ENGINE PROPULSION SYSTEM

• US 20150013303A1
• Filed: 07/10/2014
• Published: 01/15/2015
• Est. Priority Date: 07/10/2013
• Status: Abandoned Application

• Current Assignee: Derrick T. Miller Jr
• Original Assignee: Derrick T. Miller Jr
• Inventors: MILLER, DERRICK T. Jr.
• Application Number:
  US14/328,546
• Publication Number:
  US 20150013303A1
• Time in Patent Office: Days
• US Class Current: 60/204
• CPC Class Codes: F02C 3/14 characterised by the arrangement of the combustion chamber in the plant combustion chambers per se F23R; F02C3/205 takes precedence
• CPC Class Codes: F02C 3/165 the combustion chamber contributes to the driving force by creating reactive thrust
• CPC Class Codes: F02C 5/02 characterised by the arrangement of the combustion chamber in the chamber in the plant combustion chambers per se F23R
• CPC Class Codes: F02C 5/04 the combustion chambers being formed at least partly in the turbine rotor
• CPC Class Codes: F02C 5/12 the combustion chambers having inlet or outlet valves, e.g. Holzwarth gas-turbine plants
• CPC Class Codes: F02K 9/00 Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
• CPC Class Codes: F02K 9/95 characterised by starting or ignition means or arrangements safety devices F02K9/38
• CPC Class Codes: F05D 2220/32 in gas turbines
• CPC Class Codes: F41A 19/13 Percussion or firing pins, i.e. fixed or slidably-mounted striker elements; Mountings therefor F41A19/26 takes precedence
• CPC Class Codes: H02K 7/1823 structurally associated with turbines or similar engines

Abstract

An engine propulsion system is configured to utilize bursts of media in order to create mechanical energy. The engine propulsion system includes at least one cannon, wherein each cannon is configured to displace the media and further includes a firing pin casing configured to accommodate a firing pin. The firing pin is configured to create the mechanical energy when moved thus allowing the media to exit the cannon.

Claims

1. An engine propulsion system further comprising:

turbine blades mechanically coupled to at least one cannon;

a turbine shaft mechanically coupled to the turbine blades configured such that the at least one cannon creates mechanical energy by turning the turbine shaft.

2. The engine propulsion system of claim 1, further comprising an electronic propulsion nozzle arranged proximate turbine blades and configured to allow space flight.

3. The engine propulsion system of claim 1, wherein the at least one cannon is configured to operate in a synchronized mode of operation.

4. The engine propulsion system of claim 3, wherein the synchronized mode of operation uses at least one motor.

5. The engine propulsion system of claim 3, wherein the at least one cannon has at least one exit port.

6. The engine propulsion system of claim 3, wherein the at least one cannon is a plurality of cannons and the plurality of cannons share an exit port.

7. The engine propulsion system of claim 1, wherein the at least one cannon is configured to operate in an alternating mode of operation.

8. The engine propulsion system of claim 7, wherein the alternating mode of operation uses at least one motor.

9. The engine propulsion system of claim 7, wherein the at least one cannon has at least one exit port.

10. The engine propulsion system of claim 7, wherein the at least one cannon is a plurality of cannons and the plurality of cannons share an exit port.

11. An energy generation tubing or channel configured to charge a battery;

the energy generation tubing comprising;

a plurality of turbine shafts each mechanically coupled to a plurality of turbine blades;

at least one generator attached to each turbine shaft forming a series of turbine/generator systems; and

a medium surrounding and passing the series of turbine/generator systems which creates electrical power.

12. The energy generation system of claim 31 further comprising a surface around the energy generation system that is sealed and covered in order to prevent injury which otherwise could be caused by exposure to the surface.

13. An energy generation tubing or channel configured to charge a battery;

the energy generation tubing comprising;

a plurality of turbine shafts each mechanically coupled to a plurality of turbine blades;

at least one alternator attached to each turbine shaft forming a series of turbine/alternator systems; and

a medium surrounding and passing the series of turbine/alternator systems which creates electrical power.

14. The energy generation system of claim 33 further comprising a surface around the energy generation system that is sealed and covered in order to prevent injury which otherwise could be caused by exposure to the surface.

15. An electronic system, configured to operate an engine propulsion system to create mechanical energy, the electronic system comprising:

a central processing unit mechanically coupled to the engine propulsion system and configured to engage the engine propulsion system.

16. The electronic system of claim 15, wherein the central processing unit further communicates with a local processing unit communicatively coupled to solenoids which directs the engine propulsion system.

17. The electronic system of claim 15, wherein the central processing unit further comprises processor instructions for accelerating the engine propulsion system, further comprising:

calculating stored energy available.

18. The electronic system of claim 15, wherein the central processing unit further comprises processor instructions for accelerating the engine propulsion system, further comprise:

determining additional energy and/or firing rate needed to accelerate.

19. The electronic system of claim 15, wherein the central processing unit further comprises processor instructions for accelerating the engine propulsion system, further comprise:

increasing pressure and/or firing rate of a media thereby obtaining additional energy.

20. The electronic system of claim 15, wherein the central processing unit further comprises processor instructions for accelerating the engine propulsion system, further comprise:

increasing a cannon firing rate.

21. The electronic system of claim 15, wherein the central processing unit further comprises processor instructions for accelerating the engine propulsion system, further comprise:

calculating and displaying a time until stored energy and/or media is depleted.

22. The electronic system of claim 15, wherein the central processing unit further comprises processor instructions for decelerating the engine propulsion system, further comprise:

reducing a cannon firing rate.

23. The electronic system of claim 15, wherein the central processing unit further comprises processor instructions for decelerating the engine propulsion system, further comprise:

decreasing energy being emitted on the engine propulsion system.

24. The electronic system of claim 15, wherein the central processing unit further comprises processor instructions for decelerating the engine propulsion system, further comprise:

calculating and displaying a time until stored energy is restored.

25. The electronic system of claim 15, wherein the central processing unit further comprises processor instructions for decelerating the engine propulsion system, further comprising:

displaying an error if an operating rate is less than or equal to a rate to increase stored energy;

but only if a first stored energy value at a first time is equal to a second stored energy value at a second time.

26. The electronic system of claim 15, further comprises a local processing unit communicatively coupled to each solenoid wherein at least one solenoid is mechanically coupled to at least one cannon;

wherein the local processing unit directs the at least one solenoid as to when to fire each connected cannon.

27. A process for creating mechanical energy on a rotating device;

the process comprising;

directing a propulsion device towards the rotating device;

pushing a media from the propulsion device creating a force;

wherein the force moves the rotating device creating the mechanical energy.

28. The process of claim 27;

further comprising directing flow of the media with at least one solenoid.

29. The process of claim 27;

further comprising isolating media from all channels with seals and preventing the media from inadvertently escaping a controlled exit.

30. The process of claim 27;

further comprising connecting an electrical power generation device to the rotating device.