Inconel 713 Superalloy Turbine Rotor/Impeller Lost-Wax Casting and Precision CNC Machining for Low-Altitude Flight-System Inquiries
Let’s define your requirement
Send a product link, drawing or short brief. We’ll work through the details with you.
- Confirm the specificationGrade or model, size and intended use.
- Define your orderQuantity, finish or configuration, and samples.
- Agree the quotation scopeIncluded work, key checks and delivery needs.
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Component FormImpeller / RotorSurface FinishSandblasted , Polished
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warranty2 Yearsweight (kg)100
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video outgoing-inspectionProvidedmachinery test reportProvided
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engine typeKerosene, diesel fueltypeTurbocharger,Turbine Wheel
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Product TypePrecision Power & Propulsion Components
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CustomizationInconel 718 / 625 / Titanium Alloy / Stainless SteelProcessInvestment Casting / Lost Wax Casting / CNC Machining / HIP
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ApplicationTurbine Engines / UAV Propulsion Systems / Industrial Power UnitsMax Temperature Resistance≥1000°C (Alloy Dependent)
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Max Rotational Speed30,000-100,000 RPMTolerance±0.01-0.05 mm (Precision Grade)
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Surface TreatmentGrinding / Polishing / Sand Blasting / Coating / Heat TreatmentDrawing Format2D: PDF, DWG, DXF / 3D: STEP, IGS, STP
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PackagingCarton / Plywood Case / Anti-Rust Protection
Lost-wax investment casting and precision CNC machining are offered for turbine rotor and turbine-wheel components. Inconel 713 is part of the rotor scope, with customization choices including Inconel 718, Inconel 625, titanium alloy and stainless steel. HIP is also a processing option, allowing the manufacturing discussion to follow the selected component design.
Alloy choice before thermal duty
Temperature resistance is ≥1000°C with an alloy-dependent qualification. Keep that qualification attached to the selected material and agree the thermal duty for the actual rotor. The Inconel, titanium and stainless choices should be reviewed as separate material decisions, with the required material and acceptance conditions defined for the application.
Rotor speed and dimensional acceptance
The rotational-speed reference is 30,000–100,000 RPM, with a precision-grade tolerance of ±0.01–0.05 mm. Agree how those references apply to the rotor geometry, selected alloy and intended operating duty. Any balancing and inspection requirements should be defined for the component before using the figures as acceptance criteria.
Surface work for the selected alloy
Surface and treatment options include grinding, polishing, sand blasting, coating and heat treatment. Select the required work around the chosen alloy and identify the relevant surfaces on the rotor drawing. A machinery test report is offered, so the required report scope can be agreed alongside the component's inspection acceptance.
Drawings and engine application review
Drawing inputs include 2D PDF, DWG and DXF, plus 3D STEP, IGS and STP. Application inquiries cover turbine engines, UAV propulsion and industrial power units, with kerosene and diesel-fuel engine types identified. For a low-altitude flight-system impeller or rotor project, confirm the exact engine interface, operating envelope and applicable flight-qualification requirements; the manufacturing inquiry should remain tied to that specific design.
