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SAE ARP1795A

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This document establishes a test procedure for determining the propensity of aircraft turbine engine cleaning and maintenance materials for causing stress-corrosion cracking of titanium alloy parts. The evaluation is conducted on representative titanium alloys by determining the effect of contact with cleaning and maintenance materials on tendency of pre-stressed titanium alloys to crack when subsequently heated to elevated temperatures.

Julkaisun tiedot

  • Standardi julkaisijalta SAE International
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  • Julkaisutyyppi: IS
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  • Publisher SAE International
  • Distributor SAE International

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