An exhaust nozzle for a gas turbine engine includes a modular chevron. The chevron includes dual skins fixedly joined together at a base flange, and at a rim extending along the trailing edge of the chevron between the base and apex thereof.
申请公布号
WO2009025895(A2)
申请公布日期
2009.02.26
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