Invention Grant
- Patent Title: Combustor of gas turbine with concentric swirler vanes
- Patent Title (中): 燃气轮机与同心旋流叶片的燃烧器
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Application No.: US11334744Application Date: 2006-01-19
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Publication No.: US07669421B2Publication Date: 2010-03-02
- Inventor: Keijiro Saitoh , Masataka Ohta , Satoshi Tanimura , Shigemi Mandai
- Applicant: Keijiro Saitoh , Masataka Ohta , Satoshi Tanimura , Shigemi Mandai
- Applicant Address: JP Tokyo
- Assignee: Mitsubishi Heavy Industries, Ltd.
- Current Assignee: Mitsubishi Heavy Industries, Ltd.
- Current Assignee Address: JP Tokyo
- Agency: Westerman, Hattori, Daniels & Adrian, LLP
- Priority: JP2005-124690 20050422
- Main IPC: F02C3/00
- IPC: F02C3/00

Abstract:
A gas turbine combustor having an inner tube and a transition pipe connected together is provided. The combustor includes an internal swirler and an external swirler. The internal swirler is composed of a cylindrical inward swirler ring disposed concentrically with respect to a central axis of the inner tube, and a plurality of inward swirler vanes provided on an outer peripheral surface of the inward swirler ring. The external swirler is composed of a cylindrical outward swirler ring disposed on an outer peripheral side of the inward swirler vanes and concentrically with respect to the inward swirler ring, and a plurality of outward swirler vanes provided on an outer peripheral surface of the outward swirler ring. The internal swirler and the external swirler are disposed within the inner tube.
Public/Granted literature
- US20060236700A1 Combustor of gas turbine Public/Granted day:2006-10-26
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