Mechanical disconnects for parallel power lanes in hybrid electric propulsion systems

Patent metadata

Field	Value
Publication number	US-11732639-B2
Application number	US-201916707587-A
Country	US
Kind code	B2
Filing date	Dec 9, 2019
Priority date	Mar 1, 2019
Publication date	Aug 22, 2023
Grant date	Aug 22, 2023

Abstract

A hybrid propulsion system includes a heat engine configured to drive a heat engine shaft. An electric motor is configured to drive a motor shaft. A transmission system includes at least one gear box. The transmission system is configured to receive rotational input power from each of the heat engine shaft and the motor shaft and to convert the rotation input power to output power. The motor shaft includes a disconnect mechanism to allow the heat engine to rotate with the electric motor stopped. The heat engine shaft includes a disconnect mechanism to allow the electric motor to rotate with the heat engine stopped.

First claim

What is claimed is:

1. A hybrid propulsion system comprising:
a heat engine configured to drive a heat engine shaft;
an electric motor configured to drive a motor shaft; and
a transmission system including at least one gear box, wherein the transmission system is configured to receive rotational input power from each of the heat engine shaft and the motor shaft and to convert the rotational input power to output power, wherein the heat engine shaft includes a first disconnect mechanism between the heat engine and the electric motor to allow the electric motor to rotate with the heat engine stopped and the electric motor shaft includes a second disconnect mechanism between the electric motor and a first gearbox of the at least one gearbox to allow the heat engine to rotate with the electric motor stopped,
wherein the heat engine shaft and the motor shaft are concentric, wherein the first gear box includes a reduction gear box connected to each of the heat engine shaft and the motor shaft, and wherein the heat engine shaft connects to a turbine shaft for driving a turbine and compressor operatively connected on an opposite side of the heat engine from the second disconnect mechanism and the first gearbox, wherein the heat engine shaft runs through the motor shaft and through the second disconnect mechanism of the motor shaft.

2. A hybrid propulsion system comprising:
a heat engine configured to drive a heat engine shaft;
an electric motor configured to drive a motor shaft; and
a transmission system including at least one gear box, wherein the transmission system is configured to receive rotational input power from each of the heat engine shaft and the motor shaft and to convert the rotational input power to output power, wherein the heat engine shaft and the motor shaft are combined as a single common shaft connected to the transmission system, wherein the electric motor includes a first disconnect mechanism within the electric motor to allow the heat engine to rotate with the electric motor stopped and wherein the single common shaft includes a second disconnect mechanism between the electric motor and the heat engine to allow the electric motor to rotate with the heat engine stopped.

3. The system as recited in claim 2 , wherein the at least one gear box includes a reduction gear box connected to the single common shaft.

Assignees

• Pratt & Whitney Canada

Inventors

• Latulipe Eric
• Thomassin Jean
• Spierling Todd A
• Bayles Robert A

Classifications

• B64D35/024 Primary

  of series type · CPC title

• B64D35/025

  of parallel type · CPC title

• B64D27/10 Primary

  of gas-turbine type  (jet aircraft B64D27/16) · CPC title

• B64D27/351

  using energy recovery · CPC title

• B64D35/023

  of series-parallel type · CPC title