The ABC™ Rotor - A historical perspective

Annual Forum Proceedings - American Helicopter Society

Volumn 2, Issue , 2004, Pages 2306-2352

  Burgess, Robert K ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AUXILIARY PROPULSION CONFIGURATION; ORTHOGONALITY; PHASE ANGLE;

AIRCRAFT; CONTROL SYSTEMS; FATIGUE OF MATERIALS; NATURAL FREQUENCIES; SPEED CONTROL; STRUCTURAL LOADS; TURBOMACHINE BLADES; VIBRATIONS (MECHANICAL); WAKES; WIND TUNNELS;

HELICOPTER ROTORS;

EID: 4143087018     PISSN: 07334249     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (9)

1. U.S. Patent No. 3,409,249 issued November 5, 1968 to R.R. Bergquist, et al assignors to United Aircraft Corporation, E. Hartford, Connecticut
2. Cheney, M.C., Jr., THE ABC HELICOPTER, AIAA Paper No. 69-217 presented at the joint AIAA/AHS VTOL Research, Design and Operations Meeting, February 17 -19, 1969
3. FULL-SCALE WIND TUNNEL INVESTIGATION OF THE ADVANCING BLADE CONCEPT ROTOR SYSTEM, USAAVLABS Technical Report 71-25, Eustis Directorate, U.S. Army Air Mobility R&D Lab, Fort Eustis, VA, August 1971, AD 734338
4. th Annual National V/STOL Forum of the American Helicopter Society, Washington, D.C., May, 1971
5. Specification No. 712B, T400-CP-400 ENGINE SPECIFICATION, Pratt & Whitney of Canada, Ltd.
6. JT12 INSTALLATION HANDBOOK, Pratt and Whitney Aircraft, 14 April 1966
7. Curtiss, H.C., et al, AN EXPERIMENTAL INVESTIGATION OF THE LOW SPEED TRIM AND STABILITY CHARACTERISTICS OF A COAXIAL HELICOPTER WITH HINGELESS ROTOR ON THE PRINCETON DYNAMIC MODEL TRACK, Princeton University, TRN 1196, September 1974
8. Phelps, A.E., and Mineck, R.E., AERODYNAMICS CHARACTERISTICS OF A COUNTER-ROTATING, COAXIAL, HINGELESS ROTOR HELICOPTER MODEL, NASA TN-78705, May 1978
9. ADVANCING BLADE CONCEPT (ABC) TECHNOLOGY DEMONSTRATOR, A.J. Ruddell, etal; SIKORSKY AIRCRAFT DIVISION, UNITED TECHNOLOGIES CORPORATION, Stratford, Connecticut 06602 April, 1981