LIFT FAN PROPULSION SYSTEMS V/STOL AIRCRAFT CONTROL THE GENERAL ELECTRIC CO

Format:

Conference/Event

Author/Creator:

Beeler, E. F., author.

Conference Name:

Aeronautic and Space Engineering and Manufacturing Meeting (1965-10-04 : Los Angeles, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1965

Summary:

This paper discusses aircraft control power requirements provided by lift fan systems. Gas power transfer is described and estimated performance presented. A performance comparison is made between the thrust spoiling system used in the present Army XV-5A flight research vehicle and a gas power transfer system. Gas power can provide adequate aircraft control forces. Thrust spoiling is not needed for fan dynamic response, use of a phase lead network in the control circuit of a gas power transfer system can provide sufficiently rapid fan dynamic response

Notes:

Vendor supplied data

Publisher Number:

650831

Access Restriction:

Restricted for use by site license