21CrMoV5-7 Gas Turbine Bolts (EN 10269 / 1.7709)

21CrMoV5-7 gas turbine bolts service

21CrMoV5-7 gas turbine bolts are specified into compressor casing flanges, combustor liner flanges and turbine outer-case bolting on industrial gas turbines where metal temperatures sit in the 200 to 550 deg C window. The Cr-Mo-V Q+T chemistry resists thermal-cycle relaxation through the start-stop cycles characteristic of peaking and load-following gas turbines.

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Service Envelope

Gas turbine stageTypical metal temp21CrMoV5-7 use
Inlet casing20 to 50 deg Cn/a (carbon steel acceptable)
Compressor casing (front)50 to 200 deg COptional; 42CrMo4 acceptable
Compressor casing (rear)200 to 500 deg CPrimary choice
Combustor outer casing400 to 550 deg CPrimary choice; design margin tight
Turbine outer case (LP)400 to 550 deg CPrimary choice
Turbine outer case (HP)550 to 700 deg COutside envelope; Durehete 1055 or nickel-base

Bolting Form Factors Used

Mechanical Floors for Gas Turbine Bolts Service

PropertyValueCondition
Tensile (Rm)700 to 850 MPaRT, Q+T
0.2 percent proof stress (Rp0.2)≥550 MPaRT, Q+T
Elongation A5≥16 percentRT, longitudinal
Charpy V impact (KV)≥63 J20 deg C
0.2 percent proof at 500 deg C≥450 MPaelevated-temp
Hardness210 to 250 HBWQ+T

Standards Anchor

21CrMoV5-7 gas turbine bolts to EN 10269. Cross-procurement on US-design gas turbines (GE, Siemens-Westinghouse) uses ASTM A193 Grade B16 with dual-certification. Combustor and turbine outer-case bolting on the HP end (above 550 deg C) steps up to Durehete 1055.

When to Step Up the Grade

For service above 550 deg C metal temperature, the design steps up to Durehete 1055 (Alloy T41 / Werkstoff 1.7729 / 20CrMoVTiB4-10) with Ti+B microalloying for extended creep envelope. For heavier sections of the same temperature window, sister grade 21CrMoV5-11 (1.8070) provides extended hardenability.

Frequently Asked Questions

Q. What gas turbine OEMs specify 21CrMoV5-7?
Siemens Energy gas turbines (SGT-300 / SGT-500 / SGT-700 / SGT-8000H families), GE / Baker Hughes industrial gas turbines (Frame 6 / Frame 7 / Frame 9), Mitsubishi Power H-class, BHEL industrial gas turbines, Alstom (now GE) GT26 family. The grade is the European-derived workhorse for compressor and combustor casing bolting.

Q. How is the metal-temperature envelope set for gas turbine bolting?
By the design steady-state metal temperature at the bolt location plus a thermal-cycling allowance for start-stop and load-following service. Peaking gas turbines cycle daily; combined-cycle base-loaded units cycle less. The cycling allowance reduces the allowable design stress by 5 to 15 percent.

Q. Are body-bound studs used in gas turbine casings?
Yes. On compressor casing half-joints where cyclic thermal expansion would rock a clearance-fit bolt, body-bound studs with H7/n6 fit transfer the shear load through the bolt body.

Q. What is the difference between gas turbine and steam turbine bolting selection?
Steam turbine bolting sees more steady-state high-temperature service; gas turbine bolting sees more thermal cycling. 21CrMoV5-7 handles both within the 550 deg C envelope, with cycling design margin set in the gas turbine application.

More 21CrMoV5-7 service applications: Steam Turbine Bolts · Power Plant Bolting · Pressure Vessel Bolts · Boiler Bolts · Heat Exchanger Bolts · Fired Heater Bolts · Petrochem Reactor Bolts. Back to the 21CrMoV5-7 Alloy Hub.