Invention Grant
- Patent Title: Gas turbine fuel injector comprising a splitter having a cavity
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Application No.: US16903456Application Date: 2020-06-17
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Publication No.: US11300293B2Publication Date: 2022-04-12
- Inventor: Luca Tentorio , Juan Carlos Roman Casado , Giacomo Di Chiaro , Jonathan Knapton , Filippo Zambon , Radu Irimia
- Applicant: ROLLS-ROYCE plc
- Applicant Address: GB London
- Assignee: ROLLS-ROYCE plc
- Current Assignee: ROLLS-ROYCE plc
- Current Assignee Address: GB London
- Agency: Oliff PLC
- Priority: GB1909168 20190626
- Main IPC: F23R3/28
- IPC: F23R3/28 ; F23R3/14 ; F23R3/34

Abstract:
A fuel injector comprising a first air swirler passage and a second air swirler passage extending axially through the fuel injector and arranged to direct air through the fuel injector, a splitter arranged between the first air swirler passage and the second air swirler passage and comprising a first splitter surface having a first divergent portion which is divergent in the downstream direction, a second splitter surface located radially inward of the first splitter surface and having a second divergent portion which is divergent in the downstream direction, a third splitter surface located radially inward of the first and second splitter surface, and a first connecting surface extending between the second and third splitter surfaces, wherein a first cavity is formed between the first and second splitter surfaces, and the second divergent portion comprises at least one opening in fluid communication with the first cavity.
Information query