The History of the Xv-15 Tilt Rotor Research Aircraft from Concept to Flight

The History of the Xv-15 Tilt Rotor Research Aircraft from Concept to Flight
Author: Martin D. Maisel
Publisher: BiblioGov
Total Pages: 224
Release: 2013-06
Genre:
ISBN: 9781289146375

This monograph is a testament to the efforts of many people overcoming multiple technical challenges encountered while developing the XV-15 tilt rotor research aircraft. The Ames involvement with the tilt rotor aircraft began in 1957 with investigations of the performance and dynamic behavior of the Bell XV-3 tilt rotor aircraft. At that time, Ames Research Center was known as the Ames Aeronautical Laboratory of the National Advisory Committee for Aeronautics (NACA). As we approach the new millennium, and after more than 40 years of effort and the successful completion of our initial goals, it is appropriate to reflect on the technical accomplishments and consider the future applications of this unique aircraft class, the tilt rotor. The talented engineers, technicians, managers, and leaders at Ames have worked hard with their counterparts in the U.S. rotorcraft industry to overcome technology barriers and to make the military and civil tilt rotor aircraft safer, environmentally acceptable, and more efficient. The tilt rotor aircraft combines the advantages of vertical takeoff and landing capabilities, inherent to the helicopter, with the forward speed and range of a fixed wing turboprop airplane. Our studies have shown that this new vehicle type can provide the aviation transportation industry with the flexibility for highspeed, long-range flight, coupled with runway-independent operations, thus having a significant potential to relieve airport congestion. We see the tilt rotor aircraft as an element of the solution to this growing air transport problem.

The History of the XV-15 Tilt Rotor Research Aircraft

The History of the XV-15 Tilt Rotor Research Aircraft
Author: National Aeronautics and Space Administration
Publisher: CreateSpace
Total Pages: 220
Release: 2013-11-01
Genre: History
ISBN: 9781493648689

This monograph is a testament to the efforts of many people overcoming multiple technical challenges encountered while developing the XV-15 tilt rotor research aircraft. It is a comprehensive and detailed documentation of more than 40 years of effort at the NASA Ames Research Center designing this unique class of aircraft. The tilt rotor aircraft combines the advantages of vertical takeoff and landing capabilities, inherent to the helicopter, with the forward speed and range of a fixed wing turboprop airplane. NASA sees the tilt rotor as a new type of vehicle that will provide flexibility for high-speed, long-range flight, coupled with runway-independent operations. It takes the reader through the entire history, culminating with the first production of the V-22 Osprey, built for the U.S. Marine Corps, and the BA609 by Bell-Augusta. This publication takes the reader through the early ideas of Leonardo da Vinci through the search for an aircraft with Vertical Takeoff and Landing (VTOL) capabilities. There is abundant historical data about numerous innovative flying machines devised during the 1920s and 1930s, and German projects by Focke-Achgelis and Focke-Wulf. The publication includes illustrations from the 1930 flying machine patent of G. Lehberger, as well as the convertible aircraft patent of Haviland H. Platt (1955). The publication also describes how the XV-3 tilt rotor emerged from the Army/Air Force convertiplane program of the 1950s, and the evolution of tilt rotor, tilt wing, lift-fan, and direct lift versions and the evolution of the XV-3 program, which began in 1951. Flight tests are described in great detail, explaining the problems of stability. The development of tilt rotor aircraft technology involved some of the same factors that led to other important aeronautical accomplishments of this century. The vision of a few individuals in search of a practical and efficient new aircraft design, commitment to their goals, and their willingness to continue to pursue their objective while encountering major technical problems and programmatic challenges were critical ingredients in this tale. However, the unique aspect of the tilt rotor story was the combined Government and industry focused effort that was sustained for over four decades to explore, comprehend, develop, and refine this technology. The remarkable product of the investment of public and private funds, and the efforts of the people dedicated to the concept, is an aircraft type that will have an impact on civil and military aviation that will rival the introduction of the practical helicopter more than 60 years ago.

The History of the XV-15 Tilt Rotor Research Aircraft

The History of the XV-15 Tilt Rotor Research Aircraft
Author: National Aeronautics and Space Administration (NASA)
Publisher:
Total Pages: 193
Release: 2017-04-29
Genre:
ISBN: 9781521185155

This wonderful NASA history document tells the story of the successful development of the tilt rotor aircraft, which is not just about technology, but also about the efforts of many capable people who dedicated themselves to what they believed would be an important advancement in aviation. The tasks proved to be technically challenging and involved both high financial and safety risks. List of Acronyms * Introduction * Early Efforts * XV-3 Program * NASA-Army Cooperation * Building the Technology Base * Tilt Rotor Research Aircraft Project Office * Aircraft Development * Navy Participation * Flight Envelope Expansion * Flight Research Incidents * Paris Air Show * Evaluations and Demonstrations * Crash * The End of an Era * XV-15 Project Summary * Epilogue * Appendix A * Aircraft Descriptions * Appendix B * Key Personnel * Appendix C * Chronology * Appendix D * Awards and Records * Appendix E * Photo Gallery * Appendix F * Bibliography of Tilt Rotor Related Publications * Footnotes The XV-15 tilt rotor research aircraft program resulted in part from earlier investigations by the U.S. military seeking new and more efficient concepts for air support of field operations. The XV-3 tilt rotor emerged from the Army/Air Force convertiplane program of the 50s as a strong contender. However, it faced significant stability problems that discouraged many supporters and threatened to swamp the program. The program was continued by those in industry and Government who believed in the concept and its potential, and were willing to risk their investment. They were rewarded by the discovery of new techniques and the incorporation of new materials technology that made it possible to propose the XV-15 tilt rotor research aircraft project. It was my privilege to successfully advocate Army participation in the program with both funding and personnel. The unique aspects and synergistic values of the Army AARL/AMRDL-NASA interagency participation made this possible. It demonstrated the value of sharing resources in direct partnership toward common goals. Although not yet integrated into Army field strategies, the tilt rotor aircraft holds significant potential for consideration in future missions. The Marine V-22 Osprey demonstrates the rewards of the investment of defense dollars in the tilt rotor research aircraft project. There likely will be more.

Simulation of the XV-15 Tilt Rotor Research Aircraft

Simulation of the XV-15 Tilt Rotor Research Aircraft
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
Total Pages: 26
Release: 2018-07-21
Genre:
ISBN: 9781723407215

The effective use of simulation from issuance of the request for proposal through conduct of a flight test program for the XV-15 Tilt Rotor Research Aircraft is discussed. From program inception, simulation complemented all phases of XV-15 development. The initial simulation evaluations during the source evaluation board proceedings contributed significantly to performance and stability and control evaluations. Eight subsequent simulation periods provided major contributions in the areas of control concepts; cockpit configuration; handling qualities; pilot workload; failure effects and recovery procedures; and flight boundary problems and recovery procedures. The fidelity of the simulation also made it a valuable pilot training aid, as well as a suitable tool for military and civil mission evaluations. Simulation also provided valuable design data for refinement of automatic flight control systems. Throughout the program, fidelity was a prime issue and resulted in unique data and methods for fidelity evaluation which are presented and discussed. Churchill, G. B. and Dugan, D. C. Ames Research Center NASA-TM-84222, A-8848, NAS 1.15:84222 RTOP 532-04-11