DEVELOPMENT OF HIGH TEMPERATURE AIRCRAFT ELECTRICAL SYSTEM

Abstract

DESCRIPTORS: (*Aircraft carriers, *Boilers, Combustion, Control systems, Design.) (Naval vessels, *Pressure regulators, Blowers, Gas flow, Steam, Air.) Identifiers: CVA66.A combustion control system suitable for use without combustion control dampers was developed for use on CVA66 boilers. This is a conventional steam pressure control system with air flow and oil flow sub-loops; additional modes were added to develop boiler steam flow rate of change augmenting air flow demand, and air flow rate of change augmenting air flow feedback within the air flow loop. This arrangement is designed to produce rapid response of the combustion controls to changes in air flow conditions as well as to changes in boiler load. Optimum system response is possible because of excellent dynamic response of the forced draft blowers. As finally developed, the system is recommended for use on CVA66. (Author)

Document Details

Document Type
Technical Report
Publication Date
Sep 20, 1961
Accession Number
AD0271895

Entities

People

  • D.l. Burkholder

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Flow
  • Aircraft Carriers
  • Combustion
  • Control Systems
  • Dynamic Response
  • Flow
  • Flow Rate
  • Gas Flow
  • High Temperature
  • Naval Vessels
  • Pressure Regulators
  • Regulators

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Robotics and Automation.