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Dive into the research topics where Keith Towers Brown is active.

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Featured researches published by Keith Towers Brown.


SAE transactions | 2004

High Efficiency Ice Protection System (HEIPS) for Aircraft Engine Inlets

Keith Towers Brown; Michael John Layland; David B. Sweet

Goodrich Aerostructures Group and Goodrich De-icing and Specialty Systems Division (DSSD) are jointly developing an electrical High Efficiency Ice Protection system (HEIPS) for aircraft engine inlets. Engine Inlets designed with HEIPS technology, will improve efficiency of the engine and provide a lower weight inlet structure, when compared to a conventional hot air Thermal Anti-ice (TAI) system. In addition eliminating the pressures and temperatures associated with the traditional pneumatic anti-ice system is a breakthrough that allows for new nacelle concepts to be considered, including the use of conventional acoustic treatment in the lip area. The latter is important because aircraft noise is a major driver in current and future aircraft design, since international noise regulations are becoming more and more stringent.


44th AIAA Aerospace Sciences Meeting and Exhibit | 2006

Develpment and Test Results on a High Efficientily Ice Protection System

Brian Bobby Burkett; Milian Metrovic; Dave Sweet; Galdemir C. Botura; Dean Burner; Michael John Layland; Keith Towers Brown

Goodrich Aerostructures Group, Goodrich Materials and Simulation Center, and Goodrich Deicing and Specialty Systems Division are jointly developing a Highly Efficient Ice Protection System (HEIPS) for aircraft engine inlets. Engine Inlets designed with HEIPS technology, will improve efficiency of the engine and provide a lower weight inlet structure, when compared to a conventional Hot Air Thermal Anti-ice system. Eliminating the pressures and temperatures associated with the traditional pneumatic anti-ice system, allows for new nacelle concepts to be considered, including the use of conventional acoustic treatment in the lip area. The latter is important because aircraft noise is a major driver in current and future aircraft design, since international noise regulations are becoming more and more stringent.


Archive | 2007

Acoustic nacelle inlet lip having composite construction and an integral electric ice protection heater disposed therein

Michael John Layland; Keith Towers Brown; Claude Marc Hubert; Daniel P. Christy


Archive | 2008

Aircraft engine nacelle inlet having access opening for electrical ice protection system

Michael John Layland; Keith Towers Brown


Archive | 2008

Aircraft engine nacelle with translating inlet cowl

Michael Patrick McDonough; Keith Towers Brown; Scott Gilzean


Archive | 2006

Aircraft engine nacelle inlet having electrical ice protection system

Michael John Layland; Keith Towers Brown


Archive | 2016

MODULAR PLENUM AND DUCT SYSTEM FOR CONTROLLING BOUNDARY LAYER AIRFLOW

Keith Towers Brown


Archive | 2016

MULTI-ZONE ACTIVE LAMINAR FLOW CONTROL SYSTEM FOR AN AIRCRAFT PROPULSION SYSTEM

Keith Towers Brown; Stuart J. Byrne; Steven M. Kestler


Archive | 2015

ACCESS PANEL(S) FOR AN INNER NACELLE OF A TURBINE ENGINE

Keith Towers Brown


Archive | 2006

Aircraft engine nacelle inlet

Michael John Layland; Keith Towers Brown

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