Accession Number:

AD0600717

Title:

STRUCTURAL INTEGRITY, ACCELERATED CORROSION AND FLOW CAPACITY TESTS OF PARKER AIRCRAFT COMPANY VALVE, CHECK, ONE-INCH, AIRBORNE, FUEL PARKER PART NUMBER 2630014. GD/A PART NUMBER 27-02402-5

Descriptive Note:

Test rept.

Corporate Author:

WYLE LABS EL SEGUNDO CA

Personal Author(s):

Report Date:

1964-01-01

Pagination or Media Count:

33.0

Abstract:

Two units were submitted for testing. The test program consisted of diameter measurements, accelerated corrosion, flow capacity and burst pressure tests. A 30-day accelerated corrosion test caused severe corrosion of the body base metal but, there was no evidence of stress corrosion cracking. The pressure drop was 5.2 psi allowable is 9 psi at a water flow rate of 70 gpm. The burst pressure of a unit free of corrosion was 5l00 psig. A unit previously subjected to a 30-day accelerated corrosion test demonstrated a burst pressure of 3650 psig. Minimum required burst pressure is 2400 psig. A detailed description of all tests and results, including a list of equipment employed in the performance of the test program, is presented in this report.

Subject Categories:

  • Pumps, Filters, Pipes, Tubing, Fittings and Valves

Distribution Statement:

APPROVED FOR PUBLIC RELEASE