초록 ▼

An exhaust nozzle for a gas turbine engine comprising a duct 17(c) extending along an axis and having at a dowstream end thereof a mechanism for varying the geometry and area of the nozzle. The mechanism 28 comprises an axially translatable member 28 which has a face 29 extending in a direction tran

An exhaust nozzle for a gas turbine engine comprising a duct 17(c) extending along an axis and having at a dowstream end thereof a mechanism for varying the geometry and area of the nozzle. The mechanism 28 comprises an axially translatable member 28 which has a face 29 extending in a direction transverse to the axis of the duct 17(c) against which pressurized gases flowing through the duct acts to balance out the loads on the flaps. A plurality of flaps 38,43 are spaced circumferentially around the axis of the duct. The flaps 38 are pivotally attached to the axially translatable member 28 and are provided with a cam follower 40 that co-operates with a cam 37. The cams 37 are fixed relative to the duct 17(c) and thereby defines the attitude of each flap 38 relative to the member 28. Seal plates 41 and 45 cover the gaps between adjacent flaps 38 and 43 to the seal plates 45. A plurality of struts interconnect the member 28 and the second flaps of the pivotal attachment of the flaps 43 to the flap 38. A set of flaps 47 are provided to provide fairing between the downstream ends of the member 28 and the flaps 43. In operation axial movement of the member 28 moves the flaps 38 and 43 to different positions.

대표청구항 ▼

1. An exhaust nozzle for a gas turbine engine comprising a duct extending along an axis and having at a downstream end thereof a mechanism for varying the geometry and area of the nozzle, the mechanism comprising an axially translatable member which has a face extending in a direction transverse to

1. An exhaust nozzle for a gas turbine engine comprising a duct extending along an axis and having at a downstream end thereof a mechanism for varying the geometry and area of the nozzle, the mechanism comprising an axially translatable member which has a face extending in a direction transverse to the axis of the duct against which pressurised gases flowing through the duct acts to bias the member in a direction along the duct, a plurality of first flaps spaced circumferentially around the axis of the duct each of which is pivotally attached at its upstream end to the axially translatable member, each first flap being provided with a cam follower that co-operates with a cam that is fixed relative to the fixed duct thereby to define the attitude of each first flap relative to the member, a plurality of first seal plates each of which is pivotally attached at an upstream end to the member and positioned to cover the gap between adjacent first flaps, a set of circumferentially spaced second flaps each of which is pivotally attached at its upstream end to the downstream end of a first flap, a plurality of second seal plates each of which is pivotally attached at an upstream end to the downstream end of one of the first seal plates and positioned to cover the gap between two adjacent second flaps, a plurality of struts each of which is pivotally connected at one end to the member and pivotally connected at another end to a second flap at a region of the second flap downstream of the pivotal attachment of the second flap to the first flap, and a plurality of third flaps each of which is pivotally attached at one end to the member and pivotally attached at its other end to the downstream end of one of the second flaps. 2. A nozzle according to claim 1 wherein the axially translatable member is a right circular cylindrical annular structure which is moved axially by means of one or more lead screws which is rotatable in a nut which is carried by the member and the first flaps and first seal plates are pivotally mounted on an inner circumference of the annular member, and the third flaps are pivotally mounted on an outer circumference of the annular member. 3. A nozzle according to claim 2 wherein the annular member is mounted to slide axially on axially extending supports and the supports carry an annular framework that defines a plurality of axially extending cam surfaces spaced around the axis of the annular framework. 4. A nozzle according to claim 3 wherein the cam surfaces face inwards and each first flap is provided with the cam follower on its outer facing side. 5. A nozzle according to claim 2 wherein the axially translatable member slides in the bore of the duct and a sliding seal means is provided between the member and the duct. 6. A nozzle according to claim 1 wherein roller means which contact the outward facing sides of the first flaps are provided on each of the first seal plates. 7. A nozzle according to claim 1 wherein roller means which contact the outward facing sides of the second flaps are provided on each of the second seal plates.