Propeller Pump Blade Trimming for Precise Duty Point Matching

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Solution Overview

Problem

Conventional propeller pumps face challenges in accurately adjusting the pitch angle of adjustable blades during assembly, leading to inefficiencies and increased lead time, while fixed-blade propellers require numerous configurations to cover various applications, resulting in compromises on duty points and efficiency.

Innovation Solution

A method for manufacturing propellers with fixed blades that involves axial trimming to adapt to specific applications, allowing for precise adjustment of the duty point without changing the radial dimensions, thus reducing the number of required propeller configurations and simplifying the assembly process.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If adjustable blades are used to adapt to different applications, then the duty point can be precisely adjusted, but the assembly process becomes complicated and lead time increases

Engineering Contradiction:
Improveduty point adjustmentVSAvoidassembly lead time
Core Design Contradiction:
Adaptability or versatilityVSLoss of time

Solution Approach 1:

The blade pitch angles are pre-calculated and pre-marked on the blade surfaces during manufacturing. This preliminary action eliminates the need for complex iterative adjustment during assembly, as installers only need to align the blade with the marked angular positions corresponding to the desired duty point, significantly reducing assembly lead time while maintaining adaptability.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The adjustable blade mechanism is segmented into discrete angular positions with corresponding duty point markings. Each blade can be independently positioned at specific angular increments, allowing precise duty point selection without requiring continuous adjustment, thereby simplifying the assembly process while preserving adaptability across different applications.

Inventive Principle:
Principle #1Segmentation

2Loss of time

If fixed blades are used to reduce assembly complexity, then lead time decreases, but numerous propeller configurations are required to cover different applications

Engineering Contradiction:
Improveassembly lead timeVSAvoidnumber of propeller configurations
Core Design Contradiction:
Loss of timeVSDevice complexity

Solution Approach 1:

A single propeller design with fixed blades incorporates multiple universal angular position markings that can accommodate various duty points. The blade geometry and marking system are designed to be multi-functional, allowing the same propeller configuration to serve different applications by selecting appropriate angular positions, thereby reducing the need for multiple specialized propeller designs.

Inventive Principle:
Principle #6Universality (Multi-functionality)

Solution Approach 2:

The invention changes the parameter approach from varying blade geometry across multiple propeller designs to varying the angular position parameter of fixed blades. By maintaining consistent blade geometry and introducing angular position markings, the system achieves adaptability through parameter variation rather than structural changes, reducing the number of required configurations.

Inventive Principle:
Principle #35Parameter changes

3Ease of manufacture

If fixed blades with limited configurations are used, then manufacturing is simplified, but compromises must be made on duty point precision

Engineering Contradiction:
Improvepropeller manufacturingVSAvoidduty point accuracy
Core Design Contradiction:
Ease of manufactureVSManufacturing precision

Solution Approach 1:

During the manufacturing process, precise angular markings are pre-applied to the blade surfaces indicating the optimal angular positions for achieving specific duty points. This preliminary action ensures manufacturing precision is maintained, as the markings guide both the manufacturing tolerance and the final installation positioning, eliminating the need for post-assembly adjustments while keeping manufacturing processes simple.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS12025145B2Method for manufacturing a propeller for a propeller pump, and propeller for a propeller pump
Publication Date: 2024.07.02 SULZER MANAGEMENT AG
  • US12025145B2 patent drawing
  • US12025145B2 patent drawing
  • US12025145B2 patent drawing

AI summary

A method for manufacturing a propeller for a propeller pump includes providing a base propeller including a hub extending from an axial end in the axial direction, and a plurality of blades fixedly connected to the hub, each blade including a pressure side, a suction side, a leading edge, an initial trailing edge, and a blade tip extending from the leading edge to the initial trailing edge at the end of the blade facing away from the hub, trimming each of the blades of the base propeller the axial direction, and forming a modified trailing edge bye removing a part of the initial trailing edge along the entire pressure side from the hub to the blade tip.