SUPERSONIC TRANSPORT AIRCRAFT ENGINE. PHASE II-B. DEVELOPMENT PROGRAM FUEL CONTROL SYSTEM STUDY. APPENDIX B.

Abstract

Hamilton Standard, under contract to Pratt and Whitney Aircraft, has conducted a design and development study to conceive and optimize, within contract and time limitations, a fuel control system for the P and WA SST engine. This effort consisted of design and analytical studies, material investigations, and development efforts necessary to adapt current state-of-the-art concepts and new concepts into a fuel control system compatible with the SST environments, envelope requirements, and accuracy tolerances specified for this application. The system decided upon and studied is a hydromechanical unitized concept featuring high reliability, ease of maintenance, durability, and low overall system weight. This report covers all studies conducted under Phase 2 B of the contract for the fuel control system as well as Hamilton Standard funded elastomeric seal development work.

Document Details

Document Type
Technical Report
Publication Date
Jun 30, 1965
Accession Number
AD0807390

Entities

Organizations

  • Pratt & Whitney

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Accuracy
  • Aircraft Engines
  • Aircrafts
  • Contracts
  • Control Systems
  • Engines
  • High Reliability
  • Reliability
  • Standards
  • Supersonic Transport Aircraft
  • Transport Aircraft

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Software Engineering

Technology Areas

  • Hypersonics