Apparatus for driving and adjusting flaps hinged to an aircraft
View Patent ↗Flaps, for example leading edge flaps and/or trailing edge flaps of an aircraft wing, are driven and adjusted by respective drive units. Drive shafts of neighboring flaps are coupled to each other by a differential gear. The differential gear is thus coupled to a main drive shaft which is driven by a main drive unit. Additionally, the differential gear is coupled to a secondary drive unit. The main drive power and the secondary drive power and thus the respective flap motions are super-imposable on each other, which permits operating the flaps independently of each other or in synchronism with each other.
1. An apparatus for driving and positioning flaps operatively secured to a left wing and to a right wing of an aircraft, said apparatus comprising a pair of left wing flaps ( 1 , 2 ) and a pair of right wing flaps ( 1 ′, 2 ′), each pair of flaps including an inner flap closer to a body of said aircraft and an outer flap further away from said body, at least one actuator ( 3 ) operatively connected to each inner and outer wing flap of each pair, a primary drive ( 9 ) provided in common for the flaps of both wings, inner drive shafts ( 4 ) connecting said primary drive ( 9 ) to said at least one actuator ( 3 ) of said inner flap of each pair of flaps, a first differential gear ( 6 ) operatively interposed between said at least one actuator ( 3 ) of said inner flap ( 1 ) and said at least one actuator ( 3 ) of said outer flap ( 2 ) of said pair of left wing flaps, a second differential gear ( 6 ) operatively interposed between said at least one actuator of said inner flap ( 1 ′) and said at least one actuator of said outer flap ( 2 ′) of said pair of right wing flaps, outer drive shafts ( 5 ) connecting said first and second differential gears ( 6 ) to said at least one actuator of said inner flap and to said at least one actuator of said outer flap of each pair of flaps ( 1 , 2 ; 1 ′, 2 ′), wherein said inner drive shafts ( 4 ) couple said primary drive ( 9 ) and said first and second differential gears ( 6 ) to each other, wherein each of said outer flaps ( 2 , 2 ′) of each pair of flaps is drivable through its respective differential gear ( 6 ) of said first and second differential gears, at least one secondary drive ( 8 ′), and secondary drive trains operatively connecting said at least one secondary drive ( 8 ′) to each of said first and second differential gears ( 6 ) for superimposing a rotation of said at least one secondary drive ( 8 ′) through said first and second differential gears ( 6 ) on a rotation of said primary drive ( 9 ).
2. The apparatus of claim 1 , comprising two secondary drives ( 8 ), one secondary drive for each pair of said wing flaps ( 1 , 2 ; 1 ′, 2 ′), said secondary drive trains coupling a respective secondary drive of said two secondary drives to a respective differential gear ( 6 ) of said differential gears.
3. The apparatus of claim 1 , further comprising a computer for producing a control signal, flap position sensors providing flap position information to said computer for generating said control signal in response to said flap position information, and a control signal connection (C) between said computer and said at least one secondary drive for symmetrically operating said flaps in response to said control signal.
4. The apparatus of claim 3 , wherein said flap position sensors are adapted for sensing a position representing value for each individual flap of each wing.
5. The apparatus of claim 3 , wherein said computer comprises a program with a tuned algorithm for synchronizing the driving of said flaps.