发明名称 |
Gas turbine engine nozzle apparatus including a nozzle flap slot seal |
摘要 |
Apparatus for modulating the area of a gas turbine engine nozzle which provides for positive sealing between overlapping articulated flaps when the overlapped flap is axially slotted to receive a portion of the overlapping flap. An arcuate seal is attached to the overlapping flap by means of a floating connection, the overlapping flap dragging the seal therewith in the axial direction. A seat is mounted on either side of the slot to slidingly receive a pair of shoulders laterally extending from the seal. A portion of the seal is received within the slot and is so contoured as to partially define the nozzle flow path. A sleeve captures and supports the seal shoulders during their axial travel.
|
申请公布号 |
US4073441(A) |
申请公布日期 |
1978.02.14 |
申请号 |
US19760729594 |
申请日期 |
1976.10.04 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
NASH, DUDLEY O.;CLAYTON, THOMAS S. |
分类号 |
F02K1/10;F02K1/12;(IPC1-7):B64C15/06 |
主分类号 |
F02K1/10 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|