COOLING A COMBUSTOR HEAT SHIELD PROXIMATE A QUENCH APERTURE
摘要
An assembly is provided for a turbine engine. A combustor wall of the turbine engine assembly includes a shell and a heat shield. The combustor wall defines a quench aperture through the shell and the heat shield. The heat shield defines an effusion outlet a distance from the quench aperture equal to between about twenty-five times and about seventy-five times a width of the effusion outlet.
申请公布号
EP3077726(A1)
申请公布日期
2016.10.12
申请号
EP20140867256
申请日期
2014.12.04
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
CUNHA, FRANK J.;KOSTKA, JR., STANISLAV;MCKINNEY, RANDAL G.