Compressor terminal fault interruption method and apparatus

• US 6,760,207 B2
• Filed: 12/11/2001
• Issued: 07/06/2004
• Est. Priority Date: 12/12/2000
• Status: Expired due to Term

• Current Assignee: Tecumseh Products Company
• Original Assignee: Tecumseh Products Company
• Inventors: Alvey, Alex, Wyatt, Arnold G.
• Primary Examiner(s): Jackson, Stephen W.
• Assistant Examiner(s): DEMAKIS, JAMES A
• Application Number:
  US10/014,692
• Publication Number:
  US 20020106945A1
• Time in Patent Office: 938 Days
• Field of Search: 361/30, 361/31, 361/33, 361/93.5, 361/93.6, 361/93.7, 361/93.9, 361/95, 361/96, 361/93.1, 361/22
• US Class Current: 361/93.1
• CPC Class Codes: F04B 2203/0201 Current
• CPC Class Codes: F04B 2203/0205 Temperature
• CPC Class Codes: F04B 2203/0212 Amplitude of the electric current
• CPC Class Codes: F04B 49/065 and making use of computers
• CPC Class Codes: H02H 3/08 responsive to excess current responsive to abnormal temperature caused by excess current H02H5/04
• CPC Class Codes: H02H 7/08 for dynamo-electric motors

Abstract

A compressor terminal fault interruption method and interrupter for disconnecting power to a compressor terminal when terminal venting failure is imminent including a current sensing circuit for sensing current provided to the terminal by a power source and outputting a sensed signal representing the current provided to the terminal and a control circuit. The control circuit includes a first circuit for outputting a reference signal representing input current much higher than locked rotor current, a second circuit connected to the current sensing circuit and the first circuit for comparing the sensed signal to the reference signal, and a third circuit connected to the second circuit for disconnecting power to the terminal when the sensed signal exceeds the reference signal, thereby preventing excessive current from reaching the compressor terminal.

Claims

1. A method of preventing damage to the terminal of a hermetic compressor having a motor, said method comprising the steps of:

sensing current draw through the terminal;

monitoring a signal representing the sensed current draw;

comparing the monitored signal to a reference signal corresponding to a current draw substantially greater than a current draw associated with a locked rotor condition of the motor; and

rapidly disconnecting power to the terminal when the monitored signal exceeds the reference signal to prevent heating of the compressor terminal to a level likely to cause terminal venting;

wherein the reference signal corresponds to current draw that will subsequently heat the terminal to a level that the differential temperature between a pin and surrounding glass of the terminal exceeds a level where stresses in the glass will cause failure of the pin/glass seal.

2. The method of claim 1 wherein the reference signal corresponds to a current draw greater than twice the current draw associated with a locked rotor condition of the motor.

3. The method of claim 1 wherein the current draw is sensed externally of the compressor.

4. A method of preventing damage to the terminal of a hermetic compressor having a motor, said method comprising the steps of:

sensing power draw through the terminal;

monitoring a signal representing the sensed power draw;

comparing the monitored signal to a reference signal corresponding to a power draw substantially greater than the power draw associated with a locked rotor condition of the motor; and

rapidly disconnecting power to the compressor terminal when the monitored signal exceeds the reference signal to prevent heating of the compressor terminal to a level likely to cause terminal venting;

wherein the reference signal corresponds to power draw that will subsequently heat the terminal to a level that the differential temperature between a pin and surrounding glass of the terminal exceeds a level where stresses in the glass will cause failure of the pin/glass seal.

5. The method of claim 4 wherein the reference signal corresponds to a power draw greater than twice the power draw associated with a locked rotor condition of the motor.

6. The method of claim 4 wherein the power draw is sensed externally of the compressor.