Patent ID: 8834315
Filing Date: 2014-09-16
Classification: A61C,F02C,F02K,F16H

Abstract:
1. A rotary mechanism, comprising: at least first, second, and third rotational components, wherein at least one of the rotational components comprises at least a first implement selected from the group consisting of: a first propeller, a first impeller, a first fan assembly, a first fan, a first blade, a first compressor, a first booster, a first combustor, a first rotor, a first turbine, a first nozzle, a first duct, a first generator, a first motor, a first gear component, and a first component thereof; at least first and second counter-rotational mechanisms, wherein the first counter-rotational mechanism operably engages at least the first and second rotational components, and wherein the second counter-rotational mechanism operably engages at least the second and third rotational components; and, at least one drive mechanism component or a portion thereof that operably engages one or more of the rotational components and/or one or more of the counter-rotational mechanisms, which drive mechanism component or portion thereof is configured at least to effect rotation of the rotational components and the counter-rotational mechanisms such that the first and third rotational components rotate in a first direction and the second rotational component rotates in a second direction.