A gas turbine engine comprising a combustion chamber section, a turbine section, and a compressor section. The turbine section surrounds the combustion chamber and the compressor section surrounds the turbine section.

 
Web www.patentalert.com

< Methods of preparing polysilynes

< Microwave induced process for the preparation of substituted 4-vinylphenols

> Method for making extreme ultraviolet lithography structures

> Light weight porous structure
~ 00234