#F02C7/047

ICING CONDITION IDENTIFICATION FOR GAS TURBINE ENGINE

A gas turbine engine (20) includes a propulsor for providing air into a core engine housing and propulsion air radially outwardly of the core engine housing. The core engine housing surrounds a compre…

DRIVE·Mar 4·2 min read

F02C7/047 PRATT & WHITNEY CANADA [CA]

PRESSURE REGULATING SHUT-OFF VALVE

A pressure regulating shut-off valve (1) has a valve member (2) regulating flow of fluid between an inlet (4) and an outlet (6). A pneumatic actuator (8) has a piston having first and second faces (14…

DRIVE·Aug 28·1 min read

F02C7/047 MICROTECNICA SRL [IT]

System and method for gas turbine inlet air heating

A gas turbine system for part load efficiency improvement and anti-icing within the inlet (16) and at the compressor inlet is described. The system includes a gas turbine (12) having a compressor (13)…

DRIVE·Aug 14·1 min read

F02C7/047 GEN ELECTRIC [US]

Combustion turbine inlet anti-icing resistive heating system

A resistive heating system for a combustion turbine susceptible to inlet air filter house component (42) and compressor icing includes a plurality of heating panels (bundles) (48) arranged in a substa…

DRIVE·Jul 31·1 min read

F02C7/047 GEN ELECTRIC [US]

De-icing device for gas turbine engine

The attachment element has a nacelle (30) and an annular tube element (31) that are connected with each other by a fastening unit, such that relative movement between nacelle and annular tuber element…

DRIVE·Jul 24·1 min read

F02C7/047 ROLLS ROYCE DEUTSCHLAND [DE]

Turbomachine Nacelle And Anti-Icing System And Method Therefor

An anti-icing system for a nacelle (50) of an aircraft engine (10). The nacelle (50) has an inlet lip (56) that defines a leading edge of the nacelle (50), and further has an annular-shaped cavity (58…

DRIVE·Aug 10·1 min read

F02C7/047 MRA SYSTEMS INC [US]

Gas turbine engine and intake for a gas turbine engine with a device to prevent ice forming

A gas turbine engine (10) comprising a nacelle (21) having an intake (12), the intake (12) defining a generally annular chamber (35), an engine accessory (33, 34) and a heat exchanger (36) for cooling…

DRIVE·Nov 24·1 min read

F02C7/047 ROLLS ROYCE PLC [GB]