Fire Suppression Drone (Near Earth Object - Asteroid impact mitigation tool)
The following design system is a flight drone that can accommodate an occupant. The system is a "active" fire suppression method to then extract oxygen from the air directly above an active wild fire using arc destruction for oxygen removal, causing the continual production of chilled compressed Nitrogen and Carbon Dioxide to then be used upon the fire as a fire suppressant.
The flight drone then may also be useful in ocean search and rescue being a flight craft that does not require fuel for long duration search. The top mounting tool "groove" then may accommodate a boom and net deployment system to, at range, safely redirect an Earth impacting asteroid or comet. Multiple craft may be required. The net metal cable core then an insulated electric resistor (heater filament) to maintain material selection strength as the low temperature of outer space causes the "embrittlement" of material.
Parts List
1. air flight hyper electric jet engine discharge "rotator"
2. "rotator" control arm controls the position of the rotator
3. hyper jet air flight "rotator" hydraulic piston system changes position of the "rotator"
4. hydraulic piston pivot mount
5. screened air intake side port
6. electric motor transonic pneumatic impeller
7. electric "counter tilt" high speed ratio gear set (graphite lubrication / gear pump stir by internal air flow draft)
8. high speed transonic air flow compressor and electric "brush less" electricity generator about
the circumference of the air compression fan
9. intake air flow louver system (hydraulic actuation) used in high speed flight to allow more air into
the two electric air flight hyper jets
10. forward deflection pyramid (solid surface)
11. air intake louvers
12. video camera for instrumentation panel display monitor
13. environmental sensor array (to also detect radiation levels)
14. exterior lighting lamp
15. bolt system (mounts letter "B" into it's external shock casing upon the 360 degree rotation mounting)
16. decompression "pressure sphere"
17. super cooler refrigeration refrigerant flow pipes
18. super cooler refrigeration compressor and electric circuit controlled refrigerant switch block
19. super cooler refrigerant pressure tank with refrigerant fill compression fitting upon the flow pipe union
20. engine management control electronics "Bay" control electronic unit
21. thru bore electricity transfer slip ring / multi path signal for the helm to communicate with the engine
22. injector particle accelerator (electron injection plus electromagnetic "bottle" to focus ion flow from the
coil particle accelerator that produces low pressure within the engine force displacement end of the
sealed electric lifter motor)
23. ion flow restriction valve assist in the retainment of "pressure" within number 24
24. pressure sphere
25. engine flow temperature control valve
26. magnetic field accelerator field pump particle accelerator helical coil to "off set" the resultant return
force offsetting the "force static" then the flow cycle
27. electric motor compression transonic jet fan ( brush less electric motor )
28. engine main body venturi
29. electricity generator transonic air flow impeller transonic fan and input rotation to the high speed air
flow compressor number 27 with a 1:20 ratio gear set connecting the drive line so that the air compression
fan rotates twenty times faster than the impeller fan - magnetics in the generator system basal intensity
level to allow for electrical "tilt" ie... to produce more electric current than is being used by the acceleration
electric motor air flow compressor electric motor, number 27 - engine internal "inert gas pressure level" -
p.s.i. - pounds per square inch) a factor
30. engine thrust discharge venturi vents high speed inert gas air flow into low / negative "pressure" (vacuum)
31. thrust venturi over pressure safety valve and pressure sensor reports to engine management for
safe operation
32. electric compound hyper jets causes low negative pressure in the aft of the engine system and vents to
the helical particle accelerator coil
33. high speed ratio gear set to cause acceleration by inert gas "draft effect" 1:150 ratio gearing
sealed lubrication - contains electric counter tilted internal gearing and electric inductance grounding
system
34. brush less electric motor upon the circumference of the vacuum jet field coil
35. vacuum chamber
36. chilled air flow return pipe encased with the super cooler's refrigeration system evaporator insulated
shock casing feeds air to letter "L"
37. dual super cooler evaporators
38. electrical current pick up contained within number 29
39. brush less electricity generator rotating field coil
40. electron injector - ionizes the inert gas (Argon) within the engine system - also used for high speed flight
41. pneumatic impeller
42. main electron injector
43. electron injector
44. electricity transference slip ring
45. micro wave transmitter to "pressurize" the flow of ionized plasma by carrier wave compression
46. letter "b" outer casing for the engine's 360 degree rotation rotator mounting hydraulic fluid positioning
to spin the sealed jet, Letter "B"
47. electric motor and reduction gearing with safety system for correct operation tandem rotating with
the hydraulic position impeller in number 45 to the assist in the control of the position of letter "B"
48. cargo "bay" hydraulic piston system lowering system pressurized part of the drone that runs the length
of the vehicle
49. lower hull surface cargo bay floor (non slip surface)
50. outer hull electromagnet ship shield magnetic surface
51. internal air processing and atmospheric storage CO2 scrubbers (redundant) water processing
52. electronics "bay" accessible from the interior of the craft (instrumentation electronics - dial flight
hardware)
53. levitation hydraulic piston assembly
54. pitch yaw roll levitation system - the sealed motor in letter "E" also assist in pitch yaw roll
55. cockpit roll electric motor and gear assembly
56. craft hydraulic pressure electric motors "brush less" electric motor flight controls
57. craft hydraulic pump used for the hydraulic flight control system (also with
cross over flow valve system to use the hydraulic flight control system hydraulic pressure to lower
the landing gear or vise versa to use the landing gear hydraulic pressure to route to the flight
controls - used if component failure occurs
58. landing gear hydraulic pressure system "brush less" electric motor
59. landing gear hydraulic pressure system hydraulic pump
60. landing gear hydraulic piston system
61. landing gear sway bar and shock absorption (shock absorption piston system - strut)
62. landing gear tire
63. cockpit chair - toilet - heater seat - stereo - communications system
64. instrumentation arm rest - cup holder - ship instrumentation display panel
65. septic treatment system
66. armor lock (used in high speed flight as the occupant then stands inn the vertical position for better
shielding after the cockpit chair has tilted forward and allows the pilot to stand upon the grid particle
detector - a safety feature to warn of high energy particle gain vs. speed of flight craft)
67. particle detection grid standing platform
68. landing gear tire
69. instrumentation display panel environmental atmospheric "jack in" for sealed space suit should hull
breach occur redundant / emergency atmospheric "pressure" space suit umbilical jack in
70. water / lamp / ship internal heating and ventilation system
71. water / lamp / ship internal heating and ventilation system
72. tool dock hydraulic piston system
73. tool dock lock
74. tool dock lock
75. tool dock lock electromagnet
76. hull insulation micro particle impact shied surrounds the occupiable compartment - pressurized
hull - entry hatch behind the levitation "tumbler" letter "D"
77. external vessel shield electromagnet shielded magnet pole - magnetic shielding for the internal of the
craft to then not effect the pilot with high intensity magnetism
78. external hull magnetic shield electromagnetic emission points at number 50 both sides of the craft
79. levitation tumbler field coil
80. levitation core guide roller wheel
81. levitation tumbler "armature frame"
82. armature frame fixed electromagnet
83. height adjustable electromagnet
84. height adjustable electromagnet connecting bracket
85. tension guide hoop accepts slide bar - upon each "end" of electromagnetic plates that have
height adjustment (keeps the adjustable electro-magnetics aligned - slide bar the locks to the field coil
of the levitation tumbler)
86. armature frame fixed electromagnet
87. armature frame core spindle
88. adjustable electro-magnets connecting bracket
89. hydraulic pressure coupling - causes the level adjustment of hydraulic fluid in the hydraulic piston
number 90 that raises or lowers the adjustable electro-magnets to produce lift upon the armature frame
at the roller wheel contact points thus lifting the circular field coil that is mounted to the vessel
hull - inner hydraulic fluid pipe mounting the has the ability to rotate for structural integrity of the
hydraulic fluid flow pipe from number 94
89. hydraulic fluid pressure coupling
90. hydraulic piston
91. armature frame
92. lower "plate" connects the bracket that raises and lowers the adjustable electromagnets
93. electric motor armature windings allows for the lift vector of the levitation assembly to change position
about 360 degrees circular armature sum of two each side of the levitation tumbler the circular
armature then bolts to the frame also locking by bolt system to the fixed electromagnetic plates. The
rise plates (electro-magnetics), then are able to remain in their reference by the guide bars that allow
motion travel by electromagnetism
94. hydraulic piston mounting assembly - mounts to sealed lubrication bearing races that have the core
spindle at their center
95. thru bore electricity transference "slip ring" multi path circuit slip ring
96. hydraulic fluid flow pipe
97. connecting rod bore hole
98. nut and bolt assembly (the adjustable electromagnetic "plates" move in tandem)
99. locking hydraulic piston and plate union
100. roller wheel guide track affixed to the circular frame of the levitation tumbler that accommodates the
field coil wire windings
101. hover motor mounting frame mount points (rotates 360 degrees)
102. hover motor mounting frame (rotates 360 degrees)
103. hover motor electric motor (rotates the force displacement of the sealed force vectoring hover motor
letter "A")
104. hydraulic positioner for the hover motor
105. radian sensor (detects the position of the displacement force vector to then allow for the helm to
adjust the hover motor's position) used with the electric motor number 103
106. hydraulic fluid flow pipe
107. hydraulic fluid flow pipe
108. ribbon wire / multi wire radian sensor current feed
109. letter "B" pressure tank for high velocity ionized Argon
110. dual coil flow pipe to the pressure chamber for the main electric jet
111. vacuum chamber elongation - allows for better performance dynamic
112. aerodynamic flow guide
113. pneumatic compressor and brush less electric motor air flow compression fan electric turbo jet
114. high speed compression jet fan electricity generator brush less generator 1:20 ratio gear set so that
the electric generator jet fan is rotating twenty times faster than the input rotation produced by the
pneumatic impeller, number 113
115. high velocity return coil to offset the "static" in the force equation by perpendicular reintroduction
of flow velocity
116. vacuum jet fan system electric (sum of four) about the center point of a circle to "cause" negative
pressure at the discharge of pressure and velocity
117. brush less electric motor transonic impeller accelerates the compression fan (number 113),
compressor air flow chamber discharge into valve venturi "funnel" with 9 port holes to then increase
air flow discharge pressure
118. electric cable wench (rescue wench)
119. cable hook
120. air craft lamp
121. electric motor and reduction gear assembly (drive chain and sprocket system - locking ratchet)
122. drive chain
123. drive chain
124. tension sprocket adjustable
125. mounting base locks to number 75
126. active fire suppression boom structural member
127. electric motor sprocket / drive chain wench system to "tilt" the active fire suppression
air stratifier liquefaction unit letter "C"
128. drive chain
129. hinge
130. quick release union plate allows for quick exchange of the fire suppression head
131. hinge
132. magnetic field inductance control cage (prevents engine loss due to electromagnetic pulse)
133. impact / insulator - carbon carbon + expansion gel laminate
134. boom guide plate (also mounts number 124)
135. impact casing
136. aircraft beacon lamp
137. plasma arc oxygen destruction unit - removes the O2 (oxygen) from the system intake air
138. liquid N2 (nitrogen pressure tank)
139. air intake orifice
140. fire suppression exhaust air flow (minus the oxygen)
141. pneumatic draft impeller drives the piston type air compression pump in tandem with the electric
clutch upon the drive line
142. two cylinder liquefaction compression pumps (sum of two independent units)
143. air flow distributor
144. super cooler evaporator cooling exchanger flow pump
145. lower evaporator (refrigeration system) chills the air flow travel coil entering number 170
146. super cooler evaporator
147. super cooler refrigeration compressor
148. super cooler refrigeration switch block
149. super cooler refrigeration refrigerant tank
150. super cooler condenser cooling fans
151.
152.
153.
154.
155.
156.
157.
158.
159.
160. super cooler condenser
161. casing vents
162. refrigerant fill valve one way valve
163. refrigeration evaporator
164. air intake vents
165. reintroduction air flow sensors / valve system includes pressure sensors
166. electric clutch
167. electric compound hyper jet blower fan system electric jet engine
168. 1:150 ratio gear set to then cause acceleration by pneumatic draft
169. electric blower and electric motor circumference
170. air flow distributor valve system
171. pneumatic travel coil "chilled"
172. super cooler evaporator
173.
174. super cooler condenser
175. air flow distributor - the system also uses long tubes perpendicular to the air stratifier head to increase
the fire suppression effective area
176. vacuum chamber
177. air compressor - refills automatically
178. air compression control system
179. static electricity control unit remove unwanted electrical charge from the flow system
180. pulley
181. marker / work lamp aircraft beacon lamp
182. oil fill coupling
183. valve control solenoid
184. vacuum system negative pressure in the lower part of the hover motor
185. pressurized chamber compression seal
186. flight control yolk
letter "A" = main hull lifting bank hover motors sum of six total three each side ( sealed force
vectoring ) - contains venturi restriction lock plate between the hyped electric compression system
and the vacuum producing fans. the venturi "plate" then containing multiple funnel shape venturi to
compress the air flow and increase the air flow speed sum of 9 eight in equal spaced circular
array and a larger diameter port venturi / "funnel" in the center of the plate as the main thrust port
letter "B" = hover motor with electron compression by frequency transmitter (high speed flight sealed
force vectoring)
letter "C" = super cooler and active nitrogen carbon dioxide used as a fire suppressant
letter "D" = levitation core / levitation "tumbler" a multi position electromagnetic lifter motor power feed by
flex ribbon wire to the electromagnetic plates
letter "E" = fuel less "pressurized hydraulic draft effect fuel less electricity generator"
letter "F" =
letter "G" = air flight electric compound hyper jet
letter "H" = air flight electric jet air velocity displacement rotator
letter "I" = hover motor mounting frame and electric motor system to control the orientation of
force displacement circular rotation
letter "J" = particle accelerator assist in negative pressure / vacuum in the aft chamber
letter "K" = wild fire suppression boom
letter "L" = vacuum producing electric hyper jet
letter "M" = hydraulic fluid restriction valve electric circuit controlled
letter "N" = hydraulic fluid impeller centrifugal type
letter "O" = voltage regulator feeds controlled electricity level to the field coil armature - circuit contained
so that the field coil armature within the high voltage electrical generator can be increased
letter "P" = dual shaft electric drive motor brush less
letter "Q"= electricity thru bore electrical current transfer slip ring used to electrify one half of
the electromagnetic clutch
letter "R" = electromagnetic clutch
letter "S" = redundant magneto "back up" also acts as resistance break to prevent "run away effect"
current transfer slip ring to "electrify one half of the electromagnetic clutch
letter "T" = magneto permanent magnet electricity generator "brush less"
letter "U" = 1:20 ratio gear set - high side of the ratio gear set tandem rotating with the armature
of letter "V" allows for electrical transference from the voltage regulator to the field coil armature
of the high voltage generator, letter"V"
letter "V" = high voltage brush less electricity generator
letter "W" = high speed hydraulic fluid, fluid pump
letter "X" = pneumatic "start" impeller
letter "Y" = r.p.m. ( revolutions per minute sensor) reports to the generator's speed control electronics
to maintain safe operating speed
letter "Z" = electricity generator control electronics sonic "on / off" switch
Description....
The above design concept is an advancement in large wildfire suppression allowing for on site active collection of fire suppression material. ie... the air itself is a fire suppression material once the oxygen has been extracted or "converted" in CO2 / N2. This allows for a quicker fire extinguishment of the fire as the drone then can be in use without having to fetch water, as helicopter's do or reload fire retardant as large aircraft do...
It is important to understand that this design concept then also does not require fuel to operate. The system is electric. The design system will "break gravity" without fuel then able to be used as an asteroid impact avoidance tool. To then keep the earth safe from asteroid impacts.
* Note - letter "E" powers letter "A" with the assistance of the produced electrical current from number 114
* Note - redundant letter "E" placed behind the levitation tumbler to power craft systems sum of 4 - lift level
to counteract tool "weight"
*
Design Desk Inc.
Geoengineering - Climate Change Mitigation
Disclaimer - If attempting to produce these design yourself additional engineering may be required.. Design Desk Inc. will not be held liable. If you proceed with construction your self it's at your own risk... by use of "free to use systems" you acknowledge and accept the terms.. ( Please note not all systems contained here in have been released ).
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