This procurement specification covers aircraft quality bolts and screws made from a corrosion resistant, work-strengthened, cobalt-chromium-nickel alloy of the type identified under the Unified Numbering System as UNS R30035, and of 260 000 psi tensile strength at room temperature.
BOLTS AND SCREWS, COBALT-CHROMIUM-NICKEL ALLOY, CORROSION RESISTANT Forged Head, Roll Threaded After Aging, Fatigue Rated
17.01.1991
Aufsatz (Konferenz)
Englisch
SAE Technical Papers | 1991
SAE Technical Papers | 1991
SAE Technical Papers | 1995
BOLTS AND SCREWS, CORROSION-RESISTANT WORK-STRENGTHENED ALLOY Forged Head, Roll Threaded After Aging
SAE Technical Papers | 1991
SAE Technical Papers | 1991