초록 ▼

A divergent flap seal for a gas turbine engine exhaust nozzle having a longitudinal axis is provided, having a body, a spine member, and a flap position guide. The flap position guide separates adjacent divergent flaps regardless of the angle the flaps are skewed relative to the longitudinal axis of

A divergent flap seal for a gas turbine engine exhaust nozzle having a longitudinal axis is provided, having a body, a spine member, and a flap position guide. The flap position guide separates adjacent divergent flaps regardless of the angle the flaps are skewed relative to the longitudinal axis of the nozzle, thereby more evenly distributing the flaps about the circumference of the nozzle.

대표청구항 ▼

A divergent flap seal for a gas turbine engine exhaust nozzle having a longitudinal axis, comprising: a body, having: a forward end and an aft end; a length, extending between said forward and aft ends; a width; a plurality of corrugations formed in said body extending across said width; and a first

A divergent flap seal for a gas turbine engine exhaust nozzle having a longitudinal axis, comprising: a body, having: a forward end and an aft end; a length, extending between said forward and aft ends; a width; a plurality of corrugations formed in said body extending across said width; and a first and a second channel, each channel having walls extending lengthwise along said body, wherein one of said channels is disposed on each side of said width; a spine member, attached to a first side of said body, extending along the length of said body; a flap position guide, attached to said spine member, adjacent said aft end of said body, said flap position guide extending out from said body a distance sufficient to separate adjacent flaps regardless of the vectored position of the nozzle; wherein said flap position guide separates adjacent flaps.