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Conceptual Design of a Tiltrotor Transport Flight DeckA tiltrotor transport has considerable potential as a regional transport, increasing the air transportation system capacity by off-loading conventional runways. Such an aircraft will have a flight deck suited to its air transportation task and adapted to unique urban vertiport operating requirements. Such operations are likely to involve steep, slow instrument approaches for vertical and extremely short rolling take-offs and landings. While much of a tiltrotor transport's operations will be in common with commercial fixed-wing operations, terminal area operations will impose alternative flight deck design solutions. Control systems, displays and guidance, and control inceptors must be tailored to both routine and emergency vertical flight operations. This paper will survey recent experience with flight deck design elements suitable to a tiltrotor transport and will propose a conceptual cockpit design for such an aircraft. A series of piloted simulations using the NASA Ames Vertical Motion Simulator have investigated cockpit design elements and operating requirements for tiltrotor transports operating into urban vertiports. These experiments have identified the need for a flight director or equivalent display guidance for steep final approaches. A flight path vector display format has proven successful for guiding tiltrotor transport terminal area operations. Experience with a Head-Up Display points to the need for a bottom-mounted display device to maximize its utility on steep final approach paths. Configuration control (flap setting and nacelle angle) requires appropriate augmentation and tailoring for civil transport operations, flown to an airline transport pilot instrument flight rules (ATP-IFR) standard. The simulation experiments also identified one thrust control lever geometry as inappropriate to the task and found at least acceptable results with the vertical thrust control lever of the XV-15. In addition to the thrust controller, the attitude control of a tiltrotor transport may be effected through an inceptor other than the current center sticks in the XV-15 and V-22. Simulation and flight investigations of side-stick control inceptors for rotorcraft, augmented by a 1985 flight test of a side-stick controller in the XV-15 suggest the potential of such a device in a transport cockpit.
Document ID
20020034912
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Decker, William A.
(NASA Ames Research Center Moffett Field, CA United States)
Dugan, Daniel C.
(NASA Ames Research Center Moffett Field, CA United States)
Simmons, Rickey C.
(NASA Ames Research Center Moffett Field, CA United States)
Tucker, George E.
(NASA Ames Research Center Moffett Field, CA United States)
Aiken, Edwin W.
Date Acquired
August 20, 2013
Publication Date
January 1, 1995
Subject Category
Aircraft Design, Testing And Performance
Meeting Information
Meeting: SAE Aerotech Conference
Location: Los Angeles, CA
Country: United States
Start Date: September 19, 1995
End Date: September 21, 1995
Sponsors: Society of Automotive Engineers, Inc.
Funding Number(s)
PROJECT: RTOP 538-07-15
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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