Accession Number:

AD0271895

Title:

DEVELOPMENT OF HIGH TEMPERATURE AIRCRAFT ELECTRICAL SYSTEM

Descriptive Note:

Corporate Author:

NORTH AMERICAN AVIATION INC LOS ANGELES CALIF

Personal Author(s):

Report Date:

1961-09-20

Pagination or Media Count:

1.0

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

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE