alloy up to IO to I5 hours age hardening (depending on application) before placing in operation. Anchoring for Machining: Bismuth-25.6Pb-I 2.8Sn-9.6Cd-4ln alloy can be used to support jet- engine blades for machining and broaching. The final machining, which involves several...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1981) 30 (2): SS-382.
Published: 01 February 1981
... in continuous service to 1500 F and in intermittent service to 1800 F. Its many high-temperature applications include jet-engine turbine wheels and blades, bolting and afterburner parts. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1981) 30 (10): Co-79.
Published: 01 October 1981
... blades, parts for jet engines and aerospace components. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on high temperature performance and corrosion...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1966) 15 (11): SA-204.
Published: 01 November 1966
... HECLA EM, 20 is an iron-nickel-cobalt-chromium austenitic alloy steel having high oxidation and scaling resistance. It is recommended for high temperature service and medium loads up to 2000 F, such as turbine blading, jet engine exhaust stacks and combustion chambers. This datasheet provides...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1967) 16 (9): SS-200.
Published: 01 September 1967
... AISI No. 616 is a hardenable martensitic type stainless steel recommended for high temperature applications up to 1200 F. It is used for steam turbine blades and buckets, valves, jet engine components, and high temperature bolting. This datasheet provides information on composition, physical...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1968) 17 (2): SA-222.
Published: 01 February 1968
... AISI No 602 is a low-alloy high-temperature constructional steel of the Cr-Mo-V-Si type that possesses useful strength after suitable heat treatment at temperatures up to 1000 F. It is used for jet engine compressor wheels and blading. This datasheet provides information on composition, physical...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1981) 30 (5): Bi-24.
Published: 01 May 1981
... to anchor many types of parts and components (such as jet-engine blades and buckets) for machining and grinding. Common practice is to set several blades in Indalloy 136 within an iron form and machine all of them simultaneously. This alloy expands rapidly after solidification to give a firm grip...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1982) 31 (3): Bi-28.
Published: 01 March 1982
... the grinding and buffing operations on optical lenses and components. Anchoring: Ostalloy 136 alloy can be used to anchor many types of parts and components (such as jet-engine blades and buckets) for machining, broaching and grinding. The alloy gives support between interrupted cuts and pre- vents tool...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1982) 31 (9): Bi-29.
Published: 01 September 1982
... (such as jet-engine blades and buckets) for machining and grinding. Common practice is to set a number of blades in lndailoy 281 within an iron form and machine all of them simul- taneously. This alloy expands rapidly after solidification to give a firm grip on the blade. The small amount of subsequent...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1963) 12 (6): Co-19.
Published: 01 June 1963
.... Forms Available: Precision castings Applications: Turbc+supercharger buckets, gas turbine and jet engine blades, and for high temperature applications. Manufacturer: General Electric Company Metallurgical Products Department Detroit, Michigan ...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1979) 28 (6): Bi-12.
Published: 01 June 1979
... is jet-engine blades and buckets. The blade is set in the fusible alloy within an iron form; several blades can be machined simultaneously. Alloy 2431 ex- pands rapidly after solidification to give a secure grip on the blade. The alloy remelts in hot water and is re- usable. DOI: 10.31399/asm.ad.bi0012...