Manufacturing Record

Aerospace Hollow Rotary Shaft

A quenched-and-tempered hollow shaft engineered for high rotational loads and demanding aerospace service.

Engineering case

Engineering challenge, manufacturing response and verified result

Component application, material and performance requirements are translated into defined manufacturing controls and documented verification.

01Project context
Component
Aerospace Hollow Rotary Shaft
Dimensions & Weight
Project-specific

Application

Aerospace rotating equipment

Material

34CrMo1A alloy steel

Performance & acceptance points
  • Tensile strength >= 1080 MPa
  • Quenched and tempered
02Engineering problem

Challenge

For Aerospace rotating equipment, the Aerospace Hollow Rotary Shaft must use 34CrMo1A alloy steel at project-specific dimensions and weight while meeting Tensile strength >= 1080 MPa; Quenched and tempered. The engineering challenge is coordinated control of metal flow, section uniformity and internal integrity.

03Manufacturing response

Manufacturing Scope

01Material & heat review02Heating & open-die forging03Post-forging heat treatment04Rough & finish machining05NDT & property testing06Final inspection & packing
Core Manufacturing Strategy

YL Solution

The forming strategy controls metal flow, section uniformity and internal integrity. Heating practice, deformation sequence, forging reduction, heat treatment and machining allowance are coordinated with defined material, dimensional, NDT and property release points.

Forming capabilityOpen-die hydraulic presses and project-specific tooling
Heat treatmentPost-forging heat treatment aligned to material and property targets
MachiningHeavy turning, milling and project-specific finishing
Inspection controlChemistry, mechanical properties, NDT and dimensional inspection
04Verified delivery

Result / Verification

Delivery basis: Machined condition. Tensile strength >= 1080 MPa; Quenched and tempered are incorporated into the project inspection plan, with final inspection records and the quality dossier supporting acceptance and release.

Product technical recordParameters, inspection and delivery records
Material grade34CrMo1A alloy steel
Mechanical propertyTensile strength >= 1080 MPa
ServiceHigh-speed aerospace rotating equipment
Critical controlsHollow geometry, heat-treatment uniformity and dynamic-load integrity
Inspection plan

Heat/lot traceability and chemical analysis

Mechanical-property testing to the approved specification

UT / MT / PT and dimensional inspection as technically required

Delivery dossier

Material certificate and heat/lot traceability

Heat-treatment and inspection records

Final dimensional report and release dossier

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