Method and apparatus for preventing pump cavitation

• US 3,981,618 A
• Filed: 02/14/1975
• Issued: 09/21/1976
• Est. Priority Date: 02/14/1975
• Status: Expired due to Term

• Current Assignee: Grumman Aerospace Corporation (Northrop Grumman Corporation)
• Original Assignee: Grumman Aerospace Corporation (Northrop Grumman Corporation)
• Inventors: Nelson, George R. Jr.
• Primary Examiner(s): Freeh, William L.
• Assistant Examiner(s): Look, Edward
• Application Number:
  US05/550,042
• Time in Patent Office: 585 Days
• Field of Search: 417/12, 417/23, 417/34, 417/43, 417/17-20, 417/22-24, 417/26, 417/34, 417/42, 417/12, 169/13, 169/24, 415/27, 415/1, 415/17
• US Class Current: 417/12
• CPC Class Codes: F02B 1/04 with fuel-air mixture admission into cylinder
• CPC Class Codes: F02D 29/04 peculiar to engines driving pumps
• CPC Class Codes: F04B 49/06 Control using electricity regulating by means of floats actuating electric switches F04B49/04
• CPC Class Codes: F04B 49/103 Responsive to speed
• CPC Class Codes: F04B 49/20 by changing the driving speed

Abstract

The speed of an engine driven pump is sensed and compared with the desired maximum operating speed to detect overspeed. The discharge of the pump is controlled by a variable flow rate controller. When an overspeed condition exists, a command signal is sent to the discharge controller to reduce flow by a discrete decrement. The control signal is blocked after activating the controller for a preselected time interval. During the blocking interval the engine speed is maintained substantially at the operating speed by cyclical reduction of the power input thereto.

Claims

1. A method of controlling a system having a pump driven by an engine, said pump having a discharge conduit with a variable flow rate controller to prevent cavitation due to engine overspeed comprising the steps of:

continuously sensing the speed of said engine and comparing the speed to a preselected set point speed;

generating a command signal when said sensed speed exceeds said set point speed;

actuating said flow controller with said command signal to change the flow rate of said discharge conduit by a predetermined decrement;

subsequently blocking said command signal from activating said flow controller for a selected time interval to permit the flow rate to reach steady state, while reducing energy input to the engine to cause said engine speed to drop below said set point speed, whereby said engine speed is maintained substantially at said set point speed to prevent cavitation in the pump.

2. The method of claim 1 wherein said energy reducing step is performed by decreasing the flow of fuel to the engine.

3. The method of claim 1 wherein said energy reducing step is performed by momentarily terminating the ignition of said engine.

4. The method of claim 1 wherein said predetermined time interval is an interval having a duration of from 5 to 10 seconds.

5. The method of claim 4 wherein said duration is 5 seconds.

6. The method of claim 1 further including the step of energizing an alarm when said sensed speed exceeds said set speed.

7. The method of claim 1 further including the step of reducing said engine speed to idle when said discharge flow rate is terminated.

8. Apparatus for controlling a system having a pump driven by an engine, said pump having a discharge conduit with a variable flow rate controller to prevent cavitation due to engine overspeed comprising:

means for sensing the speed of said engine and generating a signal output proportional thereto;

comparator means electrically coupled to said sensing means to derive a signal input therefrom, said comparator means being operative to compare said signal input with a predetermined value corresponding to the maximum operating speed of the engine and generate a command signal when said engine speed exceeds said maximum operating speed;

control means operatively coupled to said variable flow rate controller, said control means being adaptable and arranged to receive said command signal and actuate said controller to change the flow rate in said discharge conduit by a predetermined decrement, said control means including means for interrupting the response thereof, to said command signal for a preselected interval following activation of said controller to permit the flow rate to reach steady state conditions; and

engine control means adapted to derive an input from said command signal and reduce the energy input to the engine to cause said engine speed to drop below said maximum operating speed, whereby said engine speed is maintained substantially at said operating speed to prevent cavitation.

9. Apparatus of Claim 8 wherein said engine is a gasoline internal combustion engine and said engine control means is adapted and arranged to ground the ignition thereof.

10. Apparatus of claim 8 wherein said variable flow rate controller includes a discharge conduit having three parallel flow branches, said branches being arranged to permit flow rates therethrough corresponding to integer multiples of said decrement, each of said branches having a control valve, said control means being operatively coupled to said control valves, whereby said discharge flow rate is reduced in response to overspeed of the engine.