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Electrotor-SloMo ~ Rotor - Hub - General |
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Overview: |
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For one axial flux electric motor (disk motor) located in the rotor. |
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Drawing:
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Working Papers:
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Item:
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Coaxial: |
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Intermeshing: |
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Interleaving and Side-by-side: |
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Hub: |
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Ref. |
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OTHER ~ Flight Dynamics - Rotor Hub - Cyclic Control for a Simple Ultralight Helicopter |
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Coning: |
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Disk Tilt Partial Restraint: |
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Hub spring There are a number of pages |
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Ref. |
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OTHER: Miscellaneous - Thoughtless Idea - De-cone the Pre-cone |
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Reduce some cross-couplings |
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OTHER: Flight Dynamics - General - Pitch-Flap Coupling; (delta3) ~ Direct Control Hub |
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Does not provide additional control power but it should (theoretically) significantly reduce the possibility of excessive teetering angle. |
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A wide idea. An alternative to hub-spring and offset hinge. |
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Ref. |
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A possible alternative |
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To remove vibration. Conventional control to be removed for this. |
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A possible alternative |
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Ref. |
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A possible alternative |
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To Give Auto-collective: |
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To give auto-collective. |
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A possible alternative Torque-Pitch idea to the above. |
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Ref. |
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A possible alternative Torque-Pitch idea to the above two. |
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Ref. |
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SynchroLite components to be selected from for this rotorhub. |
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Introduction Page | SynchroLite Home Page | Electrotor Home Page | UniCopter Home Page | Nemesis Home Page | AeroVantage Home Page
Initially displayed: August 6, 2006 ~ Last Revised: March 5, 2009
The above utility invention is openly and publicly disclosed on the Internet to negate an entity from patenting it, to the exclusion of all others whom may wish to use it. ~ Reference patent law 35 U.S.C. 102 A person shall be entitled to a patent unless - (a) the invention was known ... by others in this country, ..., before the invention thereof by the applicant for patent.