Enhance motor cooling system and method

Patent metadata

Field	Value
Publication number	US-10184494-B2
Application number	US-201313930549-A
Country	US
Kind code	B2
Filing date	Jun 28, 2013
Priority date	Jun 28, 2013
Publication date	Jan 22, 2019
Grant date	Jan 22, 2019

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. An Environmental Control System (ECS) for an aircraft, 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;
a diverter valve including a first diverter inlet, a first diverter outlet, and a second diverter outlet, said first diverter inlet being coupled to said motor cooling outlet passage and the second diverter outlet being connected to the ram outlet; and
a dedicated exhaust separate from the ram outlet coupled to the first diverter outlet;
wherein the diverter valve connects the motor cooling outlet passage to the dedicated exhaust through the first diverter outlet in a flight mode of operation of the aircraft and to said ram outlet through said second diverter outlet in a ground mode of operation of said aircraft.

2. The Environmental Control System of claim 1 , further comprising:
a dedicated outlet passage that connects said first diverter outlet to said dedicated outlet.

3. The Environmental Control System of claim 1 , further comprising:
a second diverter outlet passage that connects said ram outlet to said second diverter outlet.

4. The Environmental Control System of claim 1 , further comprising:
a flight computer electronically connected to said diverter valve that controls operation of the diverter valve.

5. The Environmental Control System of claim 1 , wherein said diverter valve further comprises:
a valve body including a first passage aligned along a first axis and a second passage aligned along a second axis that is orthogonal to said first axis;
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 said flight mode of operation or said ground mode of operation.

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

• B64D2013/0685

  with ozone control · CPC title

• B64D2013/0644

  including electric motors or generators · CPC title

• B64D13/06 Primary

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

• Y02T50/56

  Cross-Sectional Technologies · mapped topic