An exhaust nozzle for a gas turbine engine includes a modular chevron (54). The chevron includes dual skins (56, 58) fixedly joined together at a base flange, and at a rim (72) extending along the trailing edge (66) of the chevron between the base (64) and apex (62) thereof.
申请公布号
WO2009025895(A3)
申请公布日期
2009.04.30
申请号
WO2008US64184
申请日期
2008.05.20
申请人
GENERAL ELECTRIC COMPANY;TISDALE, RUDOLPH, MORRIS;UHLER, GREGORY, ALLEN;JOHNSON, MICHAEL, ROBERT;NYE, CHRISTOPHER, JOSEPH
发明人
TISDALE, RUDOLPH, MORRIS;UHLER, GREGORY, ALLEN;JOHNSON, MICHAEL, ROBERT;NYE, CHRISTOPHER, JOSEPH
