|
EP3550106A1
|
|
Cooling air for gas turbine engine with thermally isolated cooling air delivery
|
|
EP2960467A1
|
|
Simplified engine bleed supply with low pressure environmental control system for aircraft
|
|
US2019003382A1
|
|
Geared turbofan engine with low pressure environmental control system for aircraft
|
|
US2014216056A1
|
|
Heat exchange module for a turbine engine
|
|
US2013318998A1
|
|
Geared turbofan with three turbines with high speed fan drive turbine
|
|
US2013283819A1
|
|
Geared turbofan with three turbines all co-rotating
|
|
US2013125561A1
|
|
Geared turbofan with distributed accessory gearboxes
|
|
US2013192191A1
|
|
Gas turbine engine with high speed low pressure turbine section and bearing support features
|
|
US2013195648A1
|
|
Gas turbine engine with high speed low pressure turbine section and bearing support features
|
|
US2013192265A1
|
|
Gas turbine engine with high speed low pressure turbine section and bearing support features
|
|
US2013259653A1
|
|
Geared turbofan engine with power density range
|
|
US2013255275A1
|
|
Geared turbofan engine with power density range
|
|
US2013259643A1
|
|
Geared turbofan with three turbines with first two counter-rotating, and third co-rotating with the second turbine
|
|
US2013255219A1
|
|
Geared turbofan with three co-rotating turbines
|
|
US2013259650A1
|
|
Geared turbofan with three turbines with first two co-rotating and third rotating in an opposed direction
|
|
US2013224049A1
|
|
Gas turbine engine with stage dependent material selection for blades and disk
|
|
US2013195624A1
|
|
Geared turbofan engine with counter-rotating shafts
|
|
US2013219907A1
|
|
Geared turbofan architecture for improved thrust density
|
|
US2013223974A1
|
|
Variable area turbine
|
|
US2013167555A1
|
|
Aluminum fan blade construction with welded cover
|
