Invention Grant
US08899048B2 Low calorific value fuel combustion systems for gas turbine engines
有权
燃气涡轮发动机的低热值燃料燃烧系统
- Patent Title: Low calorific value fuel combustion systems for gas turbine engines
- Patent Title (中): 燃气涡轮发动机的低热值燃料燃烧系统
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Application No.: US12954008Application Date: 2010-11-24
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Publication No.: US08899048B2Publication Date: 2014-12-02
- Inventor: Lev Alexander Prociw , Andy W. Tibbs
- Applicant: Lev Alexander Prociw , Andy W. Tibbs
- Applicant Address: US IA West Des Moines
- Assignee: Delavan Inc.
- Current Assignee: Delavan Inc.
- Current Assignee Address: US IA West Des Moines
- Agency: Edwards Wildman Palmer LLP
- Agent Scott D. Wofsy; Joshua L. Jones
- Main IPC: F02C1/00
- IPC: F02C1/00 ; F23R3/34 ; F23R3/36 ; F23R3/44 ; F23R3/54

Abstract:
A combustion system for a gas turbine engine includes a housing defining a pressure vessel. A master injector is mounted to the housing for injecting fuel along a central axis defined through the pressure vessel. A plurality of slave injectors is included. Each slave injector is disposed radially outward of and substantially parallel to the master injector for injecting fuel and air in an injection plume radially outward of fuel injected through the master injector. The master injector and slave injectors are configured and adapted so the injection plume of the master injector intersects with the injection plumes of the slave injectors. The slave injectors can be staged for reduced power operation.
Public/Granted literature
- US20120125008A1 LOW CALORIFIC VALUE FUEL COMBUSTION SYSTEMS FOR GAS TURBINE ENGINES Public/Granted day:2012-05-24
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