Wing flap operation
AssigneeMBB GmbH
InventorErnst Stache
Life of this patent
Estimating the term…
Abstract
Adjusting device for landing flaps covering a gap between a landing flap or flaps and a wing proper there being a driven torsion shaft for driving the flaps, whereby particularly a transmission gear is drivingly coupled to the torsion shaft and includes a reducing gear and a gear segment being bidirectionally driven by the gear; a slotted cam is connected to and driven by the segment gear; a pair of levers with scanning elements is operated by the cam on rotation thereof; tension-compression rods are respectively linked to the levers such that the rods are operated in opposite direction; and a pair of elbow levers respectively connect the rods to two wing flaps such that the rods are tension loaded then compression loaded by the aerodynamic forces acting on the wing flaps.
Claims3
Adjusting device for wing flaps, the flaps provided for covering a gap between a landing flap or flaps and a wing proper comprising:
- a driven torsion shaft;
- a transmission gear drivingly coupled to the torsion shaft and including a reducing gear and a gear segment bidirectionally driven by the reducing gear to cover at least a particular angle;
- cam means connected to and driven by the gear segment;
- a pair of levers with follower elements and disposed to be operated by the cam means on rotation thereof;
- a pair of tension-compression rods respectively linked to the levers of the pair such that the rods of the pair are operated in opposite direction;
- and
- a pair of elbow levers respectively connecting the rods to two wing flaps such that the rods are tension loaded then compression loaded by the aerodynamic forces acting on the wing flaps.
Device as in claim, constructed so that the wing flaps can be pivoted in opposite directions, out of a neutral position, by directional operation of the torsion shaft and the transmission means.
Dependencies are inferred from the claim text.