| 摘要 |
A fuel nozzle 100 for a gas turbine engine is disclosed, the fuel nozzle comprising at least one unitary component made using a rapid manufacturing process. In one aspect, the rapid manufacturing process is a laser sintering process. Unitary components disclosed include a conduit, swirler, distributor, venturi and a centerbody. |
| 申请人 |
GENERAL ELECTRIC COMPANY;MANCINI, ALFRED;MCMASTERS, MARIE, ANN;LOHMUELLER, STEVEN, JOSEPH;KASTRUP, DAVID, ALLEN;BENJAMIN, MICHAEL, A. |
发明人 |
MANCINI, ALFRED;MCMASTERS, MARIE, ANN;LOHMUELLER, STEVEN, JOSEPH;KASTRUP, DAVID, ALLEN;BENJAMIN, MICHAEL, A. |
