Horizontal stabilizer drive

Claim 2

In an airplane, an apparatus for the transmission of mechanical power to a first and second driven means which, in turn, drive a single control surface which comprises: an epicylic gear train of the differential motion type, said gear train comprising two driven gears and a pinion gear with said pinion gear mounted for rotation on an axle which is attached to an arm which is turning about the axis of at least one of said driven gears; means for retaining said pinion gear to said pinion axle so that said pinion gear will rotate on said pinion axle only after a predetermined torque is applied to said pinion gear; means for disengaging said pinion gear from said driven gears after release of said means for retaining said pinion gear to said pinion axle; and means for attaching said first and second driven means to one each of said driven gears; whereby an input torque applied to said epicyclic gear train causes said arm with said pinion gear to rotate, driving both driven gears without relative movement between the three gears until a predetermined differential torque is experienced between said two driven gears which allows the pinion gear to rotate on its axle and disengage said driven gears.

Claim 3

A power transmission apparatus as recited in claim 1, in which said means for retaining said pinion gear to said pinion axle is a shear pin which shears at a predetermined torque.

Claim 4

A power transmission apparatus as recited in claim 1 in which said means for retaining said pinion gear to said pinion axle is a detent which releases at a predetermined torque.

Claim 5

A power transmission apparatus as recited in claim 1, in which said means for retaining said pinion gear to said pinion axle is a clutch which slips at a predetermined torque.

Claim 6

A power transmission apparatus as recited in claim 2, wherein said epicyclic gear train of the differential motion type is of the bevel gear type and said means for disengaging said pinion gear from said driven gears after failure of said shear pin further comprises mounting said bevel pinion gear to said pinion axle to permit the thrust force acting between said bevel gears to slide said bevel pinion gear on said pinion axle out of engagement with said driven bevel gears.

Claim 7

A power transmission apparatus as recited in claim 2, wherein said disengaging means comprises a pinion gear provided with teeth in two predetermined segments only, diametrically opposite each other to engage said two driven gears.

Claim 8

A power transmission apparatus as recited in claim 6, wherein said disengaging means is further enhanced by providing said two driven gears with teeth in predetermined segments only to match and engage said pinion gear teeth.

Claim 9

A power transmission apparatus as recited in claim 7 wherein said means for attaching said first and second driven means to one each of said two driven gears further comprises: first and second sprockets attached to one each of said two driven gears, and first and second chains connecting said first and second sprockets with said first and second driven means respectively.

Claim 10

A power transmission apparatus as recited in claim 7, further comprising a means for detecting and indicating a failure of said shear pin.

Claim 11

A power transmission apparatus as recited in claim 7, further comprising a means for locking said pinion gear out of engagement with said bevel gears after failure of said shear pin and rotation of said pinion gear.

Claim 12

In an airplane, an apparatus for the transmission of mechanical power to a first and second driven means which, in turn, drive a single control surface which comprises: a drive shaft, supported in bearings for rotation, and having at least one pinion axle oriented 90° to the axis of rotation of said drive shaft; a pinion gear mounted on each of said pinion axles, said pinion gear provided with teeth in two predetermined segments only, diametrically opposite each other; a first bevel gear mounted on said drive shaft free to rotate and engaging said pinion gears, said first bevel gear provided with teeth in segments only to correspond with said pinion gear teeth segments; a second bevel gear mounted on said drive shaft, free to rotate, opposite said first bevel gear with said pinion gears therebetween and engaging said second bevel gear, said second bevel gear provided with teeth in segments only to correspond with said pinion gear teeth segments; a shear pin retaining said pinion gears to said pinion axles so that said pinion gears will rotate on said pinion axles only after a predetermined torque is applied to said pinion gears; and means for attaching said first and second driven means to said first and second bevel gears respectively; whereby a torque applied to the drive shaft causes the attached pinion axles and pinion gears to rotate, driving both bevel gears without relative movement between the gears until a predetermined differential torque is experienced between the two bevel gears which shears the shear pins retaining the pinion gears which rotate on their axles disengaging the bevel gears.

Claim 13

In an airplane, an apparatus for the transmission of mechanical power to a first and second driven means which, in turn, drive a single control surface which comprises: a drive shaft, supported in bearings for rotation, and having at least one pinion axle oriented 90° to the axis of rotation of said drive shaft; a pinion gear mounted on each of said pinion axles, said pinion gear provided with teeth in two predetermined segments only, diametrically opposite each other; a first bevel gear mounted on said drive shaft free to rotate and engaging said pinion gears, said first bevel gear provided with teeth in segments only to correspond with said pinion gear teeth segments; a second bevel gear mounted on said drive shaft, free to rotate, opposite said first bevel gear with said pinion gears therebetween and engaging said second bevel gear, said second bevel gear provided with teeth in segments only to correspond with said pinion gear teeth segments; a shear pin retaining said pinion gears to said pinion axles so that said pinion gears will rotate on said pinion axles only after a predetermined torque is applied to said pinion gears; and means for attaching said first and second driven means to said first and second bevel gears respectively; whereby a torque applied to the drive shaft causes the attached pinion axles and pinion gears to rotate, driving both bevel gears without relative movement between the gears until a predetermined differential torque is experienced between the two bevel gears which shears the shear pins retaining the pinion gears which rotate on their axles disengaging the bevel gears.

Claim 14

A power transmission apparatus as recited in claim 11 further comprising a means for locking said pinion gear out of engagement with said bevel gears after failure of said shear pin and rotation of said pinion gear.

Claim 15

A power transmission apparatus as recited in claim 12 wherein said means for locking said pinion gear out of engagement with said bevel gears after failure of said shear pin and rotation of said pinion gear comprises: a detent contained in the distal end of said pinion axle; and an end cap fixed and rotating with said pinion gear, said end cap provided with three receptacles to receive said detent, a central receptacle position for normal drive with an alternate receptacle position either side of central to engage said detent following rotation of said end cap fixed to said pinion gear whereby locking said pinion gear out of engagement with said bevel gears.

Claim 16

A power transmissin apparatus as recited in claim 13 wherein said means for attaching said first and second driven means to one each of said first and second bevel gears further comprises: first and second sprockets attached to said first and second bevel gears, and first and second chains connecting said first and second sprockets with said first and second driven means, respectively.