IP Library Granted Patent US 7,096,724
Granted Patent B2
US 7,096,724 · App. 10/813,220 · Granted Aug 29, 2006

Fuel injector testing system

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Quick Facts
Patent No.
US 7,096,724
App. No.
10/813,220
Granted
Aug 29, 2006
Kind
B2
Abstract

A fuel injector testing system has a sleeve that mechanically isolates one or more test volumes in a fuel injector. The sleeve has interfaces on an inside surface. The interfaces sealably engage the O-rings on the fuel injector. An air displacement mechanism is connected to the sleeve. The air displacement mechanism adds or removes air from the test volumes. The pressure within each test volume is checked to determine whether there is any air leakage from the test volume.

Claims (42)

1. A method for testing a fuel injectors, comprising the steps of:

mechanically isolating at least one test volume of the fuel injector that is disposed within a sleeve;

changing the amount of air in the at least one test volume;

testing the at least one test volume for air leakage;

removing the fuel injector from the sleeve;

inserting a test plug in the sleeve;

mechanically isolating at least one check volume of the test plug with the sleeve;

changing the amount of air in the at least one check volume; and

testing the at least one check volume for air leakage.

2. The method for testing a fuel injector of claim 1 , further comprising the step of sealably engaging at least two O-rings on the fuel injector with at least two interfaces on the sleeve.

3. The method for testing a fuel injector of claim 1 , further comprising the step of sealably engaging at feast two O-rings on the test plug with at least two interfaces on the sleeve.

4. The method for testing a fuel injector of claim 1 , where the fuel injector is a hydraulically activated electronically controlled unit injection (HEUI) fuel injector.

5. The method for testing a fuel injector of claim 1 , further comprising the steps of:

adding air to the at least one test volume until the at least one test volume reaches a selected pressure level; and

after a time period, determining whether the at least one test volume has a pressure less than a tolerance below the selected pressure level.

6. The method for testing a fuel injector of claim 5 , wherein the selected pressure level is in the range of about 31 inches Hg (787 torr) through about 35 inches Hg (889 Torr); wherein the time period is in the range of about 5 minutes through about 7 minutes; and wherein the tolerance is in the range of about 0 through about 0.5 inches of Hg (11 Torr).

7. The method for testing a fuel Injector of claim 1 , further comprising the steps of:

removing air from the at least one test volume until the at least one test volume reaches a selected vacuum level; and

after a time period, determining whether the at least one test volume has a pressure more than a tolerance above the selected vacuum level.

8. The method for testing a fuel injector of claim 7 , wherein the selected vacuum level is in the range of about 25 inches Hg (635 Torr) through about 29 inches Hg (737 Torr), wherein the time period is in the range of about 5 minutes through about 7 minutes, and wherein the tolerance is in the range of about 0 through about 0.5 inches of Hg (11 Torr).

9. The method for testing a fuel injector of claim 1 , further comprising the steps of:

adding air to the at least one check volume until the at least one check volume reaches a selected pressure level; and

after a time period, determining whether the at least one check volume has a pressure less than a tolerance below the selected pressure level.

10. The method for testing a fuel injector of claim 9 , wherein the selected pressure level is in the range of about 31 Inches Hg (787 Torr) through about 35 inches Hg (889 Torr); wherein the time period is in the range of about 5 minutes through about 7 minutes; and wherein the tolerance is in the range of about 0 through about 0.5 inches of Hg (11 Torr).

11. The method for testing a fuel injector of claim 1 , further comprising the steps of:

removing air from the at least one check volume until the at least one check volume reaches a selected vacuum level; and

after a time period, determining whether the at least one check volume has a pressure less than a tolerance below the selected vacuum level.

12. The method for testing a fuel injector of claim 11 , wherein the selected vacuum level is in the range of about 25 inches Hg (635 Torr) through about 29 inches Hg (737 Torr), wherein the time period is in the range of about 5 minutes through about 7 minutes, and wherein the tolerance is in the range of about 0 through about 0.5 inches of Hg (11 Torr).

13. A method for testing a fuel injector, comprising the steps of:

mechanically isolating at least one test volume of a fuel injector that is disposed in within a sleeve having an inside surface;

changing an amount of air in the at least one test volume by using an air displacement mechanism connected to the test volume through a tube; and

testing the at least one test volume for air leakage;

removing the fuel injector from the sleeve;

inserting a test plug in the sleeve;

mechanically isolating at least one check volume of the test plug with the sleeve;

changing the amount of air in the at least one check volume by using the air displacement mechanism connected to the check volume through the tube; and testing the at least one check volume for air leakage.

14. The method for testing a fuel injector of claim 13 , wherein the step of changing an amount of air in the at least one test volume includes:

connecting an air passage to the tube;

connecting an air pump to the air passage;

attaching a pressure gauge to the air passage;

connecting a valve to the air passage, the valve disposed between the air pump and the pressure gauge;

operating the air pump.

Assignments (4)
RELEASE OF SECURITY INTEREST Recorded Nov 10, 2017
From: JPMORGAN CHASE BANK, N.A., AS COLLATERAL AGENT
To: INTERNATIONAL ENGINE INTELLECTUAL PROPERTY COMPANY, LLC; INTERNATIONAL TRUCK INTELLECTUAL PROPERTY COMPANY, LLC; NAVISTAR, INC.; NAVISTAR INTERNATIONAL CORPORATION
Reel/Frame 044416/0867 →
SECURITY AGREEMENT Recorded Sep 12, 2012
From: INTERNATIONAL ENGINE INTELLECTUAL PROPERTY COMPANY, LLC; INTERNATIONAL TRUCK INTELLECTUAL PROPERTY COMPANY, LLC; NAVISTAR INTERNATIONAL CORPORATION; NAVISTAR, INC.
To: JPMORGAN CHASE BANK, N.A., AS COLLATERAL AGENT
Reel/Frame 028944/0730 →
CORRECTION TO THE ASSIGNEE Recorded Jun 24, 2004
From: WILDMAN, MARK A.
To: INTERNATIONAL ENGINE INTELLECTUAL PROPERTY COMPANY, L.L.C.
Reel/Frame 014774/0842 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 22, 2004
From: WILDMAN, MARK ALAN
To: INTERNATIONAL TRUCK INTELLECTUAL PROPERTY COMPANY, LLC
Reel/Frame 014760/0538 →