Assignee
TURBO PROPULSORES IND
US·9 granted patents·2 pending applications·135 citations·filing 1993–2015
Top patents by PatentIndex Score
11 records- 0151US5332357AStator vane assembly for controlling air flow in a gas turbine engienTURBO PROPULSORES IND·Filed 1993·Granted Jul 26, 1994·26 cites·7 claims
- 0248US6378781B1Exit area control mechanism for convergent divergent nozzlesTURBO PROPULSORES IND·Filed 2000·Granted Apr 30, 2002·18 cites·7 claims
- 0341US6148608ADivergent petal arrangement for a convergent-divergent aircraft engine nozzleTURBO PROPULSORES IND·Filed 1998·Granted Nov 21, 2000·17 cites·5 claims
- 0441US6102307ALoad strut for a variable geometry nozzleTURBO PROPULSORES IND·Filed 1998·Granted Aug 15, 2000·17 cites·2 claims
- 0539US6192671B1Cross bar centering mechanism for slave petals in covergent divergent nozzles with variable geometryTURBO PROPULSORES IND·Filed 1998·Granted Feb 27, 2001·21 cites·2 claims
- 0639US2008240972A1Low-density directionally solidified single-crystal superalloysTURBO PROPULSORES IND·Filed 2007·Application pending·0 cites
- 0735US5316438AGas turbine engine variable aerofoil vane actuation mechanismTURBO PROPULSORES IND·Filed 1993·Granted May 31, 1994·10 cites·7 claims
- 0833US6382076B1Piston servo-actuation main system with hydromechanically self-contained detectionTURBO PROPULSORES IND·Filed 1999·Granted May 7, 2002·9 cites·6 claims
- 0931US6311478B1Guiding mechanism for variable geometry vectoring nozzlesTURBO PROPULSORES IND·Filed 1999·Granted Nov 6, 2001·13 cites·6 claims
- 1023US2015275674A1Gas turbine rotorTURBO PROPULSORES IND·Filed 2015·Application pending·0 cites
- 1116US6098400ADivergent petal for gas turbine engine nozzleTURBO PROPULSORES IND·Filed 1998·Granted Aug 8, 2000·4 cites·5 claims
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Counts cover granted patents and pending applications in the PatentIndex corpus. How scoring works →