Fuel Flow Testing Apparatus with Bypass Valve for Returnless Systems

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Solution Overview

Problem

Testing fuel flow in returnless fuel systems is challenging due to low flow rates, leading to potential misdiagnosis and unnecessary replacement of costly components, as existing methods struggle to accurately measure both flow rate and pressure.

Innovation Solution

A testing apparatus with a housing, primary flow passage, and bypass passage, equipped with devices for measuring flow rate and pressure, and a movable bypass valve to accommodate both return and returnless systems, allowing for accurate testing by adjusting the flow path.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of energy

If a returnless fuel system is used to improve fuel efficiency and reduce evaporation, then fuel economy and environmental performance are improved, but accurate measurement of fuel flow rate becomes difficult leading to potential misdiagnosis

Engineering Contradiction:
Improvefuel evaporation lossVSAvoidfuel flow rate measurement
Core Design Contradiction:
Loss of energyVSMeasurement precision

Solution Approach 1:

The patent introduces a test pump as an intermediary device that can temporarily assume the role of the fuel pump during testing. This test pump, equipped with flow meters and pressure gauges, serves as a mediator between the fuel system components and the measurement devices, enabling accurate measurement of fuel flow rate and pressure in returnless systems without requiring modification of the actual fuel delivery system.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The patent creates a simplified copy or model of the fuel system for testing purposes. By using a test pump that replicates the fuel pump's function but with integrated measurement capabilities, the system allows accurate measurement of flow rate and pressure without interfering with the actual fuel delivery to the engine. This copying approach enables diagnostic testing while maintaining the integrity of the returnless system architecture.

Inventive Principle:
Principle #26Copying

2Measurement precision

If a standard return fuel system is used to simplify testing, then measurement of fuel flow and pressure becomes easier, but fuel temperature rises and evaporation increases

Engineering Contradiction:
Improvefuel flow and pressure measurementVSAvoidfuel evaporation
Core Design Contradiction:
Measurement precisionVSObject-generated harmful factors

Solution Approach 1:

The patent employs a dynamically adjustable test pump that can modify its operation based on testing requirements. The pump can vary flow rates and pressure levels during different measurement phases, allowing the system to adapt to different testing scenarios. This dynamic capability enables accurate measurement while maintaining fuel temperature within acceptable ranges, reducing evaporation losses compared to static return systems.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The patent utilizes parameter changes in the test pump operation to optimize measurement conditions. By adjusting flow rates, pressure levels, and test durations as parameters, the system can achieve accurate measurements of fuel flow and pressure while controlling fuel temperature. This parameter optimization reduces evaporation losses while maintaining measurement precision, resolving the contradiction between ease of measurement and environmental impact.

Inventive Principle:
Principle #35Parameter changes

3Productivity

If fuel flow rate is reduced to match engine needs in returnless systems, then fuel efficiency improves, but measurement accuracy of flow rate becomes insufficient for reliable diagnosis

Engineering Contradiction:
Improvefuel efficiencyVSAvoidfuel flow rate measurement accuracy
Core Design Contradiction:
ProductivityVSMeasurement precision

Solution Approach 1:

The patent segments the fuel system into distinct testable components by introducing a test pump with integrated measurement devices. This segmentation allows independent measurement of flow rate and pressure at specific points in the system, enabling accurate diagnosis even at low flow rates typical of returnless systems. The segmented approach with dedicated measurement points ensures that fuel efficiency improvements do not compromise measurement accuracy.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent replaces traditional mechanical flow measurement methods with electronic sensing and data processing systems integrated into the test pump. This substitution enables more precise measurement of low flow rates through electronic sensors that can detect and quantify fuel flow accurately even at the low rates required for returnless system operation. The electronic measurement system maintains measurement precision while supporting fuel efficiency improvements.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Data Source

PatentUS7228729B1Apparatus and method for testing fuel flow
Publication Date: 2007.06.12 LINCOLN INDUSTRIES CORP
  • US7228729B1 patent drawing
  • US7228729B1 patent drawing
  • US7228729B1 patent drawing

AI summary

Apparatus for testing fuel flow in a return or returnless fuel system. The apparatus comprises a housing, a primary flow passage in the housing having an inlet for connection to the fuel system for receiving fuel pumped by the fuel pump, and an outlet adapted for connection to the fuel system for flow of fuel to one or more fuel injectors. The apparatus includes a first device for measuring a rate of fuel flow through the primary flow passage, and a second device for measuring a fuel pressure in the primary flow passage. A bypass valve in the primary flow passage is movable between a first position in which the bypass passage is closed and the primary flow passage is open to permit the flow of fuel to the outlet of the primary flow passage and a second position in which the bypass passage is open and the primary flow passage is closed whereby fuel is directed through a bypass passage for transfer to a fuel receptacle. The bypass valve is movable to its first position for testing fuel flow in a return flow system and to its second position for testing fuel flow in a returnless fuel flow system.