Apollonian Cavity-Resonator Gaskets

I’m tripping a bit on the magnetron designs the cavity resonator system does something like the braided vortex water system i shared. That takes me a bit toward vimana engines, and the related circuitry that was shared with me about a purported UFO engine. While also it makes me think about a resonator with a fractal cavity. First glance the ideas seem unrelated. I’m hopefully they’ll have a union.

I think I see a union - the cavities can be formed by any dieletric difference, not just an airgap. With enough design, this can make it a transistor. Then the central electron flow is not through an airgap, but through ‘laminar hyperbolic hydrodynamic double-layer braiding’. Think of the electron channel ‘arcs’ that happen with topological changes due to the braiding changes. Said ‘arcs’ could be quantized emissions (‘photons’ of some kind), which makes the braid network analogous to transistors / circuits. The entirety of coupled systems then an analogue of a calculator, in the way that an automatic-transmission valve body calculates the gear. The coupling in this system could ‘calculate’ a power efficiency in higher dimensions.
Maybe wormholes are pressure activated.

§Cavity Magnetron

“If a third electrode is inserted between the cathode and the anode (called a control grid), the flow of electrons between the cathode and anode can be regulated by varying the voltage on this third electrode. This allows the resulting electron tube (called a “triode” because it now has three electrodes) to function as an amplifier because small variations in the electric charge applied to the control grid will result in identical variations in the much larger current of electrons flowing between the cathode and anod

In the case would the triode be the fractal cavity structure itself?


§US10229999B2 - Methods of forming upper source/drain regions on a vertical transistor device

Google Patents A plurality of vertically oriented channel semiconductor structures is formed above a substrate. A bottom source/drain (S/D) region is formed proximate a lower portion of the vertically oriented channel semiconductor structure. A first dielectric layer is formed above the vertically oriented channel semiconductor structure. A thickness of the first dielectric layer is reduced to expose an upper portion of the vertically oriented channel semiconductor structure. A first semiconductor material region is formed on the exposed upper portion. The thickness of the first dielectric layer is further reduced to expose a channel portion of the vertically oriented channel semiconductor structure and to define a bottom spacer adjacent the bottom S/D region. A gate structure is formed around the channel region of the vertically oriented channel semiconductor structure. A second semiconductor material region is formed on the upper portion to define an upper S/D region after forming the gate structure. That last one is above my head but towards apollonion air gap transitors

§US10305159B2 - Apollonian-loaded split-ring resonator and method for designing the same

Google Patents The invention provides an apparatus comprising a wide bandwidth resonating structure based on a primary split ring resonator having a plurality of additional split ring resonators bounded by the primary split ring resonator. The invention provides a method for optimizing the placement and size of the additional split ring resonators to achieve the desired bandwidth for the overall resonator structure.

§US8960595B2 - Wingless hovering of micro air vehicle

Google Patents

Embodiments of the subject invention relate to an air vehicle and a power source. Embodiments can operate at reasonable power levels for hovering and withstanding expected wind gusts. Embodiments can have a diameter less than 15 cm. Embodiments can have one or more smooth (continuous curvature) surface and can be operated using electromagnetic and electrohydrodynamic principles. The wingless design of specific embodiments can allow operation with no rotating or moving components. Additional embodiments can allow active response to the surrounding flow conditions. The issue of low lift to drag ratio and degradation of airfoil efficiency due to the inability of laminar boundary layers attachment can also be significantly reduced, or eliminated. The electromagnetic force can be generated by applying a pulsed (alternating/rf) voltage between a set of grounded and powered electrodes separated by a polymer insulator, dielectric, or other material with insulating properties.


box animation surface

potentially related -findingthedot.


“For any integer n > 0, there exists an Apollonian gasket defined by the following curvatures: (−n, n + 1, n(n + 1), n(n + 1) + 1). For example, the gaskets defined by (−2, 3, 6, 7), (−3, 4, 12, 13), (−8, 9, 72, 73), and (−9, 10, 90, 91) all follow this pattern. Because every interior circle that is defined by n + 1 can become the bounding circle (defined by −n) in another gasket, these gaskets can be nested. This is demonstrated in the figure at right, which contains these sequential gaskets with n running from 2 through 20.” “Nested Apollonian gaskets”

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