Acorn Engine System
The "Acorn Engine System" is a sealed engine system implementing high pneumatic pressure and vacuum upon an electric compound hyper jet.
The design is intended for use in the MedEvac Search & Rescue ambulance located at http://www.designdeskinc.com/medevac-search---rescue-ambulance.html
In critical situations or inclement weather current transit methods are limited in duration of function then bound by fuel and or are not designed for extreme weather conditions.
Parts List
1. pneumatic pressure sphere- contains manifold pressure sensors upon each discharge manifold reports
to the systems logic electronics to then safety the system to limit the engines systems not to
exceed mechanical tolerances of the components material selection.
2. sold engine cap ( contains electrical inductance "cage" )
3. oil fill plug
4. core drive shaft locking nut assembly
5. final balance " fly wheel" bearings
6. oil filled torque converter and generator Permanent Magnet type generator
7. torque converter electricity generator
8. torque converter roller ball "brushes" commutator contacts
9. core electric jet intake manifold
10. bi-directional pneumatic compressor
11. electric motor impeller transonic jet fan accelerates upon pneumatic displacement of number 50
12. pneumatic flow venturi ( focus of thrust "cone" )
13. pneumatic pressure storage toroid / torus
14. primary vacuum jets
15. lamp housing "search light"
16. fuel less generator "bay" contains fuel less generator system listed
at http://www.designdeskinc.com/cross-pump-generator.html redundant also casing contains inductance
"cage" as stray electrical voltage control system. The start venting upon the cross pump generator
schematic , number 32, then union port connected vent piping to the vacuum chamber number 17 upon
the Acorn Engine design. The intake to then "re-pressurize" the cross pump generator then an
additional pneumatic feed "air pressure" pipe from the pressure storage tank upon the Acorn Engine
design , number 18.
17. Main vacuum chamber
18. diameter of pneumatic pressure storage toroid / torus
19. baffle - allows for the force vector high velocity pressure to then have low pressure effect close to the final
containment casing , contains bore holes to control the outer chamber "pressure keeping the system within
the material selection mechanical tolerance
20. circumference thrust tubes negative pressure toroid / torus connects to the main vacuum chamber
21. 1:10 ratio gear set aligned so that the input torque is by the electric motor transonic and the out put rotational
torque is then advancing number 10 at ten times the velocity. This allows the fixed yet adjustable electricity
flow powering number 11 to then ride atop the compounding velocity rate of rotation.
22. throttle assembly - air flow valve
23. pneumatic flow valve actuator polar array upon the unit redundant total of four times
24. hydraulic flow valve actuator polar array upon the unit redundant total of four times
25. vent tumbler height position
26. pneumatic pressure sensor ( valve pressure sensor - measures the internal pneumatic pressure
of the chamber)
27. focus venturi air flow port inverse open ended funnel cone
28. pneumatic guide ports
29. re-tension spring keeps the valve closed in it's natural position array about the polar center point eight times
30. system circumference thrust tube control valves electric positioning with pneumatic feed pressure
as redundant back up actuation by manual sheathed steel cord.
31. bearing race
32. commutator for the electric motor , number 88 roller ball "brush contacts"
33. commutator for the electric motor , number 88 roller ball "brush contacts" - stagger hour use life of
the "brush" circuit as fault safety to indicate brush failure
34. primary horizontal electric compound jets ( detailed component same as number 79 )
35. core electric jet R.P.M. ( revolutions per minute ) sensor reports to engine system electronic circuit
system "mapping" control board
36. commutator - redundant "brushes" roller ball type brushes
37. pneumatic discharge tube internal baffle contains multiple ports to allow a low pressure between the
baffle and the chamber wall
38. lower pneumatic pressure manifold - feeds air pressure controlled to the independent internal electric
jets "Air Drive" system so that if electric component fails the system will still produce rotation upon
pneumatic pressure. A back up flight system.. may be automatically instigated by the system
logic / mapping electronics
39. center electric jet vacuum manifold - pulls air pressure from between the baffle and the chamber wall
40. pneumatic flow valve hydraulic flow pipes / hoses
41. pneumatic pressure injection valve - electric - adjust the "pressure bubble in the venturi
42. electric air compressor connected to components as illustrated by flow pipes sum of six
about the circumference
43. air compressor control valve
44. multi wire "ribbon wire" electrical wire control circuits
45. main pneumatic pressure "static force canceling" pneumatic return coil flow pipe / tube
46. inner pneumatic pressure return coil assist in vacuum production to aid the system in obtaining
pressurization differentiation within the engine system - "keeping" the high pneumatic pressure
toward the top of the system and vacuum upon the discharge low end of the design as depicted.
47. electronics "bay" mapping logic circuits
48. fuel less generator electrical power supply listed athttp://www.designdeskinc.com/cross-pump-generator.html
49. vacuum assist "up draft " flow fan blade tilt pneumatic compressor
50. transonic propeller air compressor " down vector discharge
51. hyper jet compressor pressurizes the core electric jet faster than the discharge to then keep the
pressure atop while producing sealed lift as effect same schematic as total system listed as number 79
52. electric motor
53. union point bolt plates - rivet joined
54. pneumatic centrifugal impeller
55. 1:50 ratio gear set high side rotation tandem to number 53 and subsequent assembly
56. pneumatic counter tilt impeller - reduces the mechanical resistance of the ratio gear set
57. pneumatic impeller mounting system
58. fly wheel
59. lock washer
60. lock nut threaded
61. hyper jet mounting casing
62. pneumatic draft impeller
63. R.P.M. sensor
64. Hyper jet transonic generator and propeller
65. hyper jet core system mounting bracket
66. aero flow stabilizer guides the internal air flow to assist in directional stability - prevents excessive
helical motion of the air flow multiple units within the system from end point center point polar array
sum of four vanes
67. generator stator / field coil with variable intensity electric coils around the permanent magnets
to then increase the electromagnetic field of the stator within the engine system yielding more electricity
out put volt and current intensity level controlled by volt regulator and potentiometer.
68. volt regulation
69. redundant volt regulator
70. venturi maximum pressure sensor one way flow valve ( vents via pipe pressure from the venturi
into the vacuum chamber and reporting pressure sensor - contains fault indicator is the pressure
sensor has failed
71. hyper jet feed pipe pressure couplings
72. vacuum tank pipe coupling allows the air pressure from the hyper jet's internal impeller system to
then vent into negative pressure
73. vacuum level sensor upon the pneumatic feed flow pipe to the air compressor valve control
74. hyper jet manifold feed pipe from the air compressor , number 42 and or air pressure storage tank number 18
75. flow pipe union via coupling to the vacuum chamber - negative pressure tank
76. full encasement " electrical inductance cage" acts to prevent engine disruption by lightning strike
and or electromagnetic pulse
77. plasma box - control discharges any static electricity - contains actuation sensor and as a
safety feature a fault indication circuit
78. multi wire "bus" connector
79. hyper jet
80. electricity generator commutator
81. roller ball contact "brush" for electricity transference
82. roller ball contact "brush" for electricity transference
83. electric motor circumference and diameter pneumatic draft impeller
84. hyper jet engine core mounting bracket
85. internal static electricity control - static electricity is collected upon the outer casing of number 21
86. external casing of number 36 is a multiple resistor electric resistance heater and cooling grid with
the refrigeration system then in the air compressor valve control bay , number 47, cooling system
by pneumatic flow as a sealed transfer medium so that the flow can be recovered should rupture
or leak occur also placement of refrigeration condenser connects to number 47
87. core thrust chamber
88. torque converter rotation balance weight places where required to stable any wobble within
the system - there are multiple the weight retainer is circular atop the torque converter
89. electricity generating transonic jet fan impeller causes number 50 to higher rates of rotation via
the ratio gear set number 21
90. refrigerated venturi via refrigeration system in number 47 connects via flow pipes
91. pneumatic flow pipes actuates the pneumatic piston opening valve ,number 23 allowing air flow
92. solid engine cap mounting bolts about the circumference contains inductance cage and carriage
mount system that attaches to the mobile servo electric position system to control final force vector
of the internal displacement
93. engine mount
94. mounting bolt plate - rivet plate
95. strut - shock absorption - shock absorber
96. mount union link - pivots to also dampen excessive load or discharge of the engine system when
heavy acceleration is occurring
97. strut - shock absorption - shock absorber
98. hydraulic shock absorption piston
99. mobile mount engine link mount engine system to the mobile
100. mobile carriage
101. rotating servo contains current transfer thru bore slip ring to allow the engine system to
connect - communicate to the ships cockpit multi track also allows for the manual cable system
function to then be actuate via hydraulic interface upon the servo - hydraulic system then
moving the sectional manual flight system.
102. multi wire bus "ribbon wire" electric circuit control ribbon wire connects to the multi track thru bore
electrical transference slip ring . The other half of the thru bore electricity transference slip ring
then connects to adjacent mounting thru bore electricity slip ring repeating until the current is able
to be directed to the cockpit control systems hydraulic slip rings then transfer mechanical motion
with sheathed cables to then manually adjust the system as redundant flight controls.
* Note - The design system then can be used for commercial air craft to then act as a gentle hover
landing system multiple Acorn Engines ( mounted within the hull and or upon the exterior)
to forever prevent jet liner air craft crashes due to engine failure.
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