Active gas turbine lubrication system flow control

• US 7,506,724 B2
• Filed: 07/23/2004
• Issued: 03/24/2009
• Est. Priority Date: 07/23/2004
• Status: Expired due to Fees

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Delaloye, Jim E.
• Primary Examiner(s): FENSTERMACHER, DAVID MORGAN
• Application Number:
  US10/897,782
• Publication Number:
  US 20060054406A1
• Time in Patent Office: 1,705 Days
• Field of Search: 184/6.1, 184/6.2, 184/6.4, 137/38, 60/360.8
• US Class Current: 184/6.2
• CPC Class Codes: F01D 25/18 Lubricating arrangements of machines or engines in general F01M
• CPC Class Codes: F01D 25/20 using lubrication pumps
• CPC Class Codes: Y10T 137/0753 Control by change of position or inertia of system

Abstract

A lubrication system is provided for an aircraft turbine machine, the lubrication system being controlled by a closed-loop logic arrangement, wherein the oil pressure of a lubricant circulated therein is monitored and altered according to attitude data, acceleration data, operating mode data, or some combination thereof contained in a signal received from an airframe flight controller and according to a oil pressure signal and an oil temperature signal. The logic responsively provides a supply pump speed control signal, according to a predetermined target oil pressure value selected to correspond to the data contained in the signals. The target value may be continuously compared to the present oil pressure value and the present oil pressure adjusted by sending a motor control signal to the supply pump and a valve flow control signal to a flow control valve that conditionally allows oil from the outlet side of the supply pump to be fed back to its inlet side.

Claims

1. A control system for a lubrication circuit of a turbine machine, the lubrication circuit having a supply pump and a scavenging pump jointly operated by a shaft of an electric motor for circulation of a lubricant through the lubrication circuit, the supply pump responsive to a motor control signal, the lubrication circuit providing an pressure signal representing the pressure of the lubricant, the control system comprising:

a control device receiving the pressure signal from the lubrication circuit, the control device also receiving a maneuver signal, the control device providing to the lubrication circuit a motor control signal; and

a control module residing in a digital memory of the control device, the control module operatively responsive to both the pressure signal and the maneuver signal in order to provide the motor control signal to vary the speed of the electric motor.

2. The control system described in claim 1, wherein:

the lubrication circuit additionally comprises a flow control valve responsive to a valve control signal for selectively controlling a flow of lubricant through a feedback path between an outlet side of the supply pump to an inlet side of the supply pump; and

the control module further providing the valve control signal that is also responsive to the pressure signal and the attitude signal.

3. The control system described in claim 1, wherein:

the lubrication circuit additionally provides a temperature signal representing the temperature of the lubricant; and

the control module operatively responsive to the pressure signal, the temperature signal, and the maneuver signal in order to provide the motor control signal to vary the speed of the electric motor.

4. The control system described in claim 3, wherein:

the lubrication circuit additionally comprises a flow control valve responsive to a valve control signal for selectively controlling a flow of lubricant through a feedback path between an outlet side of the supply pump to an inlet side of the supply pump; and

the control module further providing the valve control signal that is also responsive to the pressure signal, the temperature signal, and the maneuver signal.

5. The control system described in claim 1, wherein the lubricant is oil.

6. The control system described in claim 1, wherein the maneuver signal contains data selected from the group consisting of attitude data and acceleration data.