- Patent Title: Dual-fuel injector with a double pipe sleeve gaseus fuel flow path
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Application No.: US14461532Application Date: 2014-08-18
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Publication No.: US10094567B2Publication Date: 2018-10-09
- Inventor: Shota Igarashi , Hirokazu Takahashi
- Applicant: Mitsubishi Hitachi Power Systems, Ltd.
- Applicant Address: JP Yokohama-shi
- Assignee: Mitsubishi Hitachi Power Systems, Ltd.
- Current Assignee: Mitsubishi Hitachi Power Systems, Ltd.
- Current Assignee Address: JP Yokohama-shi
- Agency: Crowell & Moring LLP
- Priority: JP2013-195007 20130920
- Main IPC: F23R3/30
- IPC: F23R3/30 ; F23R3/32 ; F23R3/34 ; F23R3/36 ; F23R3/28

Abstract:
A dual-fuel burning gas turbine combustor having a diffusive combustion burner to burn a liquid fuel and a gaseous fuel placed at the axis of the gas turbine combustor and a plurality of pre-mixing combustion burners to burn a liquid fuel and a gaseous fuel placed on an outer circumferential side of the diffusive combustion burner, each pre-mixing combustion burner having a liquid fuel nozzle, a plurality of gaseous fuel spray holes, a plurality of air holes, and a pre-mixing chamber to mix gaseous fuel and air, wherein each pre-mixing combustion burner has a double pipe sleeve at a connected portion between end cover and the pre-mixing combustion burner, and the double pipe sleeve has an inner sleeve having a gaseous fuel flow path, an outer sleeve positioned on an outer circumferential side of the inner sleeve, and a circular spacing formed between the inner sleeve and the outer sleeve.
Public/Granted literature
- US20150082770A1 Dual-Fuel Burning Gas Turbine Combustor Public/Granted day:2015-03-26
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