Geoengineering - Climate Change Mitigation

Design Desk Inc.

MedEvac Search & Rescue Ambulance

Currently with so many natural disasters regarding the changing climate increased search and rescue medical systems have become costly and at times not enough to then provide adequate service due to the nature of the current design system capacity or cost associated with performing the required functions.

The following design system is much different from current methods of search and rescue. The design system then acts as a  hover craft then implementing sealed engine system thus not displacing high velocity air to remain aloft. The engine system for this design system is called an "Acorn Engine". The system then is an electric flight system implementing fuel less high density high voltage production of electricity.

The design is then also able to attach multiple service  "bays" to then act according to the systems installed. The flight system then may also be used for planting forest, fire suppression using Nitrogen derived from via air

stratifiers (, and or to be used to transport  commodities for commerce. The interchangeable "bay" then has flotation able to support the craft in the water for ocean rescues.

Parts list

1. air pressure  "return" volume sphere - allows a more responsive burst of air when accelerating

    by the hollow pressure sphere then containing a bit more volume of air

2.  solid - heated via electric resistance engine cap

3.  electric drive motor dual roller ball brush system (redundant electricity contact points )

4.  embedded electric resistor ( heats the engine cap to prevent icing )

5. upper air pressure reserve pressure torus - air pressure pressure tank

6. primary air flow coil "air flow" high pressure "return"

7. main air flow flow control valve / acts in tandem with system speed to attain required pneumatic

    force displacement to attain lift  .. acts in tandem with the electricity re-introduction system when the

    core electric jet is then speeding up to then control pressure level discharge

8. outer circumference air flow pump causes updraft in the position as depicted at the same time that

    the compressor transonic jet fan , number 11 is then causing pneumatic pressure and velocity in a

    downward fashion.

9.  pneumatic "draft" impeller causes total system to gain rate of velocity

10. 1:10 ratio gear set high side rotation tandem rotating with number 11

11. permanent magnet generator armature transonic compressor causes number 9 to "hyper draft" causing

      system incline rotation rates  producing electricity to then cause number 3 to become electrified. The

      system has electricity production redundancy upon each engine system located at the

      system's base, number 16

12. pneumatic discharge conical venturi "focus cone" - "funnel" acts to compress the air flow under great velocity

13. letter "J" then the same as letter "A" yet positioned and aligned to then become a vacuum pump

      assisting in the low pressure effect in the air jet discharge chamber

14.  high pressure pressure storage tank torus doughnut style pressure tank with external air

       intake and air compressor driven by electric motor.

15. vacuum chamber negative pressure retainer vacuum tank

16. fuel less generator "cell" bank redundant sum of four individual generator systems systems

      such as

17. negative pressure " lower return manifold sum of 8 about the center point polar array. Letter "G" is then

      eight times about a polar array from the center point of the engine's top view

      ( the depiction is in the side view)

18. inner return air flow coil pipe - fed air pressure from J then the "vacuum pump" with the same
     components as letter "A" pulling air between the baffle and the system casing to assist in causing
      the "low pressure effect in the discharge chamber letter "G"

19. injection air control valve

20. flow baffle - an air guide with holes in the length to allow lateral air flow into the vacuum system

21. hydraulic piston

22. hydraulic piston

23. water proof flotation

24. hinge

25. med bay mount for the primary hydraulic piston system

26. drain

27. step deck and grab rail

28. water tight door

29. operations deck enclosed base

30. deck drain pipe

31. electromagnetic lock for rear transonic air compressor (pneumatic pressure regain fan compressor lid lock)

32. air intake grid

33. hydraulic piston and rear compressor lid mounting coupling

34. electric resistor lid heater

35. air pressure recovery fan lid hinges sum of three

36. air intake manifold

37. electric air compressor- allows for active flight system pneumatic replacement pressure

38. rear marker lamp

39. safety parachute and associated assembly

40. rear market lamp and pneumatic parachute launcher

41. augmented static compressor upon spherical positional mobile positional servos electric

      redundant  and hydraulic The  "ring" thru bore current transfer slip rings then also contain multi-wire

      "ribbon wire" control system instrumentation wires ie... to then control the engines dynamic systems and 

       vector position  augmented static compressor listed at

42.  main engine system zero atmosphere yaw / pitch decompression chamber contains angled surfaces

       to then change the rate of system roll air craft position in zero gravity

43. angled surfaces

44. angled surfaces

45. adjustable pneumatic discharge nozzle

46. air pressure discharge nozzle control electric motor and linkage system

47. negative pressure end of the internal main engine system

48. circumference electric motor draft impeller input shaft to the core engine system thru shaft transmission

      also located in the venturi vented by letter "A" then as a system speed indicator R.P.M. system and within

      the intake flow to both letter "A" then also able to generate electrical current as a permanent

      magnetic dynamo

49. generator air compressor transonic jet fan mounting ratio gear set so that a 1:2 ratio is attained causing two         times the rotation upon the electric  draft impeller number 48 and is tandem with the core connecting

      drive shaft

50.  thru shaft transmission - so that the mechanical transmission then causes greater rotational out put

      rotation upon the larger output shaft/ pipe that tandem rotates with number 49. The input shaft the

      tandem rotating with the draft impeller number 48 that is also an electric motor. These systems in

      tandem allow for ultra high speed rates of rotation upon a set current as the draft effect will allow

      for the set rate of rotation by electricity to then incline as it rides atop the draft effect rotation.

51. commutators with roller ball brush systems extreme hardness conductor redundant brush systems

      off set failure rate per use hours

52. flow focus bracket

53. air pressure pressure tank

54. main engine system electric re pressurizing air compressor able to recover operating air pressure

      from outside the air craft

55. med bay air lock

56. access ladder

57. forward elevator / forward flap style elevator heated placed upon the upper wing leading edge

58. electric resistance heater

59. Acorn engine hydraulic bus hydraulic fluid bus with internal electric / pneumatic pumping to cause

      hydraulic fluid flow

60. med bay mounting points

61. rudder water or air motivated  by hydraulic bus hydraulic fluid bus with internal electric / pneumatic

       pumping to cause hydraulic fluid flow pivot mounted with electric servo.

62.  landing gear tire

63.  landing gear hydraulic lowering / retracting hydraulic pistons and shock dampening systems coil

       spring about the outer circumference of the hydraulic piston

64. forward electromagnetic field pulse bouncer / electron emitter " launches magnetic bubbles to then by

      force of microwave transmitter project in advance of the craft to then act as a field plow.

65. pilots chair

66. flight system management system fault indication ( shielded computer systems to prevent inductance

      due to electromagnetic pulse)

67. generator systems / atmospheric processing / communications / pulse plow transmitter / septic & water


68. canopy / cockpit door handle heated via electric resistance

69. floor mount landing gear pull lever and twist crank- hydraulic oil valve  - manual pump crank also
      lowers the landing gear

70. walk tread non slip surface for a good grip.... heated by electric resistance

71. forward lamps

72. main forward electromagnetic field pulse bouncer / electron emitter " launches magnetic bubbles to then by
      force of microwave transmitter project in advance of the craft to then act as a field plow.

73. air break causes aft letter "B" to cause retro force vector 

74.  yolk "steering " drives like an automobile with the addition of the elevator flaps then a

       push or pull,pull causes noes up

75. hover height lever craft altitude control handle

76. co-pilots flight control

77. lavatory co-pilots chair -water jet cleaning

78. optional bed stow under cockpit access through number 81

79. atmospheric processing atmospheric storage

80. canopy hinge and hydraulic piston assist to then lessen the weight of the the canopy

81. access hatch pressurized tube to the med bay

82. accelerator foot pedal

83. forward flotation hydraulic piston assembly "sinks the flotation upon telescoping hydraulic piston assembly

84. forward flotation hydraulic piston assembly "sinks the flotation upon telescoping hydraulic piston assembly

85. landing gear hinge

86. flotation pontoon

87. medical bay mounting points unions to the hull of the hover craft

88. hydraulic elevator piston

89. pneumatic elevator control piston

90.  solenoid elevator control

91. access tube

92. hydraulic servo  also positions by electric motor

93. Acorn Engine servo

94. servo hydraulic coupling

95. lid hydraulic

96. med bay air exchange h.v.a.c. external air filter heat dissipation for the internal air conditioning


97. H.V.A.C.  ( H.V.A.C. = heating ventilation air conditioning ) bay - contains the air handeling

      system / air filtration

98. heated encasement sphere

99. parachute pneumatic control

100. rescue wench and cable system

101. life preserver flotation life float ring

102. in frame tow hoop / mooring hoop

103. co-pilot computer display

104. Acorn engine servo pneumatic hydraulic  and electric actuation

105. multi track multi wire thru bore current transfer slip ring - contains electric transference to

        and from the Acorn to then control the system functions

106. static compressor servos - positions the sealed engine system contains thru bore current transfer

        slip rings multi wire "ribbon wire" to then control the engine system velocity and vector position

107. Aft Acorn Engine support mounting  frame

108. lamp

109. vacuum manifold - pulls negative pressure from the main force vector discharge

110. over pressure safety valve pressure tank over pressure vent

111. one way valve "pneumatic flow valve"

112. return air flow pipe

113. flow pipe

114. end shaft instrumentation R.P.M. sensor reports to system logic mapping flight electronics.

115. main air pressure tank sensor system with one way flow air pressure coupling

116. pneumatic control system  multiple coupling to then direct the generated air pressure to the

       crafts systems to then re pressurize the flight controls should the requirement it be necessary

117. high pressure pneumatic flow pipe

118. rear lamp

119. parachute ejection pneumatic rear lamp  launcher

Letter "A" is then the compound electric jet Multiple array within the engine system ie. about the center

                point if viewed from the top multiple additional letter "A" then in polar array. Letter "A" within

                letter "D" is then multiple system to then be placed about the circumference of the system if

               viewed from the end view center point to then be installed in multiple units attached to

               multiple ( sum of eight ) number 109 so that vacuum is attained within the thrust tube between

               the baffle and the outer casing to cause low / negative pressure effect letter "K" vents into the

               core of the baffle ( also depicted as number 20 also contained in the core internal forward

               flight engine letter "D" post venturi.

Letter "B" is then the "Acorn Engine system" a sealed force vectoring electric jet also listed


Letter "C" is then the air pressure recovery compressor fan

Letter "D" is then an internal sealed electric jet engine - note the aft discharge system , number 42  pitch

                 yaw displacement thrust are then four times about the center line, a polar array if viewed from the

                 end of the jet if the electric jet controls the crafts "roll"

Letter "E" then over head forward flap / elevator "wing" system

Letter "F" is then the landing gear position

Letter "G" is the the Acorn Engine thrust displacement circumference air pressure vector tubes sum

                 of eight about the circumference if viewed from the top center point in a polar array

Letter "H" is then the "Acorn Engine's" negative pressure manifold sum of eight upon each thrust tube letter "G"

Letter "I" is then the "Acorn Engine's" negative pressure torus connects to all letter "G"

Letter "J" is then the same format as letter "A" then acting as a vacuum producing electric jet

Letter "K" is then the air pressure "thrust control valve operated by hydraulics with level

                indication/ position electric linear sensor

Letter "L" is then the systems "bay" ie... medical equipment required in an Ambulance,  or other function

                interchangeable "bays" then for multiple other functions ie... forest fire suppression systems

                using active harvest of nitrogen to quickly put out wildfires,

Note - Letter lower "A" and Letter "J" then run at increased speed to always cause the "pressure

           bubble" atop the system replacing the pneumatic pressure faster than the down ward air force

           vector thus allowing lift.

Note - hard impact shield plus radiation shielding canopy translucent shield impact resistant
        lens tinted-  cavitation between the dual shield to allow  ultra high radiation protection to be pumped
        like liquid between the canopy covers two separate hard retainers - also acts to correct air pressure
        loss to then gum up a breech or fracture

The flight system then implements heated forward flap design upon the upper flight  "wing" and  then "rudders", number 61 also then assisting in the flight of the vehicle in air or in water. Water propulsion then upon the hinges flotation system actuated by hydraulic pistons to then extend by hydraulic piston deep into the water to then keep the Medical "bay" at the correct water height.

The trine "Acorn" engine systems then are able to pivot and adjust the force displacement upon the spherical positional mobiles. The range of motion then hemispherical with redundant modus of position, electrical servo hydraulic servo , and pneumatic servo. The "Acorn" engines then contain their own power supply system and will not vent air as they are sealed flight system electric engines. The aft ( rear engine system then has full spherical positioning and allows the air craft to then implement the retro position as an air break). Number 98 is then an "augmented static compressor" upon a spherical positional mobile to allow for high speed extra atmospheric flight. The engine  design then being a seal flight system resist failure due to volcanic ash, bird strikes, icing , or engine failure due to hail.

The forward lamp system then mounter upon the inverse high speed flight impact shield so that when in high speed flight the lamps, number 71 mounting housing then fold back atop the canopy and is the high speed flight impact shield.

The "Acorn" sealed electric engine system then uses negative pressure  "vacuum" low and off sets the "static return" in the force equation by perpendicular coiled pneumatic velocity return.

The internal hull engine labeled as letter "D" is then also a draft accelerator electric engine system with a 1:50 ratio motorized electric motor in number 51 with the high side of rotation then causing the generator number 49 to advance at greater rate . This causes system incline advancement in electrical production then directed to the transonic impeller electric motor (circumference), number 48.

* Note - the lines are then flow pipes except where indicated with a +/- to then indicate a wire....

The system may be used in tandem with the flight spheres thermohaline stabilizers "unmanned" listed at

( ) to then, with large net, connected to multiple "flight spheres" be able to capture comets and or asteroids. The flight system depicted in this html then the human occupied craft  (monitor craft), with the flight spheres then unmanned.