Skip Nav Destination
Search Results for aircraft generator laminations
1-10 of 10 Search Results for
aircraft generator laminations
Alloy Digest (2004) 53 (4): Fe-128.
Published: 01 April 2004
... Rotelloy 3 has the same composition as Permandur 49 and was specifically developed for aircraft generator rotor and stator laminations. In addition to a slightly improved magnetic performance, this grade is supplied with guaranteed minimum mechanical properties. This alloy complies...
Alloy Digest (1992) 41 (5): Cp-22.
Published: 01 May 1992
... consolidation is recommended. Cool down at a rate of O.S C/min to the dry T of 25O C. then 3.O C/min to 60°C at which point the i autoc ave pressure is released and the part removed. The laminates have reprocess- ing and reforming potential. General Characteristics: The superior toughness and elongation...
Alloy Digest (1956) 5 (5): Ni-26.
Published: 01 May 1956
... MECHANICAL PROPERTIES Mechanical Annealed Cold-Worked Hydrogen Annealed Tensile strength? psi 82000 140000 65000 Yield point, PSI 31000 Eloneation. % in 2 41 Red&on of area, % Brinell hardness Rockwell hardness 15; ii000 ;: Table 4 - D-C MAG NETIZATION DATA (Laminations) H-Oersteds BKilOgaUSSCS 0.1 8.5 0.2...
Alloy Digest (1999) 48 (11): Co-107.
Published: 01 November 1999
...- chanical strengths with only a slight sacrifice in magnetic properties. The higher strength of Hiperco 50 is necessary for rotating component laminations subject to stress from high ro- tational speeds. Hiperco 50 has been used in strip form primar- ily for aircraft generators and motors. Contact...
Alloy Digest (1961) 10 (5): Fe-19.
Published: 01 May 1961
... transformers. General Purpose transformer. Space Factor 95% 4MIL H or Z Type 400 to 2600 cycles: Radio power, filament, rectifier transformers and chokes. Induction beating and ocher electronic trans- former applications. Aircraft power transformers. 90% 2MrL L Type 1 MIL M Tee Above 2600 cycles: Power pulse...
Alloy Digest (1998) 47 (10): Ti-105.
Published: 01 October 1998
... 250 1455 211 4.8 80 1738 252 1420 206 5.0 Aged at 482 C (900 F) for 20 h Table 3 Silicon Carbide (Sic): Metal Matrix Compos- ites, Typical Laminate Tensile Properties Te#llpClYtIlrC Lknsitv C - OF kg/& - -Cemikstmmh Ibh.~ MPa ii Elastic modulus GP¶ 1WLtSi 21 70 4240 0.153 1724 250 I86 27 538 loo0...
Alloy Digest (1990) 39 (11): Cp-11.
Published: 01 November 1990
... over one under 4HS: one over three under harness satin weave. Combined solvent and water of reaction. DOI: 10.31399/asm.ad.cp0011 Copyright © ASM International® 1996 Table 3 - TYPICAL AVIMID@ N /GRAPHITE LAMINATE PROPERTIES* Test Prepeg Code Number Temp., F FD1045 FD1046 FD1047 Thickness, in. 0.25...
Alloy Digest (1965) 14 (4): Mo-6.
Published: 01 April 1965
... or other material with a low coefficient of friction. Steel dies should be well lubricated with light oil. Punching and shearing dies should be kept sharp co avoid laminations and cracking of the sheet. Light gauges of sheet under 0.020 in thickness can be sheared easily at room temperature. Heavier gauge...
Alloy Digest (1960) 9 (4): Mo-1.
Published: 01 April 1960
...-TIME TENSILE PROPERTIES (9070 or more hot-coId work + I hr. at 1800°F stress relief) Powder Metahrgy Data Test Tensile Yield (Does not coincide with arc-cast, generally) Temperature StXllgth Strengtb Egy$? (0.040 sheet-stress relieved) OF Psi psi Test Ultimate Strength 112000 107000 (30) T psi iii...
Alloy Digest (1961) 10 (5): Mo-2.
Published: 01 May 1961
..., punching, shearing, and spinning. Drawing dies should be made of aluminum bronze or ochec material wiL a low coefficient of friction. Steel dies should be well lubticated witb light oil. Punching and shearing dies should be kept sharp to avoid lamin- ations and crackin under 0 020 in tii of the sheet...