Directory:Rotoverter:Replications:Deliverance:Old

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RV Resonance Recovery Circuit 1.1

(Deliverance)

The deliverance circuit was done on the PM only. The diode plug was used in the run caps position. With the plug on the PM the inverter ramp wave from could be used to synchronize the plug extraction. With the plug circuit on the alt motor the synchronization of cap loading will need to be done using the alt output waveform. I know others were working on that type of circuit. this (see further below)circuit works by sensing the resonant waveform.

Original post with commentary from Hector

Deliverance RV resonance v1.1 uploaded
--- In EVGRAY@yahoogroups.com, "davidkou wrote:

• David- The charge battery gets charged very quickly, around 0.1V/minute or more. NO INCREASED LOAD at all visible on the inverter, seems to be charging for free.
  • Hector -That is the ZERO point capture and the non reflective extraction circuit (were energy at 2x2 stages and is defined as joules second.
• David- Some points and observations;
• 1. The TIC126D Thyristors I had were all bad. I changed to 2N6509 and bingo.
  • Hector- Part selection sometimes is critical (internal resistance and switching time being main issues) along with amplification gain.
• David- 2. I put in some current limiting resistors in the Darlington drive to the thyristors. (Dampers)
• 3. I noticed that the voltage waveform across the Run Cap is 60 degree lagging the input waveform to the RV (not 90 degrees as I thought).
  • Hector- 120/2 = 60< 3 phases are 120 degrees one from the other relative to line in a phase converter is 120/2. Relative to prime mover alternator lags 30deg max. (Critical)
• David- 4. Battery carries on charging on its own for a while afterwards. Radiant energy charging like the Bedini motor.
  • Hector- Radiant energy = RESONANCE = RF (radio frequency ...)
    
• David- 5. My previous test of Kone's FWBR across Run Cap was probably crap because of the dodgy TIC126D thyristors. I will re-do this experiment soon.
• 6. A thyristor tester is useful bit of gear.
  • Hector- A solid state device analyzer is also useful, Congratulations. Remember in step down from HI voltage say 236 VAC in a RV alternator say 8 amps circulation.. 236/10 = (23.6 VAC at 80Amps !) The wire mass must be identical in primary and secondary impedance matching ballun transformer or FR trafo (transformer) 10 to one ratio must be a turn to circular mill ratio 10:1 within same weight ratio 1:1.
  • OU is OU - ZPE is ZPE and denial is no longer possible with the predicted eventual looping of these systems. The schematic at dons page ( http://www.theverylastpageoftheinternet.com ) being "understood" within standard technology being RV as sample 20 amps max at inverter input 200Vac 5 amps at alternator and split into a pulsed diode 3x3 plug and 3 dual split 2x2 extracting capacitors were joule time energy J/2 may equal 20VDC at 25 amp potential versus the 20 amp 12.7 max input expenditure fed back is a predictable 1.618 over unity as predicted in theory or 1.33 as tested in VTA in real lab testing (real world in vitro test)as is same universal principle.
  • Remember RV was first to show ratios of 1 to 12 (Cop 12) in virtual energy (radiant energy) over 1KW potential with off the shelve stuff. Can easy go 10 t0 30KW increasing frequency (with care not to Over destroying it) the way the information was put out was to force people to learn each step of the experiments as to make possible to open eyes to the KNOWLEDGE the whole represents. RV belongs to all of you... Looping it is almost there. And I can’t be happier about it! :)

22.dec.2006 posting with graphs

To clarify the timing of the SCR discharge in the deliverance RV resonance collection circuit, here is the timing diagram of the experiment I did with half a diode plug for extraction;

Graph A shows the low voltage triangle wave used in the deliverance inverter, and is used to generate the HV square waves to drive the RV PM input.
Graph B shows the square(ish) voltage at the input of the RV, together with the triangular voltage waveform across the RUN cap of the RV, which is delayed (lagging) by 60 degrees.
Graph C shows the discharge current spike from the RECOVERY CAP into the Load Battery via the SCR, which is triggered on the negative peak of the wave in graph A. This is during the BLANK PERIOD, after the RECOVERY CAP has fully been charged. Actually, the spike is a much shorter resonant impulse than shown. The load battery gets a 120V belt from the RECOVERY CAP, which doesn't reflect to the RV or the inverter.
For other applications, it may be simpler to just detect the PEAK of the Voltage waveform across the RUN CAP, and then fire the SCR at that time.

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