Design Desk Inc.
Flight Stabilizer
The following electromagnetic flight stabilizer is intended for use in long range high speed aerospace systems to auto correct flight trajectory deviance.
Parts List
1. Servo electric motor "wire bus" / multi wire
2. control arm bearing retainer
3. center pivot bearing retainer for control arm positioning
4. control arm end gear stops
5. positional sensor "wire bus" / multi wire
6. positional sensor / indicated force vector of electromagnetic stabilizer
7. control arm
8. gear guide sum of two per unit ( one left one right also using roller gear mounting to the rail mounting
frame for the electromagnets.)
9. control arm mount positional sensor / magnetic interrupt
10. pivot arm force vector assembly roller gear
11. pivot arm force vector assembly sum of six times about 360 degrees contains dual directional electric motor and reducer
gear system high spin input to low speed / higher torque rotation to position the electromagnetic system at different angle.
12. fixed position electromagnet
13. outer "repellent" electromagnet
14. high tensile strength connecting slide rod prevents magnet mal-alignment
15. hydraulic hose / pneumatic hose guide rings - mounts hydraulic and or pneumatic pressure feed hose
16. fixed position electromagnet
17. fixed position electromagnet
18. draft electromagnet - increased electricity induced magnetic field to cause high pull yielding a locking effect for force
to stabilize flight trajectory
19. pneumatic and or hydraulic fluid transfer thru-bore transfer slip ring
20. guide rail mounting system - mounts the electromagnetic assemblies ( number 11)
21. guide rail mounting system - mounts the electromagnetic assemblies ( number 11)
22. system sensor vector deviance sensor - allows auto adjust of system electric levels and position of the produce
force vectoring to stabilize vessel flight trajectory.
23. inductance dissipation "cage" prevents unwanted external inductance - also acts as an electrical ground
24. system manual user interface - system control panel - system / "logic circuit mapping" - electrical control panel
25. hydraulic or pneumatic piston system
26. electrical ground point
27. inductance "cage" hinge mount for inductance panel
28. pneumatic pressure or hydraulic fluid pressure flow lines - tube / hose - with compression fitting ends
29. hydraulic fluid pressure and or pneumatic pressure flow lines / tube / hose / pipe
30. structural frame
31. electromagnet unit mounting connector
32. electromagnet unit mounting connector
33. electromagnet unit mounting connector
34. projectile safety shield - rated to prevent projectile due to slide rod failure
35. frame electrical ground
36. electrically insulated hull mount mounting system
37. slide rod bearing race
38. hydraulic fluid pumping system
39. pneumatically pressurized hydraulic fluid reservoir
40. circuit controlled hydraulic fluid control valve - changes the fluid pressure to the hydraulic fluid piston assemblies.
41. hydraulic fluid pressure by-pass valve -rerouted the fluid pressure back to the reservoir
42. electric hydraulic fluid pump system - contains electric motor and reducer gear system for high level fluid pressure.
43. hydraulic fluid pressure reservoir fluid exhaust drain feeds oil to the hydraulic pump system
44. hydraulic fluid reservoir oil return compression fitting - flow line contains one way valve to prevent back pressure
45. pneumatic fill valve
46. hydraulic fluid fill one way valve
47. hydraulic fluid flow hose / pipe
48. fixed structural frame "compression box"
49. pneumatic piston assembly
50. electric actuation dual directional electric motor with gear to move the bar gear that compresses the air inside
the pneumatic piston assembly
51. bar gear affixed to the pneumatic piston assembly
52. pneumatic pressure storage tank
53. "return" pneumatic flow hose / pipe
54. vacuum tank
55. air pressure tank
56. air compressor electric motor driven
57. pneumatic regulator valve
58. "return" air pressure manifold - accepts compression fittings
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