초록 ▼

An adjustable section nozzle having a ring of deformable panels arranged close to its trailing edge is disclosed. Each panel has a dual-strip type structure made up of two materials presenting different coefficients of expansion, together with controlled heater devices that are thermally coupled to

An adjustable section nozzle having a ring of deformable panels arranged close to its trailing edge is disclosed. Each panel has a dual-strip type structure made up of two materials presenting different coefficients of expansion, together with controlled heater devices that are thermally coupled to the set of panels.

대표청구항 ▼

1. An adjustable-section fan nozzle comprising: a ring of deformable panels arranged close to a trailing edge of the adjustable-section fan nozzle,wherein each deformable panel comprises a dual-strip structure comprising an inner strip of thermally-insulating material together with at least one oute

1. An adjustable-section fan nozzle comprising: a ring of deformable panels arranged close to a trailing edge of the adjustable-section fan nozzle,wherein each deformable panel comprises a dual-strip structure comprising an inner strip of thermally-insulating material together with at least one outer strip of metal, said inner and outer strips presenting different coefficients of expansion and being assembled in full flat contact one against another so that a variation in temperature induces deformation of said dual-strip structure caused by the difference between said coefficients of expansion,wherein controlled heater means comprise electrical resistances distributed over the surfaces of the at least one outer strip of metal and in thermal contact therewith, andwherein the assembled inner and outer strips cause each deformable panel to curve in a direction tending to reduce a flow section at an outlet from the nozzle when said controlled heater means are actuated. 2. A nozzle according to claim 1, wherein said thermally-insulating material is a composite material. 3. A nozzle according to claim 1, wherein each deformable panel is substantially trapezoidal in shape. 4. A nozzle according to claim 1, wherein said deformable panels are mounted in an annular space defined in a wall of said adjustable-section fan nozzle. 5. A nozzle according to claim 4, wherein said deformable panels are continuous with an inside face of said wall when said controlled heater means are not in service. 6. A bypass turbojet, including a fan nozzle according to claim 1. 7. A nozzle according to claim 1, wherein an additional insulating layer covers an outer surface of each panel. 8. A nozzle according to claim 1, wherein an outer wall of said adjustable-section fan nozzle includes an inner annular casing and an outer annular casing defining an annular cavity therebetween, and said panels are housed in said annular cavity. 9. A nozzle according to claim 8, wherein said inner strip presents a stub with a first surface which abuts said inner annular casing and a second surface which abuts said outer annular casing. 10. A nozzle according to claim 2, wherein the composite material is based on carbon.