Accession Number : ADA020022

Title :   High-Performance Vane Pump for Aircraft Hydraulic Systems.

Descriptive Note : Final rept. 20 Mar 72-18 Oct 75,

Corporate Author : BATTELLE COLUMBUS LABS OHIO

Personal Author(s) : Thomas,David L.

Report Date : DEC 1975

Pagination or Media Count : 105

Abstract : The purpose of this hydraulic-pump technology-development project was to investigate the feasibility and applicability and to demonstrate the capability of new vane-pump concepts to meet future aircraft hydraulic-system requirements. The specific objective was the development of a pressure-compensated hydraulic pump to deliver 45 gpm at 4000 psi while operating at 30,000 rpm with MIL-H-5606B hydraulic fluid. The new pump concepts were the product of previous Air Force programs and included a pivoting-tip vane for hydrodynamic load support and a two-lobed deformable cam ring for variable displacement. During this program both component experiments and pump evaluations were performed.

Descriptors :   *Jet aircraft, *Hydraulic pressure pumps, Pump components, Cams, Bearings, Shafts(Machine elements), Seals(Stoppers), Fabrication

Subject Categories : Aircraft
      Hydraulic and Pneumatic Equipment
      Pumps, Filters, Pipes, Tubing, Fittings & Vlvs

Distribution Statement : APPROVED FOR PUBLIC RELEASE