PROPULSION SYSTEM

• US 20160257416A1
• Filed: 09/02/2014
• Published: 09/08/2016
• Est. Priority Date: 09/02/2014
• Status: Abandoned Application

• Current Assignee: Hamilton Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Hamilton Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Himmelmann, Richard A., Perkinson, Robert H., Tongue, Stephen E.
• Application Number:
  US14/475,146
• Publication Number:
  US 20160257416A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: B64D 27/02 Aircraft characterised by the type or position of power plants fuselages specially adapted for mounting power plants B64C1/16; wings specially adapted for power plants B64C3/32
• CPC Class Codes: B64D 27/026 comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine Hybrid electric aircraft B64D27/33
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A propulsion system and related methods are disclosed. A propulsion system may have a propulsor, an energy conversion system, an energy storage system that stores electrical energy, and a turbine. The propulsor may be in electrical communication with the energy conversion system, and the energy conversion system may receive electrical energy from the turbine or the energy storage system and deliver it to the propulsor. In this manner, a vehicle may be propelled by the propulsor even when the turbine is not operating.

Claims

1. A method of operating a propulsion system comprising:

propulsing a vehicle by a propulsor powered by an energy storage system;

depleting energy stored in the energy storage system in response to the propulsing;

pulsing on a turbine whereby energy may be provided to the energy storage system;

replenishing, by the turbine, the energy stored in the energy storage system; and

pulsing off the turbine in response to the replenishing; and

replenishing, by the propulsor, the energy stored in the energy storage system by permitting the propulsor to windmill in response to a turbine failure.

2. The method according to claim 1, wherein the pulsing off comprises retarding a throttle of the turbine to a flight idle position.

3. The method according to claim 1, wherein the pulsing off comprises shutting down the turbine.

4. A propulsion system comprising:

a first propulsor;

a first energy conversion system;

a first energy storage system; and

a first turbine,

wherein the first propulsor is in electrical communication with the first energy conversion system, and wherein the first energy conversion system receives an energy storage system electrical energy from the first energy storage system and provides a conditioned energy storage system electrical energy to at least one of the first propulsor and an emergency system.

5. A propulsion system according to claim 4, wherein the first turbine comprises a gas turbine.

6. The propulsion system according to claim 4, further comprising a second propulsor in electrical communication with the first energy conversion system.

7. The propulsion system according to claim 4, further comprising:

a second propulsor;

a second energy conversion system;

a second energy storage system;

a second turbine; and

an interconnection component comprising electrical wiring between the first propulsor and the first energy conversion system and connecting to between the second propulsor and the second energy conversion system, wherein the second propulsor is in electrical communication with the second energy conversion system, p1 wherein the second energy conversion system receives the energy storage system electrical energy from at least one of;

the second energy storage system and the first energy storage system.

8. The propulsion system according to claim 4, wherein the first propulsor further comprises:

a first propeller;

a first electric motor in mechanical communication with the first propeller; and

a first electric motor controller in electrical communication with the first electric motor,

wherein the first electric motor controller directs the first electric motor to spin the first propeller.

9. The propulsion system according to claim 8, wherein the first propulsor further comprises:

a second propeller;

a second electric motor in mechanical communication with the second propeller; and

a second electric motor controller in electrical communication with the second electric motor,

wherein the second electric motor controller directs the second electric motor to spin the second propeller, and

wherein the first propeller and the second propeller counterrotate.

10. The propulsion system according to claim 4, wherein the first propulsor further comprises:

a first ducted fan;

a first electric motor in mechanical communication with the first ducted fan; and

a first electric motor controller in electrical communication with the first electric motor,

wherein the first electric motor controller directs the first electric motor to spin the first ducted fan.

11. The propulsion system according to claim 4, wherein the first energy storage system comprises:

a battery; and

a DC/DC converter/battery charger, wherein electrical energy is conditioned by the DC/DC converter/battery charger prior to storage in the battery, and wherein electrical energy is conditioned by the DC/DC converter/battery charger prior to delivery from the battery to at least one of the first propulsor and the first energy conversion system.

12. The propulsion system according to claim 11, wherein the battery comprises a lithium ion battery.

13. The propulsion system according to claim 4, wherein the first energy conversion system comprises:

a rectifier/inverter; and

a high-speed electric machine,

wherein the high-speed electric machine at least one of;

receives the energy storage system electrical energy from the rectifier/inverter and mechanically rotates the first turbine, and

receives mechanical energy from the first turbine and generates a high-speed electric machine electrical energy communicated to the rectifier/inverter,

wherein the rectifier/inverter at least one of;

conditions the energy storage system electrical energy and delivers the conditioned energy storage system electrical energy to the high-speed electric machine, and

conditions the high-speed electric machine electrical energy and delivers a conditioned high-speed electric machine electrical energy to the first energy storage system.

14. The propulsion system according to claim 13,

wherein the conditioning the energy storage system electrical energy comprises converting the energy storage system electrical energy from direct current to alternating current, and wherein the conditioning the high-speed electric machine electrical energy comprises converting the high-speed electric machine electrical energy from alternating current to direct current.

15. The propulsion system according to claim 4, further comprising:

a second propulsor; and

an interconnection component comprising electrical wiring disposed between the first propulsor and the second propulsor whereby the first propulsor and the second propulsor are connected in parallel.