Enhanced motor cooling system and method

Patent metadata

Field	Value
Publication number	US-11959499-B2
Application number	US-202117494207-A
Country	US
Kind code	B2
Filing date	Oct 5, 2021
Priority date	Jun 28, 2013
Publication date	Apr 16, 2024
Grant date	Apr 16, 2024

Abstract

An Environmental Control System (ECS) for an aircraft includes a ram air system having a ram inlet and a ram outlet. The ECS includes a cabin air compressor motor, a diverter valve, and a dedicated outlet. The cabin air compressor motor has a motor inlet passage and a motor outlet passage with the motor inlet passage being coupled to the ram inlet. The diverter valve includes a first diverter inlet, a first diverter outlet, and a second diverter outlet. The first diverter inlet is coupled to the motor outlet passage. The dedicated outlet is connected to the first diverter outlet in a flight mode of operation of the aircraft and the ram outlet is connected to the second diverter outlet in a ground mode of operation of the aircraft.

First claim

The invention claimed is:

1. A diverter valve for use in a system comprising a ram air system including a ram inlet and a ram outlet and a ram fan that draws air from the ram inlet to the ram outlet, a cabin air compressor motor including a motor cooling inlet passage and a motor cooling outlet passage, said motor inlet cooling passage being coupled to said ram inlet and a dedicated exhaust separate from the ram outlet, the valve comprising:
a valve body including a first diverter inlet, a first diverter outlet and a second diverter outlet;
wherein the first diverter inlet is configured for connection to the motor cooling outlet passage, the first diverter outlet is along a first axis configured for connection to the dedicated exhaust and the second diverter outlet aligned along a second axis that is orthogonal to said first axis and is configured for connection to the ram outlet;
a rotary actuator mechanically connected to said valve body; and
a flapper pivotally mounted within said valve body such that said flapper is movable by said rotary actuator in response to a flight mode of operation or a ground mode of operation;
wherein in the flight mode of operation the rotary actuator causes the flapper to cause air entering the first diverter inlet to exit the diverter valve through the first diverter outlet into the dedicated exhaust separate from the ram outlet; and wherein in the ground mode of operation the rotary actuator causes the flapper to cause air entering the first diverter inlet to exit the diverter valve through the second diverter outlet into the ram outlet.

2. The diverter valve of claim 1 , wherein the flapper further comprises a sealing edge on an outer periphery of said flapper.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Army Donald E
• Mccord Patrick
• Sautron Dominique P
• Zywiak Thomas M

Classifications

• F04F5/14 Primary

  the inducing fluid being elastic fluid · CPC title

• B60K11/06

  with air cooling · CPC title

• B64D13/06 Primary

  the air being conditioned (pressurising B64D13/02) · CPC title

• F04F5/18

  for compressing · CPC title

• F04F7/00

  Pumps displacing fluids by using inertia thereof, e.g. by generating vibrations therein · CPC title