US 4,786,013 AGranted

Flap drive with variable torque limiting

AssigneeMBB GmbH

InventorUlrich Pohl

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Abstract

Flaps mounted on an carriage are being protracted and retracted in relation to a aircraft wing of which the flap is a part by a drive mechanism which is to be provided for variable torque and torque limiting and, if necessary, fixing and holding the position of the flap and its drive carriage in case of failure. A branching gear is driven for the common shaft which drives the flaps of one wing and there are separate transmission paths which include in each instance output shafts from the branching gear, crank drives and thrust rods. One of the thrust rod is directly connected to the flap carrying carriage and the other one indirectly through a load switch and a connecting rod; in addition one of the output shafts of the branching gear is lead into a delta alpha brake having as a second input, the output of the principle drive shaft. The delta alpha brake stops motion of the flap carrying carriage in case there is an angle difference among its input shafts that exceeds a particular limit.

Claims5

Dependent claims

In a drive arrangement for a landing flap on an aircraft wing which includes structure for variable torque limiting and position fixing, the particular flap being mounted on at least one carriage, the improvement comprising:

a principal drive shaft for operating the particular and other landing flaps;
a differential and branching gear having a common input connected to said principle drive shaft and having two output shafts to establish two load transmitting paths;
two additional differential gears respectively connected to and driven by said two output shafts;
two crank drives respectively connected to and driven by said two additional differential gears;
two thrust rods respectively connected to said crank drives;
one of the thrust rods being directly connected to the flap carrying carriage;
the other thrust rod being connected through a connecting rod and a load switch to said carriage, there being a variable test point connection provided between the other thrust rod and said connecting rod;
and
a mechanical delta alpha brake being interposed between said principle shaft and one of the output shafts of the branching differential gear.

6 more elements

Dependencies are inferred from the claim text.