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Ducted Cowl Support For A Gas Turbine Engine
Abstract: A ducted cowl support (54) includes an annular structure configured to be mounted to an annular turbine engine frame (46) and including one or more bypass ducts (62) integrally formed therein.
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Notices, Deadlines & Correspondence
Notices, Deadlines & Correspondence
Patent Information
Application #
Filing Date
23 December 2015
Publication Number
35/2016
Publication Type
INA
Invention Field
MECHANICAL ENGINEERING
Status
Email
bpo.mail@ge.com
Parent Application
Applicants
GENERAL ELECTRIC COMPANY
1 River Road
Schenectady, New York 12345
USA
Inventors
1. HASTING, William Howard
One Neumann Way
Cincinnati, OH 45215
USA
2. WOLFE, Jared Matthew
One Neumann Way
Cincinnati, OH 45215
USA
3. DALE, David Edward
1 Neumann Way
MD G51
Cincinnati, OH 45215
USA
Specification
SOFT COPY ATTACHED IN PDF