Books on the topic 'Helicopter transmissions'

Chaiko, Lev. Assessment of worm gearing for helicopter transmissions. [Washington, DC]: National Aeronautics and Space Administration, 1990.

Choy, Fred K. Dynamics analysis of multimesh-gear helicopter transmissions. Cleveland, Ohio: Lewis Research Center, 1988.

Michael, Savage. System life and reliability modeling for helicopter transmissions. Cleveland, Ohio: Lewis Research Center, 1986.

Savage, M. System life and reliability modeling for helicopter transmissions. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

Krantz, Timothy L. Experimental and analytical evaluation of efficiency of helicopter planetary stage. Cleveland, Ohio: Lewis Research Center, 1990.

Handschuh, Robert F. Experimental testing of prototype face gears for helicopter transmissions. [Washington, DC: National Aeronautics and Space Administration, 1992.

Lewicki, David G. Vibration characterstics of OH-58A helicopter main rotor transmission. Cleveland, Ohio: Lewis Research Center, 1987.

Lewicki, David G. Evaluation of an oil-debris monitoring guide for use in helicopter transmissions. [Washington, DC]: National Aeronautics and Space Administration, 1992.

Lewicki, David G. Evaluation of an oil-debris monitoring guide for use in helicopter transmissions. [Washington, DC]: National Aeronautics and Space Administration, 1992.

Lewicki, David G. Evaluation of an oil-debris monitoring guide for use in helicopter transmissions. [Washington, DC]: National Aeronautics and Space Administration, 1992.

Lewicki, David G. Evaluation of an oil-debris monitoring device for use in helicopter transmissions. [Washington, DC]: National Aeronautics and Space Administration, 1992.

Mitchell, Andrew M. Testing of YUH-61A helicopter transmission in NASA Lewis 2240-kW (3000-hp) Facility. Cleveland, Ohio: Lewis Research Center, 1986.

Folenta, Dezi. Design, manufacture, and spin test of high contact ratio helicopter transmission utilizing self-aligning bearingless planetary (SABP). [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

Mitchell, Andrew M. Testing of UH-60A helicopter transmission in NASA Lewis 2240-kW (3000-hp) Facility. Cleveland, Ohio: Lewis Research Center, 1986.

White, Graham. 3600 HP split torque helicopter transmission: Final report. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.

Lewicki, David G. Full-scale transmission testing to evaluate advanced lubricants. [Washington, DC]: National Aeronautics and Space Administration, 1992.

Lewicki, David G. Full-scale transmission testing to evaluate advanced lubricants. [Washington, DC]: National Aeronautics and Space Administration, 1992.

Lewicki, David G. Full-scale transmission testing to evaluate advanced lubricants. [Washington, DC]: National Aeronautics and Space Administration, 1992.

Handschuh, Robert F. Efficiency testing of a helicopter transmission planetary reduction stage. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

Lewicki, David G. Vibration characteristics of OH-58A helicopter main rotor transmission. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

Oswald, Fred B. Gear tooth stress measurements on the UH-60A helicopter transmission. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

Oswald, Fred B. Gear tooth stress measurements on the UH-60A helicopter transmission. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

Oswald, Fred B. Gear tooth stress meaurements on the UH-60A helicopter transmission. Cleveland, Ohio: Lewis Research Center, 1987.

Rovenstine, Michael J. Classification analysis of vibration data from SH-60B Helicopter Transmission Test Facility. Monterey, Calif: Naval Postgraduate School, 1997.

Lewicki, David G. Transmission research activities at NASA Lewis Research Center. [Washington, DC]: National Aeronautics and Space Administration, 1990.

Lewicki, David G. Transmission research activities at NASA Lewis Research Center. [Washington, DC]: National Aeronautics and Space Administration, 1990.

Anderson, Gregory L. Classification analysis of vibration data from SH-60B Helicopter Transmission Test Facility. Monterey, Calif: Naval Postgraduate School, 1997.

Lewicki, David G. Development of a full-scale transmission testing procedure to evaluate advanced lubricants. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

Lewicki, David G. Development of a full-scale transmission testing procedure to evaluate advanced lubricants. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

Lewicki, David G. Development of a full-scale transmission testing procedure to evaluate advanced lubricants. Cleveland, Ohio: Lewis Research Center, 1992.

Lewicki, David G. Development of a full-scale transmission testing procedure to evaluate advanced lubricants. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

Symposium of the AGARD Propulsion and Energetics Panel (64th 1984 Lisbon, Portugal). Gears and power transmission systems for helicopters and turboprops: Papers presented at the Propulsion and Energetics Panel 64th symposium held in Lisbon, Portugal, 8-12 October 1984. Neuilly sur Seine, France: AGARD, North Atlantic Treaty Organization, 1985.

Advisory Group for Aerospace Research and Development. Propulsion and Energetics Panel. Symposium. Gears and power transmission systems for helicopters and turboprops: Papers presented at the Propulsion and Energetics Panel 64th symposium, held in Lisbon, Portugal, 8-12 October 1984. Neuilly sur Seine: Agard, 1985.

P, Townsend Dennis, Oswald Fred B, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Dynamic analysis of multimesh-gear helicopter transmissions. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

United States. National Aeronautics and Space Administration., ed. Assessment of worm gearing for helicopter transmissions. [Washington, DC]: National Aeronautics and Space Administration, 1990.

L, Litvin F., United States. Army Aviation Systems Command., and United States. National Aeronautics and Space Administration., eds. Application of face-gear drives in helicopter transmissions. [Washington, DC: National Aeronautics and Space Administration, 1992.

Application of face-gear drives in helicopter transmissions. [Washington, DC: National Aeronautics and Space Administration, 1992.

L, Litvin F., United States. Army Aviation Systems Command., and United States. National Aeronautics and Space Administration., eds. Application of face-gear drives in helicopter transmissions. [Washington, DC: National Aeronautics and Space Administration, 1992.

P, Townsend Dennis, United States. Army Aviation Research and Technology Activity., and United States. National Aeronautics and Space Administration., eds. Effect of advanced component technology on helicopter transmissions. [Washington, DC]: National Aeronautics and Space Administration, 1989.

Application of face-gear drives in helicopter transmissions. [Washington, DC: National Aeronautics and Space Administration, 1992.

F, Handschuh Robert, United States. National Aeronautics and Space Administration., and United States. Army Aviation Research and Technology Activity., eds. Efficiency study comparing two helicopter planetary reduction stages. [Washington, D.C.]: NASA, 1990.

G, Lewicki David, United States. National Aeronautics and Space Administration., and U.S. Army Research Laboratory., eds. Low-noise, high-strength, spiral-bevel gears for helicopter transmissions. [Washington, DC: National Aeronautics and Space Administration], 1993.

G, Lewicki David, United States. National Aeronautics and Space Administration., and U.S. Army Research Laboratory., eds. Low-noise, high-strength, spiral-bevel gears for helicopter transmissions. [Washington, DC: National Aeronautics and Space Administration], 1993.

G, Lewicki David, United States. National Aeronautics and Space Administration., and U.S. Army Research Laboratory., eds. Low-noise, high-strength, spiral-bevel gears for helicopter transmissions. [Washington, DC: National Aeronautics and Space Administration], 1993.

G, Lewicki David, United States. National Aeronautics and Space Administration., and U.S. Army Research Laboratory., eds. Low-noise, high-strength, spiral-bevel gears for helicopter transmissions. [Washington, DC: National Aeronautics and Space Administration], 1993.

Cost benefit analysis of a 9-centistoke lubricant for helicopter transmissions: Under contract NAS2-14118. [Washington, DC]: National Aeronautics and Space Administration, 1997.

Cost benefit analysis of a 9-centistoke lubricant for helicopter transmissions: Under contract NAS2-14118. [Washington, DC]: National Aeronautics and Space Administration, 1997.

B, Oswald Fred, Schuller Fredrick T, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Testing of YUH-61A helicopter transmission in NASA Lewis 2240-kW (3000-hp) facility. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

B, Oswald Fred, Schuller Fredrick T, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Testing of YUH-61A helicopter transmission in NASA Lewis 2240-kW (3000-hp) facility. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

B, Oswald Fred, Schuller Fredrick T, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Testing of YUH-61A helicopter transmission in NASA Lewis 2240-kW (3000-hp) facility. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.