Impeller Vane Groove Inclining Angles for Fuel Pump Efficiency

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Solution Overview

Problem

Existing fuel pumps face challenges in enhancing discharge pressure and pump efficiency while minimizing energy consumption, as increasing electricity supply to fuel pumps leads to increased energy consumption and inefficient fuel pressurization.

Innovation Solution

The design of an impeller with radially inclined back surfaces and forward surfaces in vane grooves, where the backward inclining angle α ranges from 15° to 30° and the forward inclining angle β ranges from 60°, optimizing the flow of fuel through the pump passages to enhance pump efficiency without excessive energy consumption.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Stress or pressure

If electricity supply to motor portion is increased to enhance discharge pressure, then discharge pressure is improved, but energy consumption increases

Engineering Contradiction:
Improvedischarge pressureVSAvoidenergy consumption
Core Design Contradiction:
Stress or pressureVSUse of energy by moving object

Solution Approach 1:

The invention changes the geometric parameters of the impeller, specifically the inclining angles of the back surfaces of partition walls (backward inclining angle α and forward inclining angle β). By optimizing these angles within specific ranges (15°≦α≦30°, β≦60°, and 1≦β/α≦4), the pump efficiency is improved, allowing higher discharge pressure to be achieved with the same motor power, thus resolving the contradiction between discharge pressure and energy consumption

Inventive Principle:
Principle #35Parameter changes

2Stress or pressure

If pump efficiency is enhanced to increase discharge pressure, then discharge pressure is improved, but device complexity increases

Engineering Contradiction:
Improvedischarge pressureVSAvoidimpeller structure complexity
Core Design Contradiction:
Stress or pressureVSDevice complexity

Solution Approach 1:

The invention applies local quality by making the back surfaces of partition walls have specific inclining characteristics in certain regions. The radially inner side of each back surface has a backward inclining angle α, while the surface is inclined forwardly from the thickness-center toward thickness-ends with angle β. This localized geometric optimization improves pump efficiency without requiring complex overall impeller redesign

Inventive Principle:
Principle #3Local quality

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This configuration ensures efficient fuel pressurization by maintaining maximum pump efficiency within specified angle ranges, reducing resistance and enhancing the discharge pressure and amount of fuel without increasing energy consumption, thus improving the overall performance of the fuel pump.

Implementation Method 1

At least the radially inner side of the back surface is radially outwardly inclined backwardly with respect to the rotative direction

Methodology Applied
Scientific EffectFluid flow direction control through inclined surface geometry:

Implementation Method 2

The back surface is inclined from the thickness-center toward both the thickness-ends forwardly with respect to the rotative direction

Methodology Applied
Scientific EffectFlow resistance reduction through surface inclination:

Implementation Method 3

The cross section of the flow passage is gradually reduced from the inlet toward the pump passage so as to enhance efficiency of the pump portion

Methodology Applied
Scientific EffectFluid compression through passage cross-section reduction:

Data Source

PatentUS7597543B2Impeller and fluid pump having the same
Publication Date: 2009.10.06 AISAN IND CO LTD
  • US7597543B2 patent drawing
  • US7597543B2 patent drawing
  • US7597543B2 patent drawing

AI summary

An impeller includes vane grooves arranged with respect to the rotative direction. At least the radially inner side of a back surface of each vane groove is radially outwardly inclined backwardly with respect to the rotative direction. The back surface has a radially inner end and a radially outer end, which are connected via a line segment. The line segment and a radius of the impeller define a backward inclining angle α therebetween. The back surface is inclined from a thickness center of the impeller toward each thickness-end of the impeller forwardly with respect to the rotative direction. The thickness-center and the thickness-end are connected via a line segment. The line segment and the thickness-center define a forward inclining angle β therebetween. The angle α, β satisfy the following relationships: 15°≦α≦30°; β≦60°; and 1≦β/α≦4.