Invention Grant
- Patent Title: Combustor for gas turbine engine
-
Application No.: US15363414Application Date: 2016-11-29
-
Publication No.: US10775047B2Publication Date: 2020-09-15
- Inventor: Atsushi Horikawa , Masahide Kazari , Kunio Okada , Junichi Kitajima , Harald Funke , Karsten Kusterer , Anis Haj Ayed
- Applicant: KAWASAKI JUKOGYO KABUSHIKI KAISHA , B&B AGEMA GmbH
- Applicant Address: JP Hyogo, Kobe-shi DE Aachen
- Assignee: KAWASAKI JUKOGYO KABUSHIKI KAISHA,B&B AGEMA GmbH
- Current Assignee: KAWASAKI JUKOGYO KABUSHIKI KAISHA,B&B AGEMA GmbH
- Current Assignee Address: JP Hyogo, Kobe-shi DE Aachen
- Agency: Sughrue Mion, PLLC
- Priority: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@1edfbcb5
- Main IPC: F23R3/00
- IPC: F23R3/00 ; F23R3/28 ; F23R3/34 ; F23R3/18 ; F23D14/70 ; F02C7/22 ; F23R3/10 ; F23R3/16

Abstract:
A combustor includes: a combustion liner having a combustion chamber formed therein; and a fuel injector mounted to a top portion of the combustion liner, and including a fuel injection member having a plurality of fuel injection annular portions and an air guide member including a plurality of combustion air annular portions that guide air for combustion. The fuel injection annular portions and the combustion air annular portions are arranged concentrically and alternately. The fuel injector injects fuel and air into the combustion chamber. Each of the fuel injection annular portions includes a plurality of fuel injection holes that are open in a radial direction thereof, and each of the combustion air annular portions includes a plurality of air guide grooves that are open in an axial direction thereof, and guide the air to the fuel jetted from the fuel injection holes.
Public/Granted literature
- US20170082291A1 COMBUSTOR FOR GAS TURBINE ENGINE Public/Granted day:2017-03-23
Information query