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US 2015/0308292 A1Published application
Cowl with rate limited lock
AssigneeUnited Technologies Corporation
InventorMatthew J. Forcier
Life of this patent
Estimating the term…
Abstract
A core cowl for use with an engine core of a gas turbine engine includes a first cowl section for covering a first side of an engine core and a second cowl section for covering a second side of the engine core. A locking retractor connects the first cowl section to a support structure.
Claims20
A gas turbine engine comprising:
- an engine core;
- a core cowl extending circumferentially around the engine core, the core cowl comprising:
- a first cowl section on a first side of the engine core;
- and
- a second cowl section on a second side of the engine core;
- and
- a locking retractor connecting the first cowl section to a support structure.
4 more elements
A core cowl for use with an engine core of a gas turbine engine, the core cowl comprising:
- a first cowl section for covering a first side of an engine core;
- a second cowl section for covering a second side of the engine core;
- and
- a locking retractor connecting the first cowl section to the second cowl section.
1 more element
Dependencies are inferred from the claim text.