Patent | Date |
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Posture enhancement device Grant 11,241,327 - Weiler , et al. February 8, 2 | 2022-02-08 |
Posture enhancement device Grant 10,213,331 - Weiler , et al. Feb | 2019-02-26 |
Jet engine with compact arrangement of fan Grant 7,487,630 - Weiler February 10, 2 | 2009-02-10 |
Arrangement comprising a slinger associated with a shaft bearing and a gasket associated with a sealing gap Grant 7,134,667 - Weiler November 14, 2 | 2006-11-14 |
Jet engine with compact arrangement of fan App 20060236675 - Weiler; Wolfgang | 2006-10-26 |
Arrangement comprising a slinger associated with a shaft bearing and a gasket associated with a sealing gap App 20040188946 - Weiler, Wolfgang | 2004-09-30 |
Abradable layer for a turbo-engine and a manufacturing process Grant 5,326,647 - Merz , et al. July 5, 1 | 1994-07-05 |
Arrangement for the sealing-off of spaces acted upon by media of different pressures for turbomachinery and the like Grant 4,998,739 - Weiler March 12, 1 | 1991-03-12 |
Gas turbine power plant arrangement Grant 4,899,959 - Weiler February 13, 1 | 1990-02-13 |
Cooled gas turbine operable with a controlled cooling air quantity Grant 4,709,546 - Weiler December 1, 1 | 1987-12-01 |
Gas turbine engine having a minimal blade tip clearance Grant 4,578,942 - Weiler April 1, 1 | 1986-04-01 |
Arrangement for maintaining clearances between a turbine rotor and casing Grant 4,439,982 - Weiler , et al. April 3, 1 | 1984-04-03 |
Apparatus for operating shut-off members in gas turbine engines, particularly in turbojet engines Grant 4,390,318 - Weiler June 28, 1 | 1983-06-28 |
Variable stator cascades for axial-flow turbines of gas turbine engines Grant 4,314,791 - Weiler February 9, 1 | 1982-02-09 |
Compressor rotor wheel and method of making same Grant 4,273,512 - Weiler June 16, 1 | 1981-06-16 |
Gas turbine engine Grant 4,264,272 - Weiler April 28, 1 | 1981-04-28 |
Variable flow divider for turbomachines Grant 4,261,686 - Weiler April 14, 1 | 1981-04-14 |
Apparatus for operating shut-off members in gas turbine engines, particularly in turbojet engines Grant 4,253,797 - Weiler March 3, 1 | 1981-03-03 |
Fuel injection nozzle assembly for gas turbine drive Grant 4,229,944 - Weiler October 28, 1 | 1980-10-28 |
Combustion chamber, especially annular reverse-flow combustion chamber for gas turbine engines Grant 4,203,283 - Weiler May 20, 1 | 1980-05-20 |
Gas turbine engine Grant 4,147,026 - Weiler April 3, 1 | 1979-04-03 |