1-12 of 12 Search Results for

heavy duty jet engine

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
Alloy Digest (1959) 8 (4): Ni-52.
Published: 01 April 1959
... Unitemp M-252 is a high-strength nickel-base forging alloy recommended for heavy duty jet engine and gas turbine buckets. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep and fatigue. It also includes information...
Journal Articles
Alloy Digest (1962) 11 (9): Ni-32.
Published: 01 September 1962
... ALLOY M252 is a high-strength nickel-base forging alloy recommended for heavy duty jet engine and gas turbine buckers. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on forming...
Journal Articles
Alloy Digest (1967) 16 (5): Ni-124.
Published: 01 May 1967
... and forgings, wire, sheer, strip, place, ingots and ocher forms. Applications: Heavy-duty jet engine and gas turbine buckets, high temperature bolting, jet engine turbine wheels and ocher critical jet engine components. Manufacturer: Special Metals, Inc. New Hartford, New York ...
Journal Articles
Alloy Digest (1964) 13 (11): Ti-42.
Published: 01 November 1964
... Republic RS-110C is a moderate strength highly weldable titanium alloy recommended for jet engine welded rings, aircraft skins, and structural parts. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness...
Journal Articles
Alloy Digest (1970) 19 (3): SA-250.
Published: 01 March 1970
... REPUBLIC RSM 250 is an 18% nickel-cobalt-molybdenum age-hardening steel designed to develop 250,000 psi yield strength with good toughness. It is recommended where a combination of strength, toughness and notch resistance is required such as aircraft landing gears and jet engine components...
Journal Articles
Alloy Digest (2002) 51 (5): SS-853.
Published: 01 May 2002
..., and widths up to 1219 mm (48 in For other thicknesses and widths, inquire to the pro- ducer. Applications: Applications include annealing covers, high-temperature temper- ing equipment, diesel and heavy-duty automotive exhaust sys- tems, firewalls, stack liners, boiler casings, welded pressure vessels, jet...
Journal Articles
Alloy Digest (1965) 14 (11): Ti-46.
Published: 01 November 1965
... operations, slow speeds and coarse feeds are imporcanc. Heavy duty drills of short overall lengrh are recommended. DriII should be cleared frequently. Use slow wheel speeds for grinding. Grind wet LO minimize fire hazard. Aluminum oxide abrasive wheels, such as 32A60-K8VBE (Norton), are recommended. 17.3...
Journal Articles
Alloy Digest (2000) 49 (11): Cb-25.
Published: 01 November 2000
..., but a heavy-duty, extreme pres- sure (EP) type cutting compound such as PMC 9318 has proven most sat- isfactory for producing fine finishes and holding close tolerances, especially in jet or mist spray applications. For surface grinding and cy- lindrical inner and outer diameter grinding, PMC 9305 or Cimcool...
Journal Articles
Alloy Digest (1973) 22 (8): Ni-194.
Published: 01 August 1973
... at I4OOuF for 16 hours. air LOOI. Machinability: MAR-M alloy 432 is machinable in all conditions WII~ proper techniques which are stmtlar to those used with the ausrenitlc stairJess steels. Heavy-duty vtbration-free ma&me tools should be used ior best results. Cutting rools must have smooth tool<hip contact...
Journal Articles
Alloy Digest (1967) 16 (6): SS-195.
Published: 01 June 1967
... to reprecipicare carbides at 1600 deg. F after hot forming or solution heat treatment. Forms Available: Bars, rods and plates. Applications: Annealing covers, high temperature tempering equip- ment, diesel and heavy duty exhaust systems, aircraft engine manifolds, refinery equipment, welded structures, jet...
Journal Articles
Alloy Digest (1961) 10 (11): SS-124.
Published: 01 November 1961
... carbides at 1600 deg. F after hot forming or solution heat treat- ment. Forms Available: Bats, rods, sheets, strips, plates, castings, and tubing. Applications: Annealing covers, high temperature tempering equipment, diesel antI heavy duty exhaust systems. aircrafr engine manifolds, refinery equipment...
Journal Articles
Alloy Digest (1954) 3 (4): Ti-3.
Published: 01 April 1954
... for drihing. Drill should never be allowed to ride in the hole. Keep cutting at aU times. Drills should have 130 deg. point angle, 10 deg. lip relief angle, 36 deg. helix angle and polished flutes. As in all titanium machining operations, slow speeds and coarse feeds are hportant. Heavy duty drills of short...