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Применить Всего найдено 4. Отображено 4.
30-08-2011 дата публикации

Apparatus and methods for testing performance of a material for use in a jet engine

Номер: US0008006544B2
Автор: Richard Holmes, Robert G. Tryon, III, John E. Pope, Daniel A. Nasser, Michael Oja, Animesh Dey, Jesse Hamler, Jonathan Brooks, James Tryon, HOLMES RICHARD, TRYON III ROBERT G, POPE JOHN E, NASSER DANIEL A, OJA MICHAEL, DEY ANIMESH, HAMLER JESSE, BROOKS JONATHAN, TRYON JAMES, TRYON, III ROBERT G., POPE JOHN E., NASSER DANIEL A.
Принадлежит: Vextec Corporation, VEXTEC CORP, VEXTEC CORPORATION

An apparatus for testing failure of a material used in a jet engine, and more particularly to an apparatus that uses one or more model jet engine components made from a material used in a full-size jet engine and desired to be tested. The apparatus permits easy removal and disassembly of a jet engine mounted thereon as well as real-time measurements of run-time parameters. The methods and apparatus provide for predicting and analysing failure by a number of fatigue-related mechanisms including creep, fatigue, crack growth, foreign object damage, fretting, erosion, and stress corrosion.

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Номер записи: 1
28-05-2009 дата публикации

Apparatus and method for testing performance of a material for use in a jet engine

Номер: US20090133381A1
Автор: Richard Holmes, Robert G. Tryon, III, John E. Pope, Daniel A. Nasser, Michael Oja, Animesh Dey, Jesse Hamler, Jonathan Brooks, James Tryon
Принадлежит: Vextec Corporation

An apparatus for testing failure of a material used in a jet engine, and more particularly to an apparatus that uses one or more model jet engine components made from a material used in a full-size jet engine and desired to be tested. The apparatus permits easy removal and disassembly of a jet engine mounted thereon as well as real-time measurements of run-time parameters. The methods and apparatus provide for predicting and analysing failure by a number of fatigue-related mechanisms including creep, fatigue, crack growth, foreign object damage, fretting, erosion, and stress corrosion.

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Номер записи: 2
21-06-2012 дата публикации

TESTING PERFORMANCE OF A MATERIAL FOR USE IN A JET ENGINE

Номер: US20120152007A1
Автор: Richard Holmes, Robert G. Tryon, II, John E. Pope, Michael Oja, Animesh Dey, Jesse Hamler, Jonathan Brooks, James Tryon, Daniel A. Nasser, A. Lorenz Nasser, HOLMES RICHARD, TRYON II ROBERT G, POPE JOHN E, OJA MICHAEL, DEY ANIMESH, HAMLER JESSE, BROOKS JONATHAN, TRYON JAMES, NASSER DANIEL A, NASSER A LORENZ, TRYON, II ROBERT G., POPE JOHN E., NASSER DANIEL A., NASSER A. LORENZ
Принадлежит:

An apparatus for testing failure of a material used in a jet engine, and more particularly to an apparatus that uses one or more miniature jet engine components made from a material used in a full-size jet engine and desired to be tested. The apparatus permits easy removal and disassembly of a jet engine mounted thereon as well as real-time measurements of run-time parameters. The methods and apparatus provide for predicting and analyzing failure by a number of fatigue-related mechanisms including creep, fatigue, crack growth, foreign object damage, fretting, erosion, and stress corrosion. The apparatus also permits testing of a component placed in the exhaust gases of a jet engine mounted therein.

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Номер записи: 3
24-07-2008 дата публикации

Apparatus and methods for testing performance of a material for use in a jet engine

Номер: WO2008088797A1
Автор: Animesh Dey, Daniel A. Nasser, James Tryon, Jesse Hamler, John E. Pope, Jonathan Brooks, Michael Oja, Richard Holmes, Robert G. Tryon, Iii
Принадлежит: VEXTEC CORPORATION

An apparatus for testing failure of a material used in a jet engine, and more particularly to an apparatus that uses one or more model jet engine components made from a material used in a full-size jet engine and desired to be tested. The apparatus permits easy removal and disassembly of a jet engine mounted thereon as well as real-time measurements of run-time parameters. The methods and apparatus provide for predicting and analysing failure by a number of fatigue-related mechanisms including creep, fatigue, crack growth, foreign object damage, fretting, erosion, and stress corrosion.

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Номер записи: 4