Magnetic de-rotation system for a shaft fairing system
First Claim
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1. A de-rotation system comprising:
- a fairing;
an inner ring which supports an eddy current ring and at least one inner ring magnet, said eddy current ring extends for a first axial length of said inner ring while said at least one inner ring magnet extends for a second axial length of said inner ring; and
an outer ring which supports at least one outer ring magnet, said at least one outer ring magnet extends for a third axial length of said outer ring such that said at least one outer ring magnet axially extends between said first axial length and said second axial length, attraction between said at least one inner ring magnet and said at least one outer ring magnet produces a stable rotational position, wherein said at least one inner ring magnet includes a multiple of inner ring magnets equally spaced about the circumference of said inner ring and said at least one outer ring magnet includes a multiple of outer ring magnets greater in number than said multiple of inner ring magnets.
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Abstract
A magnetic de-rotation system includes an inner ring which supports an eddy current ring and at least one inner ring magnet and an outer ring which supports at least one outer ring magnet, attraction between the at least one inner ring magnet and the at least one outer ring magnet produces a stable rotational position for a fairing.
35 Citations
18 Claims
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1. A de-rotation system comprising:
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a fairing; an inner ring which supports an eddy current ring and at least one inner ring magnet, said eddy current ring extends for a first axial length of said inner ring while said at least one inner ring magnet extends for a second axial length of said inner ring; and an outer ring which supports at least one outer ring magnet, said at least one outer ring magnet extends for a third axial length of said outer ring such that said at least one outer ring magnet axially extends between said first axial length and said second axial length, attraction between said at least one inner ring magnet and said at least one outer ring magnet produces a stable rotational position, wherein said at least one inner ring magnet includes a multiple of inner ring magnets equally spaced about the circumference of said inner ring and said at least one outer ring magnet includes a multiple of outer ring magnets greater in number than said multiple of inner ring magnets. - View Dependent Claims (2)
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3. A fairing system comprising:
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a shaft fairing mounted for rotation about an axis of rotation; a magnetic de-rotation system mounted to said shaft fairing to control a rotation of said shaft fairing about said axis of rotation; an upper magnetic ring assembly affixed to said shaft fairing; and a lower magnetic ring assembly affixed to said shaft fairing, wherein each of said upper magnetic ring assembly and said lower magnetic ring assembly comprises an inner ring which supports at least one inner ring magnet and an outer ring which supports at least one outer ring magnet, attraction between said at least one inner ring magnet and said at least one outer ring magnet produces at least one stable rotational position, wherein said inner ring is eccentric to said outer ring. - View Dependent Claims (4, 5, 6, 7, 8, 9, 10, 11)
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12. A counter rotating coaxial rotor system comprising:
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a lower rotor hub mounted to a lower rotor shaft and configured to rotate about an axis of rotation; an upper rotor hub mounted to an upper rotor shaft and configured to rotate about said axis of rotation, said upper rotor shaft mounted through said lower rotor shaft and rotating in a direction opposite a direction of rotation of the lower rotor shaft; an upper hub fairing mounted at least partially about said upper rotor hub; a lower hub fairing mounted at least partially about said lower rotor hub; a shaft fairing mounted between said upper hub fairing and said lower hub fairing for rotation about said rotor axis of rotation; an upper magnetic ring assembly affixed to said upper rotor shaft and said shaft fairing, said upper magnetic ring assembly comprising at least one inner ring permanent magnet; and a lower magnetic ring assembly affixed to said lower rotor shaft and said shaft fairing, said lower magnetic ring assembly comprising at least one outer ring permanent magnet; wherein said upper magnetic ring assembly and said lower magnetic ring assembly each comprises an inner ring which supports said at least one inner ring permanent magnet and an outer ring which supports at least one outer ring permanent magnet, attraction between said at least one inner ring magnet and said at least one outer ring magnet produces a stable rotational position; and wherein said inner ring is eccentric to said outer ring. - View Dependent Claims (13, 14, 15)
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16. An aircraft comprising:
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a lower rotor hub mounted to a lower rotor shaft and configured to rotate about an axis of rotation; an upper rotor hub mounted to an upper rotor shaft and configured to rotate about said axis of rotation, said upper rotor shaft mounted through said lower rotor shaft and rotating in a direction opposite a direction of rotation of the lower rotor shaft; an upper hub fairing mounted at least partially about said upper rotor hub; a lower hub fairing mounted at least partially about said lower rotor hub; a shaft fairing mounted between said upper hub fairing and said lower hub fairing for rotation about said rotor axis of rotation; an upper magnetic ring assembly affixed to said upper rotor shaft and said shaft fairing; and a lower magnetic ring assembly affixed to said lower rotor shaft and said shaft fairing wherein said upper magnetic ring assembly includes a first plurality of magnets spaced about a circumference of said upper magnetic ring assembly, and said lower magnetic ring assembly includes a second plurality of magnets spaced about a circumference of said lower magnetic ring assembly, a number of magnets in said first plurality of magnets different than a number of magnets in said second plurality of magnets. - View Dependent Claims (17, 18)
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Specification