Cut-to-Size Titanium Plate Blanks
Waterjet-, saw- or machined titanium plate blanks supplied from traceable parent plate to drawing dimensions, with cutting allowance, edge condition, flatness and inspection agreed before production.
- Material
- Grade 2, Grade 5, Grade 7, Grade 23 or specified titanium
- Standard
- ASTM B265, AMS or customer specification as applicable
- Form
- Sheet, plate or cut blank as specified
- Documents
- MTC, heat/lot traceability and agreed inspection reports
Product Detail
Product Introduction
Cut-to-Size Titanium Plate Blanks is ordered for a specific engineering and procurement route rather than selected from grade name alone. The RFQ must identify the governing standard and revision, grade, product dimensions, condition, surface, tests and documentation needed by the finished component manufacturer.
Product Specifications
| Product | Cut-to-Size Titanium Plate Blanks | Grade | Grade 2, Grade 5, Grade 7, Grade 23 or specified titanium |
|---|---|---|---|
| Standard | ASTM B265, AMS or customer specification as applicable applies only when expressly invoked and when its scope covers the ordered product form and grade. Use the purchase-order revision and do not substitute ASTM B265, ASTM F67, ASTM F136 or AMS4911 without written technical approval. | Size & Form | Sheet, plate and cut-to-size blanks by exact thickness, width, length or drawing dimensions |
| Tolerance | Applicable product standard and order-defined thickness, width, length, flatness, edge, surface and cut-blank tolerances | Supply Condition | Hot rolled or cold rolled, annealed, descaled, pickled, ground, polished, waterjet cut, saw cut or machined as agreed |
| Inspection | Review of material certificate and heat identity, chemistry and mechanical tests, thickness/width/length, flatness and surface, edge or cut-blank dimensions, plus ultrasonic, microstructure or supplementary reports when ordered. | Documents | MTC, heat/lot traceability and agreed inspection reports |
Additional Supply & Ordering Details
Useful, technically consistent information consolidated from earlier product pages.
| Product-form boundary | Cut-to-size titanium plate blanks are rectangular or drawing-shaped intermediate stock cut from certified parent plate. They are not a distinct titanium grade, a forging or a finished machined component. |
|---|---|
| Blank geometry to specify | State parent-plate grade and specification, thickness, blank width and length or profile drawing, squareness, edge condition, flatness, rolling direction and positive machining allowance. |
| Cutting-route controls | Select saw, waterjet, laser, plasma or machining route with explicit limits for heat-affected zone, taper, dross, contamination, edge roughness and required material removal. |
| Traceability and inspection | Request parent-plate MTC and heat identity, blank mapping when needed, dimensional report, surface and edge inspection, marking transfer and packaging that prevents mixing or face damage. |
Send the complete material RFQ
Include grade, specification revision, dimensions, tolerance, quantity, condition, tests and destination.
Chemical Composition
Weight percent; maximum unless a range is shown. Titanium is the balance. The ordered specification and grade control.
| Grade / UNS | Principal Alloying Elements | Fe max | O max | C max | N max | H max | Ti |
|---|---|---|---|---|---|---|---|
| Grade 1 / R50250 | — | 0.20 | 0.18 | 0.08 | 0.03 | 0.015 | Balance |
| Grade 2 / R50400 | — | 0.30 | 0.25 | 0.08 | 0.03 | 0.015 | Balance |
| Grade 3 / R50550 | — | 0.30 | 0.35 | 0.08 | 0.05 | 0.015 | Balance |
| Grade 4 / R50700 | — | 0.50 | 0.40 | 0.08 | 0.05 | 0.015 | Balance |
| Grade 5 / R56400 | Al 5.50–6.75; V 3.50–4.50 | 0.40 | 0.20 | 0.08 | 0.05 | 0.015 | Balance |
| Grade 6 / R54520 | Al 4.00–6.00; Sn 2.00–3.00 | 0.50 | 0.20 | 0.08 | 0.05 | 0.015 | Balance |
| Grade 7 / R52400 | Pd 0.12–0.25 | 0.30 | 0.25 | 0.08 | 0.03 | 0.015 | Balance |
| Grade 9 / R56320 | Al 2.50–3.50; V 2.00–3.00 | 0.25 | 0.15 | 0.08 | 0.03 | 0.015 | Balance |
| Grade 12 / R53400 | Mo 0.20–0.40; Ni 0.60–0.90 | 0.30 | 0.25 | 0.08 | 0.03 | 0.015 | Balance |
| Grade 11 / R52250 | Pd 0.12–0.25 | 0.20 | 0.18 | 0.08 | 0.03 | 0.0125 | Balance |
| Grade 16 / R52402 | Pd 0.04–0.08 | 0.30 | 0.25 | 0.08 | 0.03 | 0.015 | Balance |
| Grade 17 / R52252 | Pd 0.04–0.08 | 0.20 | 0.18 | 0.08 | 0.03 | 0.0125 | Balance |
| Grade 19 / R58640 | Al 3.00–4.00; V 7.50–8.50; Cr 5.50–6.50; Mo 3.50–4.50; Zr 3.50–4.50 | 0.30 | 0.12 | 0.05 | 0.03 | 0.015 | Balance |
| Grade 23 / R56407 | Al 5.50–6.50; V 3.50–4.50 | 0.25 | 0.13 | 0.08 | 0.05 | 0.0125 | Balance |
Mechanical Properties – Annealed Material Reference
| Grade | Ultimate Tensile Strength min | 0.2% Yield Strength min | Elongation min |
|---|---|---|---|
| Grade 1 | 240 MPa | 170 MPa | 24% |
| Grade 2 | 345 MPa | 275 MPa | 20% |
| Grade 3 | 450 MPa | 380 MPa | 18% |
| Grade 4 | 550 MPa | 483 MPa | 15% |
| Grade 5 | 895 MPa | 828 MPa | 10% |
| Grade 6 | 828 MPa | 793 MPa | 10% |
| Grade 7 | 345 MPa | 275 MPa | 20% |
| Grade 9 | 620 MPa | 485 MPa | 15% |
| Grade 12 | 483 MPa | 345 MPa | 18% |
| Grade 11 | 240 MPa | 170 MPa | 24% |
| Grade 16 | 345 MPa | 275 MPa | 20% |
| Grade 17 | 240 MPa | 170 MPa | 24% |
| Grade 19 / Beta-C | Acceptance depends on solution treatment, aging condition, product form and section size; use the certified values required by the invoked product or aerospace specification. | ||
| Grade 23 | 860 MPa | 795 MPa | 10% |
Representative minima only. Product form, section size, heat treatment and the invoked specification determine the certified acceptance values.
Typical Physical Properties
| Grade | Density | Elastic Modulus | Thermal Expansion |
|---|---|---|---|
| Grade 1 | 4.51 g/cm³ | Approx. 103 GPa | Approx. 8.6 µm/m·K |
| Grade 2 | 4.51 g/cm³ | Approx. 105 GPa | Approx. 8.6 µm/m·K |
| Grade 3 | 4.51 g/cm³ | Approx. 105 GPa | Approx. 8.6 µm/m·K |
| Grade 4 | 4.51 g/cm³ | Approx. 105 GPa | Approx. 8.6 µm/m·K |
| Grade 5 | 4.43 g/cm³ | Approx. 114 GPa | Approx. 8.6 µm/m·K |
| Grade 6 | Approx. 4.48 g/cm³ | Approx. 110 GPa | Approx. 8.8 µm/m·K |
| Grade 7 | Approx. 4.51 g/cm³ | Approx. 105 GPa | Approx. 8.6 µm/m·K |
| Grade 9 | Approx. 4.48 g/cm³ | Approx. 105 GPa | Approx. 9.0 µm/m·K |
| Grade 12 | Approx. 4.54 g/cm³ | Approx. 103 GPa | Approx. 8.6 µm/m·K |
| Grade 11 | Approx. 4.51 g/cm³ | Approx. 103 GPa | Approx. 8.6 µm/m·K |
| Grade 16 | Approx. 4.51 g/cm³ | Approx. 105 GPa | Approx. 8.6 µm/m·K |
| Grade 17 | Approx. 4.51 g/cm³ | Approx. 103 GPa | Approx. 8.6 µm/m·K |
| Grade 19 / Beta-C | Approx. 4.82 g/cm³ | Condition-dependent; use certified engineering data | Condition-dependent; verify for design |
| Grade 23 | 4.43 g/cm³ | Approx. 114 GPa | Approx. 8.6 µm/m·K |
Typical engineering references, not inspection acceptance limits.
Certificates & Inspection Records
Services We Can Provide
Product Packaging
Sheet and plate surfaces are interleaved or wrapped as required, protected at edges and secured on pallets or in export cases with grade, heat and dimensional identification. Typical export packaging for the same physical product form is shown below; final packing is confirmed for each order.
Application Scenarios
Near-net machining blanks
Material grade, dimensions, condition and inspection must be matched to the application requirements.
Flanges, covers, brackets and structural parts
Material grade, dimensions, condition and inspection must be matched to the application requirements.
Low-volume drawing-specific titanium components
Material grade, dimensions, condition and inspection must be matched to the application requirements.
FAQ
Can another titanium plate standard be substituted?
Only with written technical approval. Standards can differ in scope, grade designation, condition, testing, microstructure, melt route and documentation.
Which dimensions should be included in the RFQ?
Provide thickness, width and length or a controlled drawing, tolerances, flatness, edge/cut condition and machining allowance.
What documentation can be requested?
State the required MTC, heat/lot traceability, chemistry, tensile results, dimensional report, ultrasonic or microstructure report and regulatory or aerospace documents.
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