Метрология / Том 2. Основы конструирования авиационных двигателей и энергетических установок / 8-12-Perechen_literatury

Контрольные вопросы

1.С решением каких проблем связано уменьшение числа ступеней при разработке перспективных турбин высокого давления?

2.За счет чего повышается эффективность турбин двухвальных двигателей при противоположном вращении роторов ТВД и ТНД?

3.В чем идея оптимизации взаимного углового расположения лопаточных решеток многоступенчатой турбины?

4.Назовите перспективные материалы для изготовления дисков и лопаток турбин.

5.Назовите перспективные направления совершенствования систем активного управления радиальными зазорами в турбинах.

Перечень использованной литературы

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8.3Thrust for Change. Flight International, 26 June – 2 July 2001.

8.4Mari C. Trends in the Technological Development of Aeroengines: An Overview. ISABE-2001-1012, 2001.

8.5GP7200: Quiet Power for the A380. Engine Yearbook 2003. Aviation Industry Press, 2003.

8.6Energy Efficient Engine. Low Pressure Turbine Subsonic Cascade Component Development and Integration Program. P&W/NASA CR-165592, 1982.

8.7Trent 900. Engine Yearbook 2004. Aviation Industry Press, 2004.

8.8GE Investing $1 Billion in 7E7’s GEnx Engine. Aviation Week Show News – Farnborough 2004, July 19, 2004.

8.9Walther R., Zarzalis N., Niehuis R. Designing Advanced Components for High Bypass Engines. ISABE 99-7109, 1999.

8.10Civil engine makers in for the long haul. INTERAVIA, November/December 2002.

8.11Ni R.-H. Advanced Modeling Techniques for New Commercial Engines. ISABE Paper 99-7043, 1999.

8.12Meece C. Gas Turbine Technologies of the Future. ISABE 95-7006, 1995.

8.13Mega-Rig. MTU Report, 1/2003.

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Advancement of Design Technology for Axial Flow Turbines. ISABE 2003-1035, 2003.

8.15Gonzalez P., Ulizar I. Advanced Low Pressure Turbine Design for a High By-pass RatioAero Engine. ISABE 2001-1061, 2001

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8.17Gupta D.K. Materials and Processes for Affordable and High Performance Propulsion Systems. ISABE-2001-1104.

8.18Steffens K., Wilhelm H. Next Engine Generation: Materials, Surface Technology, Manufacturing Processes. What comes after 2000? MTU Aero Engines, 2000.

8.19Aviation Week & Space Technology. February 23, 1998.

8.20Caesar Targets Tech Transfer. Aviation Week & Space Technology, February 9, 1998.

8.21Dailey G.M. Design and Calculation Issues. AeroThermal Performance of Internal Cooling Systems in Turbomachines. Lecture Series 2000-03. Von Karman Institute for Fluid Dynamics, 2000.

8.22No Surprises.Aviation Week & Space Technology. August 25, 2003.

8.23Gier J., Stubert B., Brouillet B., De Vito l. Interaction of Shroud Leakage Flow and Main Flow in a Three-Stage LP Turbine. GT2003-38025. Proceedings of ASME Turbo Expo 2003.

8.24Horlock J.H., Denton J.D. A Review of some design practice using CFD and a current perspective. GT2003-38973. ASME TURBO EXPO 2003.

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8.26General Electric Aims At 18-Month Engine. Aviation Week & Space Technology, October 21, 2002.