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Patent applications and USPTO patent grants for Farrar; Peter G G.The latest application filed is for "gas turbine engine blade".
Patent | Date |
---|---|
Gas turbine engine blade Grant 6,524,074 - Farrar , et al. February 25, 2 | 2003-02-25 |
Gas turbine engine blade App 20020012587 - Farrar, Peter G.G. ;   et al. | 2002-01-31 |
Ducted fan gas turbine engine having a frangible connection Grant 6,009,701 - Freeman , et al. January 4, 2 | 2000-01-04 |
Mounting for coupling a turbofan gas turbine engine to an aircraft structure Grant 5,746,391 - Rodgers , et al. May 5, 1 | 1998-05-05 |
Variable stator vane arrangement for an axial flow compressor Grant 5,044,879 - Farrar September 3, 1 | 1991-09-03 |
Intake for a turbopropeller gas turbine engine Grant 4,796,424 - Farrar , et al. January 10, 1 | 1989-01-10 |
Control systems for multi-stage axial flow compressors Grant 4,252,498 - Radcliffe , et al. February 24, 1 | 1981-02-24 |
Compressor rotor stage Grant 4,177,013 - Patterson , et al. December 4, 1 | 1979-12-04 |
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