C-Axis Single-Setup Blade Bore Angular Pitch
All blade bores in an eVTOL propeller hub — 2, 3, 4, 5, or 6 blades — are drilled and reamed in one C-axis indexed MAZAK mill-turn program from one chucking without table repositioning.
Custom CNC Propeller Machining made to your drawing. Review assembly datums, angled features and thin-wall geometry, material, finishing and inspection requirements before production.

eVTOL propeller and rotor hub machining occupies a unique technical position — bridging helicopter rotor head precision and commercial eVTOL volume production requirements.

Coordinate geometry, material, finishing and inspection around the part's intended function.
All blade bores in an eVTOL propeller hub — 2, 3, 4, 5, or 6 blades — are drilled and reamed in one C-axis indexed MAZAK mill-turn program from one chucking without table repositioning.
eVTOL propulsion components have compound-angle blade attachment interfaces, non-orthogonal bearing seat arrangements, and asymmetric structural geometries requiring 5-axis simultaneous machining for all critical features from one datum reference.
Review assembly datums, angled features and thin-wall geometry and functional requirements before defining the process.
CNCPioneer verifies every blade grip to ±1g against the matched-set mean mass , and every propeller hub against design model mass ±1g, on calibrated precision balance recorded per serial number.
Share hub or blade-grip drawings, material specifications, critical fits, order quantities and required inspection records to define the quotation scope.
Review assembly datums, angled features and thin-wall geometry before choosing the machining and inspection route.
Explore representative configurations and share your drawing for a product-specific review.

Fixed-pitch hubs for multirotor eVTOL lift systems — the most widely produced eVTOL propeller component.

Variable-pitch hub bodies for multirotor collective pitch, tiltrotor prop-rotor, and advanced eVTOL efficiency programs — the mechanically most complex machined propeller component.

Blade grip barrels serve as the structural intermediary between propeller blade and hub pitch axis bearing — receiving centrifugal, bending, and torsional blade loads while allowing smooth pitch rotation.

Pitch horns transmit collective pitch actuator force to blade grip rotation.

Tiltrotor Rotor Head & Swash Plate Components machined to your drawing. Confirm material, functional dimensions and finish before production.

Folding Propeller Mechanisms & Contra-Rotating Hubs machined to your drawing. Confirm material, functional dimensions and finish before production.
Match the component to its operating environment, assembly interfaces and documentation requirements.

CNC machining for eVTOL lift-propeller hubs, blade grips and folding mechanisms. Review motor interfaces, blade attachment geometry and matched-component requirements against the approved drawing.
Explore evtol machining
CNC machining for aircraft propeller hubs, variable-pitch components and blade-grip hardware. Bearing seats, attachment bores and pitch-control interfaces are planned around the assembly datums.
Explore aerospace machining
CNC machining for propeller hubs and rotor mounting hardware in unmanned aircraft and defense aviation equipment. Define material, mating dimensions, surface finish and inspection records for the application.
Explore defense machiningMaterials
Confirm the exact grade, delivery condition and finish compatibility with your drawing.
Titanium options for weight-sensitive and corrosion-resistant components. Confirm the approved grade, material condition and surface requirements.
Titanium options for weight-sensitive and corrosion-resistant components. Confirm the approved grade, material condition and surface requirements.
Aluminum options for lightweight machined components. Confirm the alloy, temper, finishing allowance and critical assembly dimensions.
Aluminum options for lightweight machined components. Confirm the alloy, temper, finishing allowance and critical assembly dimensions.
Stainless steel options for corrosion-resistant components. Confirm the grade, delivery condition, surface finish and cleaning requirements.
Confirm the exact material grade, condition, heat-treatment requirements and certificates against the approved drawing.
Aluminum options for lightweight machined components. Confirm the alloy, temper, finishing allowance and critical assembly dimensions.
Titanium options for weight-sensitive and corrosion-resistant components. Confirm the approved grade, material condition and surface requirements.
Finish selection
Select the finish around the specified material, functional surfaces and service conditions. Confirm process details and acceptance requirements with your drawing.
Review passivation against the material, functional surfaces and intended service conditions.
HV 400+ wear resistance for 7075-T6 and 2024-T4 aluminum propeller hub bodies — blade attachment bore retention zones, bolt hole countersink zones, hub arm surfaces subject to handling and installation contact.
Review shot peen against the material, functional surfaces and intended service conditions.
Review ptfe release treatment & corrosion inhibiting compound against the material, functional surfaces and intended service conditions.
Review dynamic balance against the material, functional surfaces and intended service conditions.
Machining resources for drawing review, prototypes and repeat-production programs.
Inspection & documentation
Review material identity, machining datums, functional dimensions and production records for your component.
Final tolerances, inspection coverage and acceptance criteria are confirmed against your drawing, material and geometry.
Confirm the certificates, inspection reports and production records needed for your order when sharing your drawing.
The product range includes Fixed-Pitch Propeller Hubs, Variable-Pitch Propeller Hub Bodies, Blade Grip Barrels. Custom geometry is reviewed against the approved drawing.
Material options include TC4 Titanium (AMS 4928 Annealed), TC4 STA, Aluminum 7075-T6. The exact grade and condition should be confirmed for your application.
Define assembly datums, angled features and thin-wall geometry, together with datums, tolerances and required surface condition.
Finishing options include passivation, type iii hard anodize, shot peen. Applicability is reviewed against the specified material and geometry.
Pricing and delivery are confirmed after reviewing the drawing, material availability, quantity, machining route, finishing and inspection scope.
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Share your drawing or 3D model, material, critical dimensions, finish and order quantity. We’ll review the machining route, inspection scope and delivery requirements.