Rotary units, rotary mechanisms, and related applications

• US 8,834,315 B2
• Filed: 03/15/2013
• Issued: 09/16/2014
• Est. Priority Date: 10/12/2008
• Status: Expired due to Fees

• Current Assignee: Christopher C. Sappenfield
• Original Assignee: Christopher C. Sappenfield
• Inventors: Sappenfield, Christopher C.
• Primary Examiner(s): Wright, Dirk
• Application Number:
  US13/832,575
• Publication Number:
  US 20140066246A1
• Time in Patent Office: 550 Days
• Field of Search: None
• US Class Current: 475/331
• CPC Class Codes: A61C 17/26 driven by electric motor
• CPC Class Codes: F02C 3/04 having a turbine driving a compressor power transmission arrangements F02C7/36; control of working fluid flow F02C9/16
• CPC Class Codes: F02C 7/36 Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user F02C3/107 - F02C3/13 and F02C7/32 take precedence; couplings for transmitting rotation F16D; gearing in general F16H
• CPC Class Codes: F02K 3/065 with front and aft fans
• CPC Class Codes: F02K 3/072 with counter-rotating , e.g. fan rotors
• CPC Class Codes: F16H 1/28 with gears having orbital motion
• CPC Class Codes: F16H 37/0813 with only one input shaft differentials for four wheel drive vehicles B60K17/346

Abstract

The invention relates to rotary units and rotary mechanisms that are suitable for use in numerous applications. Rotary units typically include rotational components that are configured to rotate. In some embodiments, for example, multiple rotary units are assembled in rotary mechanisms such that neighboring pairs of rotational components counter-rotate or contra-rotate relative to one another during operation of the rotary mechanisms. Rotational components generally include one or more implements that are structured to perform or effect one or more types of work as the rotational components rotate relative to one another in a given rotary mechanism. In certain embodiments, implements are configured to rotate and/or to effect the movement of other components as rotational components rotate. In some embodiments, engines include rotary mechanisms and are used in, for example, ground vehicles, marine vehicles, aircraft, or devices.

Claims

1. A rotary mechanism, comprising:

at least first, second, and third rotational components, wherein at least one of the rotational components comprises at least a first implement selected from the group consisting of;

a first propeller, a first impeller, a first fan assembly, a first fan, a first blade, a first compressor, a first booster, a first combustor, a first rotor, a first turbine, a first nozzle, a first duct, a first generator, a first motor, a first gear component, and a first component thereof;

at least first and second counter-rotational mechanisms, wherein the first counter-rotational mechanism operably engages at least the first and second rotational components, and wherein the second counter-rotational mechanism operably engages at least the second and third rotational components; and

,

at least one drive mechanism component or a portion thereof that operably engages one or more of the rotational components and/or one or more of the counter-rotational mechanisms, which drive mechanism component or portion thereof is configured at least to effect rotation of the rotational components and the counter-rotational mechanisms such that the first and third rotational components rotate in a first direction and the second rotational component rotates in a second direction.

2. An engine comprising the rotary mechanism of claim 1.

3. A ground vehicle, a marine vehicle, an aircraft, or a device comprising the rotary mechanism of claim 1.

4. A boat, a ship, canoe, kayak, hydrofoil, submarine, submersible, a hand-held marine propulsion device, a surf board, a wind surfing board, a boogie board, a paddle board, a personal watercraft, a water ski, or a wake board comprising the rotary mechanism of claim 1.

5. The rotary mechanism of claim 1, wherein the first implement rotates at least proximal to at least a second implement selected from the group consisting of:

a second propeller, a second impeller, a second fan assembly, a second fan, a second blade, a second compressor, a second booster, a second combustor, a second rotor, a second turbine, a second nozzle, a second duct, a second generator, a second motor, a second gear component, and a second component thereof.

6. The rotary mechanism of claim 5, wherein the first implement operably engages the second implement.

7. The rotary mechanism of claim 5, wherein at least one other component comprises the second implement.

8. The rotary mechanism of claim 7, wherein the other component comprises at least one propulsion unit.

9. The rotary mechanism of claim 1, comprising at least two rotary units that each comprises:

at least one rotational component that comprises at least one sun gear component and at least one ring gear component, and

at least one gear structure that comprises at least one support component and at least one planetary gear component rotatably coupled to the support component, and wherein the planetary gear component is configured to operably engage the ring gear component,

wherein the sun gear component of at least a first rotary unit operably engages the planetary gear component of at least a second rotary unit such that when the rotational component of the first rotary unit rotates in the first direction, the rotational component of the second rotary unit rotates in the second direction.

10. The rotary mechanism of claim 9, wherein the gear structure of the first rotary unit is operably connected to the gear structure of the second rotary unit such that the support components are substantially fixedly positioned relative to one another at least when the rotational component of the first rotary unit rotates in the first direction, the rotational component of the second rotary unit rotates in the second direction.

11. The rotary mechanism of claim 1, comprising:

at least a first rotary unit that comprises at least one rotational component that comprises at least first and second sun gear components;

at least a second rotary unit that comprises at least one rotational component that comprises at least first and second ring gear components; and

,

at least a first planetary gear component that is configured to operably engage the second sun gear component of the first rotary unit and the first ring gear component of the second rotary unit such that when the rotational component of the first rotary unit rotates in the first direction, the rotational component of the second rotary unit rotates in the second direction.

12. The rotary mechanism of claim 11, comprising at least one gear structure that comprises at least one support component, wherein the first planetary gear component is rotatably coupled to the support component, which support component is substantially fixedly positioned when the rotational component of the first rotary unit rotates in the first direction, the rotational component of the second rotary unit rotates in the second direction.

13. The rotary mechanism of claim 1, comprising at least two rotary units that each comprises:

at least one rotational component that comprises at least one ring gear component; and

,

at least one second gear component configured to operably engage the ring gear component.

14. The rotary mechanism of claim 13, wherein the drive mechanism component or portion thereof comprises at least two shaft components, wherein at least a first shaft component operably engages at least the second gear component of the first rotary unit and at least a second shaft component operably engages at least the second gear component of the second rotary unit.

15. The rotary mechanism of claim 1, comprising:

at least two rotational components that each comprises at least one ring gear component; and

,

at least one counter-rotational mechanism that comprises at least a first gear component that operably engages the ring gear component of at least a first rotational component, at least a second gear component that operably engages the ring gear component of at least a second rotational component, and at least a third gear component that operably engages at least the second gear component such that when the first gear component rotates in the first direction, the first rotational component rotates in the first direction and the second gear component and the second rotational component rotate in the second direction.

16. The rotary mechanism of claim 15, wherein the drive mechanism component or portion thereof operably engages at least the first gear component, which drive mechanism component or portion thereof is configured to effect rotation of at least the first gear component.

17. The rotary mechanism of claim 1, comprising:

at least a first rotary unit that comprises at least one rotational component that comprises at least two ring gear components;

at least a second rotary unit that comprises at least one rotational component that comprises at least two ring gear components; and

,

at least a first planetary gear component that is configured to operably engage at least one of the ring gear components of the first rotary unit and at least one of the ring gear components of the second rotary unit such that when the rotational component of the first rotary unit rotates in the first direction, the rotational component of the second rotary unit rotates in the second direction.

18. The rotary mechanism of claim 17, comprising at least one gear structure that comprises at least one support component, wherein the first planetary gear component is rotatably coupled to the support component, which support component is substantially fixedly positioned when the rotational component of the first rotary unit rotates in the first direction, the rotational component of the second rotary unit rotates in the second direction.

19. A rotary mechanism, comprising

at least first and second rotational components and at least a first counter-rotational mechanism that operably engages at least the first and second rotational components, wherein the first and second rotational components are configured to rotate substantially non-concentrically relative to one another at least partially around a rotational axis, and wherein at least one surface of the first and/or second rotational component comprises at least a first implement selected from the group consisting of:

a first propeller, a first impeller, a first fan assembly, a first fan, a first blade, a first compressor, a first booster, a first combustor, a first rotor, a first turbine, a first nozzle, a first duct, a first generator, a first motor, a first gear component, and a first component thereof; and

,

at least one drive mechanism component or portion thereof that operably engages one or more of the rotational components and/or the first counter-rotational mechanism such that when the first rotational component rotates in a first direction, the second rotational component rotates in a second direction, and the first implement rotates at least proximal to at least a second implement selected from the group consisting of;

a second propeller, a second impeller, a second fan assembly, a second fan, a second blade, a second compressor, a second booster, a second combustor, a second rotor, a second turbine, a second nozzle, a second duct, a second generator, a second motor, a second gear component, and a second component thereof.

20. An engine, comprising:

at least one rotary mechanism that comprises at least first and second rotational components and at least a first counter-rotational mechanism that operably engages at least the first and second rotational components, wherein the first and second rotational components are configured to rotate substantially non-concentrically relative to one another around a first rotational axis, and wherein the first and/or second rotational component comprises at least a first gear component;

at least one propulsion mechanism that comprises at least a first propulsion unit that is configured to rotate around a second rotational axis, wherein the first propulsion unit comprises at least a second gear component that operably engages the first gear component, and wherein the first propulsion unit comprises at least one implement selected from the group consisting of;

a propeller, an impeller, a fan assembly, a fan, a blade, a compressor, a booster, a combustor, a rotor, a turbine, a nozzle, a duct, a generator, a motor, a gear component, and a component thereof; and

,

at least one drive mechanism component or portion thereof that operably engages one or more of the rotational components, the first counter-rotational mechanism, and/or the propulsion mechanism such that when the first rotational component rotates in a first direction, the second rotational component rotates in a second direction, and the first propulsion unit rotates in the first and/or second direction.