|
US2014053533A1
|
|
Reverse flow gas turbine engine with thrust reverser
|
|
US2012308381A1
|
|
Integrally bladed rotor with slotted outer rim
|
|
US2013014490A1
|
|
Gas turbine engine with low stage count low pressure turbine
|
|
US2013291514A1
|
|
Gas turbine engine oil tank
|
|
US2013108413A1
|
|
Secondary flow arrangement for slotted rotor
|
|
US2013287565A1
|
|
TEC mount redundant fastening
|
|
US2013287545A1
|
|
Geared turbofan with three turbines all counter-rotating
|
|
US2013259638A1
|
|
Turbomachine thermal management
|
|
US2013259639A1
|
|
Turbomachine thermal management
|
|
US2013259687A1
|
|
Turbomachine thermal management
|
|
US2013259672A1
|
|
Integrated inlet vane and strut
|
|
US2013239588A1
|
|
Pump system for TMS AOC reduction
|
|
US2013239583A1
|
|
Bypass air-pump system within the core engine to provide air for an environmental control system in a gas turbine engine
|
|
US2013239582A1
|
|
Constant speed pump system for engine ECS loss elimination
|
|
US2013239584A1
|
|
Constant-speed pump system for engine thermal management system AOC reduction and environmental control system loss elimination
|
|
US2013232768A1
|
|
Turbine engine case mount and dismount
|
|
US2013233997A1
|
|
Turbine engine case mount
|
|
US2013192263A1
|
|
Gas turbine engine with high speed low pressure turbine section
|
|
US2013219859A1
|
|
Counter rotating low pressure compressor and turbine each having a gear system
|
|
US2013219860A1
|
|
Counter-rotating low pressure turbine without turbine exhaust case
|
