초록 ▼

The control device comprises at least one control ring to which one end ofn elbow lever is articulated. The vane pivot of alternating vanes is fixed at the intersection of the arms of the elbow levers. The other end of each elbow lever is connected by a rod to the end of a straight lever, the other

The control device comprises at least one control ring to which one end ofn elbow lever is articulated. The vane pivot of alternating vanes is fixed at the intersection of the arms of the elbow levers. The other end of each elbow lever is connected by a rod to the end of a straight lever, the other end of which is fixed to the pivot of an adjacent vane. The circumferential movement of the ring causes the pivots of the adjacent vanes to pivot in opposite directions. Two other embodiments have two rings.

대표청구항 ▼

1. In a multiflow turbojet engine having a primary gas flow channel and a secondary gas flow channel coaxially surrounding said primary flow channel, a device for regulating a pressure drop of a gas flow in at least one of the channels, said device comprising: a plurality of pivotable vanes in at

1. In a multiflow turbojet engine having a primary gas flow channel and a secondary gas flow channel coaxially surrounding said primary flow channel, a device for regulating a pressure drop of a gas flow in at least one of the channels, said device comprising: a plurality of pivotable vanes in at least one of said channels; two control rings; connection means connected between said control rings and said vanes, said connection means comprising means responsive to rotation of said at least control ring and respectively connecting first and second control rings to first and second ones of said vanes, for pivoting said first ones of said vanes in a first rotational sense and said second ones of said vanes in a second rotational sense opposite said first rotational sense, said first and second vanes being mutually alternating in position; and means for moving said at least one control ring, wherein each said vane includes a first pivot extending through a radially outer wall of said second flow channel, wherein said control rings are in, and concentric with, said secondary channel, one of said control rings being at either axial end of said vanes, and wherein said connection means further comprise a second pivot on one axial end of each said first vane and journalled in said first control ring, and a third pivot on an opposite axial end of each said second vane and journalled in said second control ring, and wherein said means for moving are connected to said first pivot of only two adjacent vanes. 2. The device of claim 1 wherein said means for moving comprise: a clip fixed to each said first pivot at a position radially outside of said radially outer wall; a connector part having ends pivoted to clips of adjoining pairs of said first and second vanes; and means for moving said connector piece in the direction of the axis of said engine. 3. The device of claim 1 wherein a radial height of said vanes is less than a radial height of said secondary channel.