Inventor

SCHWARZ FREDERICK M

US307 patents

⚠️ This page may combine multiple inventors who share the name “SCHWARZ FREDERICK M”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

SCHWARZ FREDERICK M

UNITED TECHNOLOGIES CORP

Geared turbofan gas turbine engine architecture

Geared architecture for high speed and small volume fan drive turbine

Geared architecture for high speed and small volume fan drive turbine

Geared turbofan engine gearbox arrangement

Fundamental gear system architecture

Geared architecture for high speed and small volume fan drive turbine

Cooling exchanger duct

Aircraft combination engines thermal management system

Modulated clearance control for an axial flow rotary machine

Cooling system for the electrical generator of a turbofan gas turbine engine

Temperature control of engine case for clearance control

Electric windmill pump for gearbox durability

Geared turbofan gas turbine engine architecture

Gas turbine engine with high speed low pressure turbine section

Gas turbine engine with geared architecture

Turbine section of high bypass turbofan

Geared turbofan gas turbine engine architecture

Gas turbine engine bowed rotor avoidance system

Geared turbofan engine with targeted modular efficiency

Turbofan engine front section

Epicyclic gear train

Geared architecture for high speed and small volume fan drive turbine

Geared turbofan gas turbine engine architecture

Gas turbine engine blade tip clearance apparatus and method

Turbine engine with integrated generator having shared lubrication system

Aircraft thermal management system with reduced exhaust re-ingestion

Cooling exchanger ducts

Rotor thrust balancing

Clearance control for gas turbine engine

Seal clearance control system for a gas turbine

Seal clearance control system for a gas turbine

Gas turbine engine blade tip clearance apparatus and method

Controlled temperature rotating seal

Turbine cooling air supply system

Seal means for a gas turbine engine

External gas turbine engine cooling for clearance control

Zero running clearance centrifugal compressor

Gas turbine engine blade tip clearance apparatus and method

Modulated gas turbine cooling air

Method of restoring exhaust gas temperature margin in a gas turbine engine

SCHWARZ FREDERICK M

Thermal management system for turbofan engines

Cabin air supercharged aircraft internal combustion engine

SUCIU GABRIEL L

Geared turbofan with three turbines all counter-rotating

Gas turbine engine compressor arrangement

MCCUNE MICHAEL E

Gas turbine engine with geared architecture

Gas turbine engine gear train

KUPRATIS DANIEL BERNARD

Gas turbine engine with fan-tied inducer section

Gas turbine engine with fan-tied inducer section and multiple low pressure turbine sections

ADAMS PAUL R

Turbine section of high bypass turbofan

SMITH PETER G

Gas turbine engine with low fan pressure ratio