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Using Engine Thrust for Emergency Flight Control: MD-11 and B-747 ResultsWith modern digital control systems, using engine thrust for emergency flight control to supplement or replace failed aircraft normal flight controls has become a practical consideration. The NASA Dryden Flight Research Center has developed a propulsion-controlled aircraft (PCA) system in which computer-controlled engine thrust provides emergency flight control. An F-15 and an MD-11 airplane have been landed without using any flight control surfaces. Preliminary studies have also been conducted that show that engines on only one wing can provide some flight control capability if the lateral center of gravity can be shifted toward the side of the airplane that has the operating engine(s). Simulator tests of several airplanes with no flight control surfaces operating and all engines out on the left wing have all shown positive control capability within the available range of lateral center-of-gravity offset. Propulsion-controlled aircraft systems that can operate without modifications to engine control systems, thus allowing PCA technology to be installed on less capable airplanes or at low cost, are also desirable. Further studies have examined simplified 'PCA Lite' and 'PCA Ultralite' concepts in which thrust control is provided by existing systems such as auto-throttles or a combination of existing systems and manual pilot control.
Document ID
19980148010
Acquisition Source
Armstrong Flight Research Center
Document Type
Reprint (Version printed in journal)
Authors
Burcham, Frank W., Jr.
(NASA Dryden Flight Research Center Edwards, CA United States)
Maine, Trindel A.
(NASA Dryden Flight Research Center Edwards, CA United States)
Burken, John J.
(NASA Dryden Flight Research Center Edwards, CA United States)
Bull, John
(Caelum Research Corp. Moffett Field, CA United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1998
Subject Category
Air Transportation And Safety
Report/Patent Number
NASA/TM-1998-206552
NAS 1.15:206552
H-2232
Report Number: NASA/TM-1998-206552
Report Number: NAS 1.15:206552
Report Number: H-2232
Meeting Information
Meeting: Aviation Safety Issues: Gas Turbine and Aeroengine Technical Congress Exposition and Users Symposium
Location: Stockholm
Country: Sweden
Start Date: June 2, 1998
End Date: June 5, 1998
Sponsors: American Society of Mechanical Engineers
Funding Number(s)
PROJECT: RTOP 522-15-34
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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