Rohr, Inc.

Jeffrey Harasha

Vijay V Pujar

Jay Francisco

Steven M Kestler

Sarah Lohman

Phillip Andelson

Vanukuri Venkatareddy

Senthilkumar Radhakrishnan

An apparatus for aircraft anti-icing includes a nozzle body, a nozzle extending from the nozzle body, an eductor shroud at least partially surrounding the nozzle, the eductor shroud configured to focus a first flow of ambient air towards a first flow of hot gas exiting the first nozzle.

Method and apparatus for aircraft anti-icing

A control system for aircraft anti-icing is disclosed including a conduit coupled at a first end to a source of hot high-pressure bleed air, a control valve in fluid communication with the conduit and an injector head, wherein the control valve is in electronic communication with a controller and configured to regulate the flow of bleed air between the conduit and the injector head, and a first sensor in electronic communication with the controller and configured to report a first data. The system may initialize a control valve to an initial regulated pressure. The system may determine a control temperature and control the control valve based on the control temperature, the first data, and a set value.

Control system for aircraft anti-icing

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Del Mar, CA, United States of America

Jeffrey Harasha