Application of Rapid Prototyping Technology in Impeller Prototype Fabrication

Contents

With increasing design iteration speed and verification efficiency of complex impeller components in high-tech industries such as aviation, energy, and automotive, traditional processing technologies have increasingly demonstrated disadvantages such as high price, long cycle, and slow response during the process of prototype development. Rapid prototyping technology, which possesses features of digital driving, mold-free manufacturing, and high geometric freedom, has become the core of new-generation prototype design.

Introduction

Impeller as a core component of fluid machinery is an essential part in equipment such as aero-engines, gas turbines, hydraulic pumps, and compressors. Because of its complex free-form surface geometrical structure, high strength requirements, and properties of high-speed rotation, production of prototypes should have both geometric accuracy and regard the usability of material performance as well as hydrodynamic testing. While traditional and mature CNC machining and casting are available, there are serious bottlenecks in multi-round design verification, functional testing, and iteration speed. Especially in the high-end manufacturing sector, response and cycle speed between design and verification directly affect system development progression.

Since its introduction during the 1980s, rapid prototyping technology has progressed step by step from concept verification to a leading process path for producing functional structural parts. CAD-driven, it makes use of the discrete layering and build-up of the material to generate three-dimensional objects directly, significantly cutting down on processing routes and machine requirements, and becoming a versatile tool for today’s complex part prototype manufacturing.

Overview of Rapid Prototyping Technology

Rapid prototyping technology is based on the “material accumulation” manufacturing principle rather than “material removal”. By slicing the three-dimensional object from CAD modeling and converting it into a series of two-dimensional cross-sectional data, materials are added successively as per this hierarchical data to create the actual component. This may be done by physical melting, laser curing, material sintering, etc., completely avoiding traditional mold dependency.

Along with the development of control systems, materials science, and laser technology, rapid prototyping has evolved from the initial visual display model to structural part production, functional part production, and even finished part production. Its typical technologies are basically:

  • Stereolithography (SLA): Lases curing photosensitive resin liquid, high precision, suitable for micro-structure display and transparent model making.
  • Selective Laser Melting (SLM): Merges metal powder to create dense metal pieces, used extensively for functional testing and temporary service.
  • Selective Laser Sintering (SLS): Sintering and forming metal, ceramic, and polymer powders, best suited for rapid mold creation.
  • Fused Deposition Modeling (FDM): Cost-effective thermoplastic material extrusion technology, best used for structural confirmation, training simulation, and rapid prototyping.
  • Laminated Object Manufacturing (LOM): Employed glued film layer-by-layer cutting and sticking, high velocity but relatively low strength, a suitable technique for prototype manufacturing of large size.

Application of Rapid Prototyping Technology in Impeller Prototype Fabrication

3.1 Design Verification and Geometric Evaluation

In the early phase of new impeller structure design, multiple rounds of inspection are required for blade layout, curvature change, and inlet/outlet. Quickly printed plastic or resin models by FDM or SLA technology not only can be used for visual inspection and assembly confirmation, but also can be used to measure important parameters such as blade gap and flow channel integrity by means of a coordinate measuring system. especially in examination of the complex internal geometry of compressor and turbine impellers, SLA models can indeed demonstrate nanometer-scale geometric details due to their high surface finish and resolution, providing realistic references for design optimization.

3.2 Flow Visualization and Wind Tunnel Testing

Transparent or transparent RP models can be combined with technologies such as LDV (Laser Doppler Velocimetry) and PIV (Particle Image Velocimetry) to visually see the flow path, vortex structure, and pressure distribution, which are commonly used for aerodynamic validation of key areas such as impeller flow channels and outlet guide vanes. Unlike traditional metal parts, polymer models not only have short manufacturing cycles and low costs but are also of high optical quality and surface uniformity, favoring precision acquisition of experimental data.

3.3 Functional Metal Impeller Prototypes

The direct fabrication of metal prototypes (such as Inconel 718, titanium alloy, etc.) by SLM technology can realize dynamic performance testing at high temperature and pressure. Through adjustable laser power, scanning path planning, and powder particle size, high density complicated blade structures could be fabricated. SLM has also been widely used for manufacturing aero-engine trial parts, especially in guaranteeing the critical performances such as vibration resistance of thin-walled structures and thermal management of blade tip turbulent flow channels.

3.4 Hybrid Manufacturing Path Integrated with Traditional Manufacturing

RP is commonly paired with CNC subtractive machining in the manufacture of high-precision impeller prototypes. For example, after SLM produces the general structure of the impeller, the five-axis machine tool is utilized to process the important locations such as the center hole of the hub and the shaft shoulder match surface, which can meet the rapid manufacturing efficiency and local high precision requirements. This type of “hybrid path of additive and subtractive manufacturing” has proved to be an excellent paradigm for producing complex aviation impellers.

Process Case Analysis

In a research institute on aviation, SLM produced a high-load compressor impeller prototype. Its maximum size has a diameter of only 180 mm, and the thinnest thickness of the blade is only 1.5 mm. The entire cycle of manufacture was shortened from 6 weeks of normal milling and welding to 10 days. Through afterwards laser drilling and hot isostatic pressing treatment, the dynamic balancing and modal test were finally completed, and the mechanical stability of the complicated structure was successfully verified.

Another wind power enterprise printed a full-scale model of a water turbine through SLA technology, optimized the internal flow pattern together with PIV experiments, and significantly improved the model test efficiency and blade design confidence. During the subsequent mass production process, the SLA model was utilized to create precision casting shells, which realized a full-scale smooth transition from the prototype to the trial parts.

Advantages and Challenges

Advantages:

  • Significantly shorten the cycle of producing impeller prototypes and support quick iteration and simultaneous verification of different schemes;
  • Extreme complex structures can be directly forged mould-free and complicated programming;
  • Can be applied to multiple links such as flow visualization, assembly inspection, and functional testing;
  • Highly compatible with traditional manufacturing, facilitating the construction of flexible development processes.

Challenges:

  • Raw material flexibility is still limited, and some performance under some states of engineering cannot be met;
  • Accuracy of forming and roughness of the surface still need secondary processing to be improved;;
  • Manufacturing metal powder RP is expensive, and equipment usage is enormous, so promotion is limited by the scale of investment;
  • Process parameters are advanced, and process control needs to be supported by advanced level engineering expertise.

Conclusion

Rapid prototyping technology is increasingly becoming the key connector in the impeller product research and development process. It has proved to be extremely effective in a number of phases such as shape verification, performance testing, functional tests, and small-batch delivery. In the future, spurred by the relentless advancement of new material systems (e.g., high-temperature ceramic matrix composites), smart control technologies, and large-size additive machines, rapid prototyping will become even closer to final part manufacturing, promoting the full transformation of impellers from “digital design” to “digital manufacturing”.

Especially for high-end equipment such as aero-engines, an intelligent rapid prototyping system with simulation feedback and manufacturing closed-loop control is utilized to complete the whole process digital manufacturing of “what you see is what you get” and offers the basis for quick and high-quality development of complex structure impellers.

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