The present embodiments disclose a system for reducing inlet air temperature of a device,
including: an air inlet, a fogging system that provides air cooling, wherein the fogging system …

An inlet strut with a hot-air anti-icing system is studied experimentally and numerically to
understand the heat transfer between impinged supercooled water droplets and solid …

In one embodiment, a system includes a turbine combustor having a combustor liner
disposed about a combustion chamber, a head end upstream of the combustion chamber …

The present invention discloses a novel apparatus and meth ods for controlling an air
injection system for augmenting the power of a gas turbine engine, improving gas turbine …

BACKGROUND 0003 Parallel to the requirements regarding the perfor mance and efficiency
of Such gas turbines, the requirements are more and more increasing as regards the cooling …

(57) ABSTRACT A method for providing an anti-icing airflow, including extracting a
compressed airflow from a core flow path of an engine, heating the compressed airflow …

(57) ABSTRACT A system includes a controller configured to control a heated flow
discharged from an outlet of an eductor to an inlet control system to control a temperature of …

Embodiments of the present disclosure are directed toWards a system having a compressor
bleed air recirculation system. The compressor bleed air recirculation system includes a …

The present application provides an inlet bleed heat control system for a compressor of a
gas turbine engine. The inlet bleed heat control system provides an inlet bleed heat …

A gas-circulation system for conditioning a disk of an aircraft may comprise a first takeoff port
configured to extract a combusted gas and a second takeoff port configured to extract an …