Invention Grant
- Patent Title: Distributed aircraft engine fuel system
- Patent Title (中): 分布式飞机发动机燃油系统
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Application No.: US13090412Application Date: 2011-04-20
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Publication No.: US08666632B2Publication Date: 2014-03-04
- Inventor: Thaddeus J. Zebrowski , Richard E. Versailles
- Applicant: Thaddeus J. Zebrowski , Richard E. Versailles
- Applicant Address: US CT Windsor Locks
- Assignee: Hamilton Sundstrand Corporation
- Current Assignee: Hamilton Sundstrand Corporation
- Current Assignee Address: US CT Windsor Locks
- Agency: Kinney & Lange, P.A.
- Main IPC: G06F19/00
- IPC: G06F19/00
Abstract:
A gas turbine engine includes a plurality of fuel injectors grouped operatively by stages in a multistage combustor. A fuel system for the gas turbine engine includes at least one fuel metering module per stage of the multistage combustor. Each fuel metering module includes a pump, a flow meter, a pressure sensor, a controller, and a motor, which work together to control fuel output.
Public/Granted literature
- US20120271527A1 DISTRIBUTED AIRCRAFT ENGINE FUEL SYSTEM Public/Granted day:2012-10-25
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