Invention Grant
- Patent Title: Gas turbine engine inlet wall design
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Application No.: US14665081Application Date: 2015-03-23
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Publication No.: US10907544B2Publication Date: 2021-02-02
- Inventor: Dmytro Mykolayovych Voytovych , Om P. Sharma
- Applicant: United Technologies Corporation
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F02C7/04
- IPC: F02C7/04 ; B64D27/00 ; F01D5/02 ; B64D33/02 ; B64D27/14 ; B64C39/10
Abstract:
A gas turbine engine includes an inlet duct that is formed with a generally elliptical shape. The inlet duct includes a vertical centerline and a fan section that has an axis of rotation. The axis of rotation is spaced from the vertical centerline and is disposed within an inlet duct orifice.
Public/Granted literature
- US20150321764A1 GAS TURBINE ENGINE INLET WALL DESIGN Public/Granted day:2015-11-12
Information query
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