Tri - Plex Lifter
The Tri - Plex Lifter is an aero space design concept that operates on a fuel less platform to force vector objects into space or to lift ships into orbit. The system is a pneumatic cycle that produces vacuum pressure at the lower or base of the system while pressurizing air at greater rate than the core discharge. This is an attempt at causing a lifting mechanism with zero exterior intake or zero exhaust from the mechanism. A sealed hover system with lifting capacity. Also for use in Asteroid or Comet mitigation.
The reason it is called a Tri -Plex Lifter is because of the structure of the vacuum intake ie. three structures of vacuum production yet four methods of producing vacuum due to the addition of horizontal pressurization by Z.
*notes*
Number 3 is a pneumatic pressure return tube...the dashed lines indicate the connection to the views opposite side as the ports are arrayed about 360 degrees. (it is a solid tube...)
Within number 8 (1:2 ratio gear set) an addition of electromagnetic clutch will be contained within the gear set.This allows for a variable rate increase of core velocity displacement.
The "air" ( Argon ) within the system should be as free of humidity as possible. Also the flow systems should be electrically grounded to direct static electricity produced within the pneumatic flow system. The pneumatic flow tubes will be insulated for electricity and correctly grounded.
Number 18 also contains an R.P.M. sensor that reports to the mapping computer.
The drafting is a side view of the mechanism and the center line is also a mirror line so that the parts can be understood (same on each side ) . Also the drafting as depicted then viewed from atop then about the center point to then polar array 3 times (3x, 4x, 5x continuing to increase in array number about 360 degrees).
The outer casing encloses the design system with accessories for lifting......and or additional "tube form" (disk lifter engine), engine systems for yaw pitch and roll force vectoring.
To balance the tendency to rotate while in "flight" the transonic compressors should rotate counter to the effect of pressure cycling within the coil. Pneumatic flow resistance fins can be added within the core compression venturi to add to the stable flight intent and counter act the tendency to rotate..
Note - Number 26 as a Magneto / circumference ( permanent magnet Ac production then regulated feeding the field coil stator in the generator circumference of number 29) also
then rotated by an electric motor number 27 and number 29 then as a High Voltage generator then converted to Ac ( alternating current / High Voltage electricity production )
generator. Number 29 then re- introduces current to number 27.
Note - Additionally to component "Z" then installed in the ratio gear set are then one hydraulic impeller and one hydraulic pump ...each rotating tandem with drive shafts then connected to each side of the ratio gear set... the hydraulic pump then positioned upon the high side of the ratio gear set then pumping silicone oil under pressure by argon gas into the pressure tank ... a combined cycle dual pressure containment tank containing pneumatic pressure ( argon) and silicone oil .
The oil exhaust tube from the pressure tank ,containing flow control valve, then enters the hydraulic impeller connected to the low side of the ratio gear set, causing rotation by the drafting of hydraulic pressure into the hydraulic pump ( via tube ) hydraulic pressure tube. The hydraulic pump then rotating tandem with the high side of the ratio gear set and venting the hydraulic oil ( via tube with one way flow valve) back into the combined cycle dual component pressure container.
Safety systems to regulate the pressure flow of the oil and will be able to the restrict the oil exhaust flow from the combined component pressure storage tank into the impeller. The system then will cause the through air then being compressed to cause velocity incline... for use within the design systems. The combined pressure storage tank has mounted upon it a one way valve allowing for the oil filling and the argon filling as well. The flow tube connecting the oil cycle then also contain the correct rated pressure fittings / couplings.
The system is electrically grounded and also "dipped" ( exterior ) in a non conductive plastic / rubber electrical insulator to prevent a shock hazard.
"Z's" Parts List
1. One way Fill Valve ( silicone oil and Argon gas high pressure
2. max pressure gas pressure relief valve ( safety valve )
3. Argon gas high pressure
4. Silicone oil
5. Oil flow control valve
6. Screened air filter exhaust valve
7. Stator / field coil ( generator )
8. Transonic impeller
9. Hydraulic impeller
10. High voltage generator Dc or Ac current
11. Hydraulic pump
12. Electric motor
13. Pneumatic impeller , can also valve route then to act as a air / argon compressor then to pressurize the combined oil/ air pressure storage tank
14. 1:20 ratio gear set High side rotation tandem to number 11, low side rotation tandem to
number 9
15. "dipped" electrical insulator
16. Electric motor
17. Commutator
18. Drive shaft hub cap
19. Pneumatic pressure intake tube "Air in" ( may also be argon in closed system )
20. Oil (hydraulic) pressure tube
21. Oil (hydraulic) pressure tube
22. Magneto circumference
23. Transonic compressor propeller
24. High voltage generator
25. One way flow valve
26. drive shaft
27. R.P.M. ( revolutions per minute ) sensor
Geoengineering - Climate Change Mitigation
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