Guiding mechanism for variable geometry vectoring nozzles

Details Guiding mechanism for variable geometry vectoring nozzles Guiding mechanism for variable geometry vectoring nozzles

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 1/00 (2006.01) F02K 1/12 (2006.01)

Patent

CA 2281385

Guiding mechanism for variable geometry vectoring nozzles, applicable to gas turbines, capable of transmitting tangential forces acting on the external ring under vectoring loads onto the inner ring, avoiding the need of a joint between the outer ring and the nozzle structure. With this purpose a guiding track (9) oriented circumferentially around the pivoting axis (8) is incorporated onto the outer ring (3) and a track (10) oriented around a second axis (6) perpendicular to the previous is incorporated on the intermediate ring (2). The sledge element (11) joint to the intermediate ring (2), slides along the track (9) as a result of vectoring around the axis (8). For vectoring around axis (6) the sledge element (12), joint to the inner ring (1) slides over the track (10).

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