Turboshaft engine air particle separation
Tài liệu tham khảo
Stallard, 1997, Helicopter engine protection, Perfusion, 12, 263, 10.1177/026765919701200410
AGARD. Engine–airframe integration for rotorcraft. Technical report LS-148, AGARD, Neuilly sur Seine; 1986.
Seddon, 1999
Calcaterra J. Experimental and numerical simulation of FOD. RTO-TR-AVT-094, NATO-RTO; 2004 [chapter 3].
van der Walt, 1995, Life prediction of helicopter engines fitted with dust filters, J Aircraft, 32, 118, 10.2514/3.46691
van der Walt, 1995, Erosion of dust-filtered helicopter turbine engines. Part I: basic theoretical considerations, J Aircraft, 32, 106, 10.2514/3.56919
van der Walt, 1995, Erosion of dust-filtered helicopter turbine engines. Part II: erosion reductions, J Aircraft, 32, 112, 10.2514/3.46690
Warren J, Gorton C, Hoff S, Alby F. Effects of sand and dust on small gas turbine engines. RTO-TR-AVT-094, NATO-RTO; 2004 [chapter Annex B].
Haider, 1989, Drag coefficient and terminal velocity of spherical and non spherical particles, Powder Technol, 58, 63, 10.1016/0032-5910(89)80008-7
U.A.M. Department. Engineering design handbook. Helicopter engineering. Part one. Preliminary design. Pamphlet A-700200, Alexandria, VA; 1974.
Prinsloo W, Villiers P, Dijken M. Vortex tube separating device. US Patent 4,985,058, January 1991.
Campolong J. Vortex separator. US Patent 3,895,930, July 1975.
DRM, TER. Centrifugal separator. US Patent 4,008,069, February 15, 1977.
Monson D, Keller D, Rothman J. Deflecting element for centrifugal separators. US Patent 3,517,821, June 30, 1970.
Brockmann H. Multi-stage cyclone separator. US Patent 4,289,611, September 15, 1981.
Simpson T. Separator. US Patent 4,255,174, March 10, 1981.
Roach C. Vortex air cleaner assembly with acoustic attenuator. US Patent 4,050,913, September 27, 1977.
Shohet H, Amelio A, Kowalonek J. Engine inlet air particle separator. US Patent 3,449,891, June 17, 1969.
Duffy R, Shattuck B. Integral engine inlet particle separator. Design guide, vol. 2. Technical report, General Electric Co.; August 1975.
Pall Pea. Vortex air cleaner assembly having uniform particle removal. US Patent 3,520,114, July 14, 1970.
Ballard J. Impact of IPS and IRS configurations on engine installation design. Engine–airframe integration for rotorcraft, vol. AGARD LS-148. Essex, UK; 1986.
McAnally W, Schilling M. Investigation of feasibility of integral gas turbine engine solid particle inlet separators. Phase I. Feasibility study and design. Technical report, USAAVLABS TR-70-44; August 1970.
McAnally W, Schilling M. Investigation of feasibility of integral gas turbine engine solid particle inlet separators. Phase II. Feasibility demonstration. Technical report, USAAVLABS TR-71-13; April 1971.
Hobbs J. Gas turbine engine air intake. US Patent 4,389,227, June 21, 1983.
Stoten M. Integral inertial particle separator for radial inlet gas turbine. US Patent 6,134,874, October 24, 2000.
Barr S. Particle separator for turbine engines of aircraft. US Patent 3,993,463, November 23, 1976.
Richardson D, Wilkins W. Moisture and particle removing means for engines. US Patent 3,148,043, September 8, 1964.
Snyder P. Particle separator for a gas turbine engine. US Patent 6,698,180, March 2, 2004.
Hull T, Nye H. Particle separator with scroll scavenging means. US Patent 3,832,086, August 27, 1974.
Jenkins J, Sperinck J, Buller M. Inlet particle separator. US Patent 4,702,071, October 27, 1987.
McAnally W. Particle and moisture separator for engine inlet. US Patent 3,766,719, October 23, 1973.
Weinstein B, Steyer W. Foreign particle separator system. US Patent 4,265,646, May 5, 1981.
Hartman P. High particle separation efficiency system. US Patent 6,702,873 B2, March 9, 2004.
Higgins T. Adaptive inertial particle separator. EU Patent 1,908,939, April 9, 2008.
Hartman P, Meadowcroft C. Engine inlet air particle separator with active flow control. U.S. Patent 7,296,395 B1, November 20, 2007.
Hamed, 1995, Particle dynamics simulations in inlet separator with an experimentally based bounce model, J Propulsion & Power, 11, 230, 10.2514/3.51415
Vittal, 1986, Development of an advanced vaneless inlet particle separator for helicopter engines, J Propul, 2, 438, 10.2514/3.22926
Musgrove G, Barringer M, Thole K, Grover E, Barker J. Computational design of a louver particle separator for gas turbine engines. In: Proceedings of ASME Turbo Expo 2009: power for land, sea and air, Orlando, FL, 2009.
Saeed, 2007, Analysis method for inertial particle separator, J Aircraft, 44, 1150, 10.2514/1.20245
Taslim M, Khanicheh A, Spring S. A numerical study of sand separation applicable to engine inlet particle separator. AHS Journal 54(4).
Suhr S. Preliminary turboshaft engine design methodology for rotorcraft applications. Master's thesis, Georgia Institute of Technology; December 2006.
Scimone M. Aircraft engine air filter and method. US Patent 6,595,742, July 22, 2003.
Stelzer J, Newman T. Engine air filter and sealing system. US Patent 7,192,562 B2, March 20, 2007.
Bear, 1972
Chen, 2009, Cake formation and growth in cake filtration, Powder Technol, 192, 217, 10.1016/j.powtec.2008.12.014
Purchas D, Sutherland K. editors. In: Handbook of filter media, 2nd ed. Elsevier; 2002.
de Nevers, 1991
Dickenson T. editor. In: Filters and filtration handbook. Elsevier; 1997.
Visser W, Broomhead M. GSP: a generic object-oriented gas turbine simulation environment. In: ASME gas turbine conference, ASME 2000-GT-0002, Munich, Germany, 2000.
Visser, 2006, A generic approach for gas turbine adaptive modeling, ASME J Eng Gas Turbine Power, 128, 13, 10.1115/1.1995770