Torque transfer across an air gap

Patent metadata

Field	Value
Publication number	US-11056962-B2
Application number	US-201815880622-A
Country	US
Kind code	B2
Filing date	Jan 26, 2018
Priority date	Jan 26, 2018
Publication date	Jul 6, 2021
Grant date	Jul 6, 2021

Abstract

In one embodiment, an aircraft includes a wing operable to fold along a wing fold gap. The wing comprises an inboard edge flap and an outboard edge flap, wherein the wing fold gap is between the inboard edge flap and the outboard edge flap. The aircraft further includes an input shaft operably coupled to the inboard edge flap, the input shaft mechanically coupled to a first magnetic torque coupler assembly at a first end of the input shaft. The wing further includes an output shaft operably coupled to the outboard edge flap, the output shaft mechanically coupled to a second magnetic torque coupler assembly at a first end of the output shaft. The first magnetic torque coupler assembly may magnetically couple to the second magnetic torque coupler assembly across the fold gap.

First claim

What is claimed is:

1. A torque coupler, comprising:
a first magnetic torque coupler assembly, comprising:
a first inside tapered edge comprising a first magnet; and
a second inside tapered edge comprising a second magnet; and

a second magnetic torque coupler assembly comprising:
a first outside tapered edge comprising a third magnet; and
a second outside tapered edge comprising a fourth magnet; and

a power drive controller coupled to the first magnetic torque coupler assembly;
wherein:
the first magnetic torque coupler assembly is configured to remain stationary;
the second magnetic torque coupler assembly is configured to rotate;
the second magnetic torque coupler assembly is configured to disengage from the first magnetic torque coupler assembly by moving from an engaged position to a disengaged position;
when in the engaged position, the first magnetic torque coupler assembly is configured to magnetically couple with the second magnetic torque coupler assembly across an aircraft wing fold gap;
when in the disengaged position, the first magnetic torque coupler assembly does not magnetically couple with the second magnetic torque coupler assembly across the aircraft wing fold gap;
the first and second magnets are electromagnets;
the second and third magnets are permanent magnets; and
the power drive controller is operable to energize the first and second magnets of the stationary first magnetic torque coupler assembly, thereby causing the second magnetic torque coupler assembly to rotate.

2. An apparatus for transferring torque across an aircraft wing fold gap, the apparatus comprising:
a first shaft mechanically coupled to a first magnetic torque coupler assembly at a first end of the first shaft, wherein the first shaft and the first magnetic torque coupler remain stationary;
a second shaft mechanically coupled to a second magnetic torque coupler assembly at a distal end of the second shaft, wherein the second shaft and the second magnetic torque coupler assembly are operable to rotate;
the first magnetic torque coupler assembly comprising a plurality of electromagnets along the inside tapered edges of the first magnetic torque coupler assembly;
the second magnetic torque coupler assembly comprising a plurality of permanent magnets along outside tapered edges of the second magnetic torque coupler assembly; and
a power drive controller coupled to a second end of the first shaft that is opposite the first end of the first shaft;
wherein the second magnetic torque coupler assembly is operable to disengage from the first magnetic torque coupler assembly by moving from an engaged position to a disengaged position;
wherein, when in the engaged position, the plurality of electromagnets are operable to magnetically couple with the plurality of permanent magnets across the aircraft wing fold gap;
wherein, when in the disengaged position, the plurality of electromagnets do not magnetically couple with the plurality of permanent magnets across the aircraft wing fold gap; and
wherein the power drive controller is operable to energize the plurality of electromagnets of the stationary first magnetic torque coupler assembly, thereby causing the second magnetic torque coupler assembly and the second shaft to rotate.

3. The apparatus for transferring torque across the aircraft wing fold gap of claim 2 , wherein one or more of the first, second, third, and fourth magnets are selected from the group consisting of neodymium iron boron magnets, samarium cobalt magnets, and alnico magnets.

Assignees

• Lockheed Corp

Inventors

• Kao Calvin

Classifications

• H02K49/10

  of the permanent-magnet type · CPC title

• H02K49/104

  Magnetic couplings consisting of only two coaxial rotary elements, i.e. the driving element and the driven element · CPC title

• B64C3/56

  Folding or collapsing to reduce overall dimensions of aircraft · CPC title

• H02K49/108 Primary

  with an axial air gap · CPC title

• B64C13/30

  using cable, chain, or rod mechanisms · CPC title