|
US2021108532A1
|
|
Turbine shroud with friction mounted ceramic matrix composite blade track
|
|
EP3672196A1
|
|
A method and process for blockchain implementation with third party devices
|
|
US2021115877A1
|
|
Gas turbine engine with reversible heat exchanger
|
|
US2021108596A1
|
|
Flexible seal for gas turbine engine
|
|
US2021070417A1
|
|
Adjustable door seal
|
|
US2021071547A1
|
|
High temperature panel damper for sheet metal structures
|
|
CA3053117A1
|
|
Dual mode starter generator
|
|
US2020355121A1
|
|
Bleed expander cooling with turbine
|
|
US2020277871A1
|
|
Non-continuous abradable coatings
|
|
US2021009282A1
|
|
Method and tool for optimizing fuel/electrical energy storage allocation for hybrid-electric aircraft
|
|
US2020388018A1
|
|
Inspection Support Apparatus
|
|
CA3045263A1
|
|
Tight temperature control at a thermal load with a two phase pumped loop, optionally augmented with a vapor compression cycle
|
|
US2020370475A1
|
|
Inlet particle separator
|
|
EP3581679A1
|
|
Slurry-based coating system repair
|
|
US2020347743A1
|
|
Parallel hybrid propulsion system
|
|
US2020340400A1
|
|
Adaptive vertical lift engine (avle) fan
|
|
US2020332724A1
|
|
Systems and methods for controlling surge margin in the compressor section of a gas turbine engine
|
|
US2020332671A1
|
|
Blade tip clearance assembly
|
|
US2020332672A1
|
|
Blade tip clearance assembly with geared cam
|
|
US2020326113A1
|
|
Method for reducing condenser size and power on a heat rejection system
|
