HN200 Helicoflexcatalog
User Manual: HN200
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HELICOFLEX® High Performance Seals and Sealing Systems Helicoflex Spring Energized Seals GENERAL INFORMATION The Helicoflex® seal represents the leading edge in seal technology for high performance sealing applications. Today’s extreme sealing requirements have rendered traditional seals & gaskets obsolete. If you can’t afford the lost time associated with leaks, put your trust in the leader: Helicoflex®. SEALING CONCEPT The sealing principle of the Helicoflex® family of seals is based upon the plastic deformation of a jacket of greater ductility than the flange materials. This occurs between the sealing face of a flange and an elastic core composed of a close-wound helical spring. The spring is selected to have a specific compression resistance. During compression, the resulting specific pressure forces the jacket to yield and fill the flange imperfections while ensuring positive contact with the flange sealing faces. Each coil of the helical spring acts independently and allows the seal to conform to surface irregularities on the flange surface. This combination of elasticity and plasticity makes the Helicoflex seal the best overall performing seal in the industry. Free State In Compression GENERAL CHARACTERISTICS • Wide range of applications: Dimensional: • • • • • • 2 Diameters from 0.250 inches (6.3 mm) to over 300 inches (7.6 m) Cross sections from 0.063 inches (1.6 mm) to over 0.625 inches (15.9 mm) Temperature: Cryogenic to 1800°F (982°C) Pressure: Ultra High Vacuum to 50,000 PSI (100,000 PSI under special conditions) Excellent springback: the spring energized Helicoflex is capable of compensating for flange distortions due to temperature and pressure cycling. Adaptable to a majority of standard flanges: ANSI, ISO, KF, ASA Suited to different types of assemblies: -metal/metal with groove -flat flanges with limiter/retainer -3 face contact Extended shelf life Excellent resistance to corrosion and radiation Minimum relaxation: the Helicoflex’s resilient spring compensates for relaxation ensuring positive seal contact. For Additional Information, Please Consult Our Engineering Staff 1-800-233-1722 CLASSIFICATION OF SEAL TYPE HN 2 Seal Configurations Cross Section Type 0 #Jackets/ Linings 8 Jacket Orientation Section Orientation CONFIGURATION GUIDE Cross Section Type HN HNR HNV HND HNDE single section ground spring for precise load control (Beta Spring) low load (Delta Seal) tandem Helicoflex seals tandem Helicoflex and elastomer seals note: “L” indicates internal limiter (ex: HLDE) Jacket/Lining 1 = jacket only 2 = jacket with inner lining Jacket Orientation 0 1 2 3 4 5 6 7 8 9 Section Orientation 0 1 2 3 4 5 6 7 8 9 TYPICAL CONFIGURATIONS HN200 HN240 Groove assemblies 3 face compression HN208 HN203 Raised face flanges ANSI B16.5 Tongue & groove HNDE290 HND229 Leak check inert gas purge Valve seats For Additional Information, Please Consult Our Engineering Staff 1-800-233-1722 3 The resilient characteristic of the Helicoflex® seal ensures useful elastic recovery during service. This elastic recovery permits the Helicoflex® seal to accommodate minor distortions in the flange assembly due to temperature and pressure cycling. For most sealing applications the Y0 value will occur early in the compression curve and the Y1 value will occur near the end of the decompression curve. The compression and decompression cycle of the Helicoflex® seal is characterized by the gradual flattening of the compression curve. The decompression curve, which is distinct from the compression curve, is the result of a hysteresis effect and permanent deformation of the spring and jacket. DEFINITION OF TERMS ec = compression limit beyond which there is risk of damaging the spring n essio n m pr e2 = optimum compression r e ssio Y0 Y1 = load on the decompression curve below which leak rate exceeds required level omp Y2 = load required to reach optimum compression e2 Y2 D ec Y0 = load on the compression curve above which leak rate is at required level Linear load (lbs/in) Y1 Co Helicoflex Seal Characteristics CHARACTERISTIC CURVE Compression (inches) e0 Permanent deformation e1 e2 ec Useful elastic recovery INTRINSIC POWER OF THE SEAL PSI Pu Pu 68° Temperature (°F) (maximum) The intrinsic power of the Helicoflex seal reflects its ability to maintain and hold system pressure for a given temperature at Y2 and e2. This value is expressed as a specific pressure and is noted by the symbols Pu (room temperature) and Pu (at operating temperature). The influence of temperature on Pu is shown in the graph above. The tables on pages 10 and 11 give the values of Pu at 68°F (20°C), Pu at a given temperature and the maximum temperature where Pu = 0. 4 For Additional Information, Please Consult Our Engineering Staff 1-800-233-1722 Helicoflex Seal Specifications DEFINITION OF CHARACTERISTIC VALUES Dj Mean reaction diameter of the seal. (For a double section seal, Dj = Dj1 + Dj2) ____________ inches Y2 Linear load corresponding to e2 compression ____________ lbs/inch Y1 Linear load on the seal to maintain sealing in service at low pressure (=Ym1) ____________ lbs/inch Pu Intrinsic power of the seal under pressure at 68°F (20°C) when the reaction force ____________ PSI of the seal is maintained at Y2 , regardless of the operating conditions. Pu Value of Pu at temperature ____________ PSI P Operating or proof pressure ____________ PSI Note: if Pu orP Pu >1, the definition of the seal must be modified This ratio must never exceed 1. Ym2 Linear tightening load on the seal at room temperature to maintain sealing under pressure. P Ym2 = Y2 Pu Ym2 Value of Ym2 at temperature Et Young’s modulus of bolt material at 68°F (20°C) ____________ PSI Ets Young’s modulus of bolt material at operating temperature ____________ PSI . Ym2 = Y2 P Pu ____________ lbs/inch ____________ lbs/inch LOAD CALCULATIONS ____________ lbs Fj Total tightening load to compress the seal to the operating point (Y2; e2) Fj = π x Dj x Y2 FF Total hydrostatic end force FF = π/4 Dj12 x P (Dj1 = Dj in case of a single section seal) ____________ lbs Fm Minimum total load to be maintained on the seal in service to preserve sealing, i.e. Fm = π Dj Ym where: Ym = the greater of the two values: Ym1 or Ym2 (see note 1 below) ____________ lbs Fs Total load to be applied on the bolts to maintain sealing in service. FS = FF + Fm ____________ lbs Fs* Increased value of FS to compensate for Young’s modulus at temperature Fs* = Fs Et / Ets ____________ lbs FB LOAD TO BE APPLIED: ____________ lbs If Fs* > Fj If Fj > Fs* then then Fb = Fs* Fb = Fj Note 1: wherever the working pressure is high and/or seal diameter is big, to such an extent that P•Dj ≥ 32 Ym, in order to remain on the safe side, whatever the inaccuracy on the tightening load may be, it is recommended to take the Fj value in lieu of Fm for the calculation of Fs so that Fs = FF + Fj. Note 2: this information is provided as a reference only. For Additional Information, Please Consult Our Engineering Staff 1-800-233-1722 5 Groove Design - Radial Pressure g CALCULATIONS Groove Depth (F) Depth Tolerance (f) Groove Width (g) Seal OD (A) Groove Finish Flatness e2 F +- f J/2 = Cross Section (CS)-e2 = e2 X 0.12 = See table below = Groove OD (C) - Clearance (J) = See table below = See table below A+- t h C+- 0.000 CLEARANCE AND MINIMUM GROOVE WIDTH Pressure < 300 psi (20 bar) Clearance Min Groove Width J g J = e2 g > CS + 2e2 J = e2 g > CS + 2e2 J = e2 g > CS + 2e2 Pressure ≥ 300 psi (20 bar) Clearance Min Groove Width J g J = 0.012 J = 0.3 g > CS + 2 e2 J = 0.020 J = 0.5 g > CS + 2 e2 J = 0.028 J = 0.7 g > CS + 2 e2 Pressure < 300 psi (20 bar) Seal Tolerance Groove Tolerance t h 0.005 0.13 0.005 0.13 0.010 0.25 0.010 0.25 0.010 0.25 0.010 0.25 0.015 0.38 0.015 0.38 0.020 0.51 0.015 0.38 Consult our engineering staff Pressure ≥ 300 psi (20 bar) Seal Tolerance Groove Tolerance t h 0.004 0.10 0.004 0.10 0.004 0.10 0.004 0.10 0.006 0.15 0.006 0.15 0.008 0.20 0.008 0.20 0.010 0.25 0.008 0.20 Consult our engineering staff Seal Cross Section CS 0.059 to 0.134 0.138 to 0.272 0.276 to 0.390 1.5 to 3.4 3.5 to 6.9 7.0 to 9.9 SEAL / GROOVE TOLERANCES Seal Diameter Range 0.350 2.001 12.001 25.001 48.001 to to to to to > 2.000 3.8 to 12.000 50.0 to 25.000 305.0 to 48.000 635.0 to 72.000 1220.0 to 72.000 > 50.0 305.0 635.0 1220.0 1830.0 1830.0 SURFACE FINISH Nr. LCA-CEA Ra in µm Rt in µm RMS SHAPED SEALS N10 N9 N8 12.5 6.3 3.2 50 37 21 500 250 125 N7 1.6 11 63 N6 N5 0.8 0.4 6.2 3.4 32 16 N4 0.2 1.9 8 Aluminum Silver, copper, iron Nickel, stainless steel recommended consult our engineering staff Note: Machining/polishing marks must follow seal circumference Groove Design: Contact our engineering staff for assistance in designing non-circular grooves. Groove Finish: Most applications will require a finish of 16-32 RMS (0.4 to 0.8 Ra µm). All machining & polishing marks must follow seal circumference. Min. Seal Radius: The minimum seal bending radius is six times the seal cross section (CS). Seating Load: The load (Y2) to seat the seal is approximately 30% higher due to a slightly stiffer spring design. FLATNESS Seal Diameter Range 0.350 to 20.000 10 to 500 20.001 to 80.000 500 to 2000 Amplitude 0.008 0.2 0.016 0.4 Tangential Slope Radial Slope 1:1000 2:1000 1:100 2:100 Dimensions in inches 6 Dimensions in mm For Additional Information, Please Consult Our Engineering Staff 1-800-233-1722 Cavity Design - Axial Pressure THREE FACE COMPRESSION 30°Type HN 140 - 240 J 45°Type HN 140 - 240 J 30° 60°Type HN 100 - 200 J 45° h Seal ID (A) e Shaft OD (E) e 60° Seal ID (A) Seal ID (A) e Shaft OD (E) Shaft OD (E) h h E=Shaft OD + 0.000 — 0.002 + 0.00 — 0.05 CALCULATIONS Axial Load (Ya) Shaft OD (E) Clearance (J) Axial Compression (e) Cavity Finish A=Seal D + 0.002 — 0.000 + 0.05 — 0.00 COEFFICIENT VALUES = K • Y2 = Seal ID (A) < CS / 10 = a • e2 < 32 RMS (0.8 um) Coefficient a K 30° 2 0.9 45° 1.4 1.2 60° 1.15 1.4 Cross Section CS “h” VALUES 30° Cross Section CS in mm 0.102 2.6 0.126 3.2 0.165 4.2 0.205 5.2 0.252 6.4 Aluminum Jacket in mm 0.130 3.30 0.157 4.00 0.207 5.25 0.260 6.60 0.321 8.15 Other Jackets in mm 0.126 3.20 0.157 4.00 0.207 5.25 0.260 6.60 0.321 8.15 45° Aluminum Other Jacket Jackets in mm in mm 0.163 4.15 0.157 4.00 0.199 5.05 0.199 5.05 0.260 6.60 0.260 6.60 0.327 8.30 0.327 8.30 0.402 10.20 0.402 10.20 60° Aluminum Jacket in mm 0.126 3.20 0.157 4.00 0.213 5.40 0.272 6.90 0.339 8.60 Other Jackets in mm 0.134 3.40 0.165 4.20 0.220 5.60 0.280 7.10 0.346 8.80 Dimensions in inches Dimensions in mm TARGET SEALING CRITERIA The ultimate leak rate of a joint is a function of the seal design, flange design, bolting, surface finish and other factors. Helicoflex seals are designed to provide two levels of service: Helium Sealing or Bubble Sealing. Helium Sealing: These Helicoflex seals are designed with a target Helium leak rate not to exceed 1x10-9 cc/sec.atm under a ∆P of 1 atmosphere. The ultimate leak rate will depend on the factors listed above. Bubble Sealing: These Helicoflex seals are designed with a target air leak rate not to exceed 1x10-4 cc/sec.atm under a ∆P of 1 atmosphere. For Additional Information, Please Consult Our Engineering Staff 1-800-233-1722 7 CALCULATIONS ACCORDING TO CODES Operating load Hydrostatic force Code Calculations Minimum service load Minimum tightening load to apply on bolts D.I.N. 2505 1990 A.S.M.E. Section VIII Division 1 CODAP 1995 Garlock Helicoflex CEFILAC FDV = π.dD.kO.KDV Wm2 = π.b.G.y FA = π.Dj.JE.PA Fj = π.Dj.Y2 2 FP = π.(dD) .P 4 2 H = π.G .P 4 2 FF = π.(Dj) .P 4 2 FF = π.(Dj) .P 4 FDB = π.dD.kB.P FSO = (1) FDV (2) FP + FBD Use the greater of the two (1) or (2) HP = 2.b.π.G.m.P W= (1) Wm2 (2) H + Hp = Wm1 Use the greater of the two (1) or (2) Fj = 2.π.Dj.JE.m.P FS = (1) FA (2) FF + Fj Fm = π.Dj.Ym Ym1 = Y1 P Ym2 = Y2 Pu Use the greater of the two Ym = FB = (1) Fj (2) FF + Fj = FS Use the greater of the two (1) or (2) Use the greater of the two (1) or (2) A.S.M.E. Section VIII Division 1 CODAP 1995 Garlock Helicoflex CEFILAC Wm2 = Fj b=1 G = Dj Y = Y2 FA = Dj = Dj JE = 1 PA = Y2 Fj Wm2 = π.Dj.Y2 FA = π.Dj.Y2 FF EQUIVALENT SYMBOLS D.I.N. 2505 1990 Operating load FDV = Fj dD = Dj kO.KDV = Y2 FDV = π.Dj.Y2 Hydrostatic force Minimum service load FP = FF dD = Dj H = FF G = Dj FA = Dj = Dj 2 FP = π.(Dj) .P 4 2 H = π.(Dj) .P 4 2 FF = π.(Dj) .P 4 FDB = Fm dD = Dj kB.P = Ym FDB = π.Dj.Ym Minimum bolt load Hp = Fm b=1 G = Dj 2.m.P = Ym m = Ym 2.P HP = π.Dj.Ym Fj = Fm Dj = Dj JE = 1 2.m.P = Ym m = Ym 2.P Fj = π.Dj.Ym FSO = FB FSO = (1) Fj (2) FF + Fm = FS W = FB W = (1) Fj (2) FF + Fm = FS FS = FB FS = (1) Fj (2) FF + Fm = FS Use the greater of the two (1) or (2) Use the greater of the two (1) or (2) Use the greater of the two (1) or (2) Note: Due to its circular cross section, the Helicoflex seal exhibits a “line” load instead of an “area load” typical of traditional gaskets. As a result, “m”, “b” and “y” factors are not pertinent when applied to the Helicoflex seal. The above equivalent equations were developed to assist flange designers with their calculations. 8 For Additional Information, Please Consult Our Engineering Staff 1-800-233-1722 ANSI B16.5 RAISED FACE FLANGE The Helicoflex® HN208a is ideally suited for standard raised face flanges. The resilient nature of the seal allows it to compensate for the extremes of high temperature and pressure where traditional spiral wounds and double jacketed seals fail. The jacket and spring combination can be modified to meet most requirements of temperature and pressure. In addition, a large selection of jacket materials ensures chemical compatibility in corrosive and caustic media. SEAL TYPE: HN208a Standard Flanges Jacket Aluminum Silver Copper Soft Iron Nickel Monel Hastelloy C Stainless Steel Alloy 600 Alloy X750 Titanium 0.120" Seal OD (A) Mean Diameter (d) Cross Section Availability (inches) Standard Standard Standard Optional Standard Optional Optional Standard Optional Optional Optional 0.160 0.160 0.155 0.155 0.150 0.150 0.150 0.150 0.150 0.150 0.150 Seating Recommended Load Flange (lbs/in)* Finish (RMS) 1150 1725 2250 2250 2800 2800 2800 3800 3800 4000 4000 63 - 125 63 - 125 63 - 125 32 - 63 32 - 63 32 - 63 32 - 63 32 - 63 32 - 63 32 - 63 32 - 63 * Note: Seating load only! Does not allow for hydrostatic end force. See page 5 for calculations. SEAL DIMENSIONS Nominal Mean Diameter Diameter (d) 1/2 0.827 3/4 1.102 1 1.417 1-1/4 1.890 1-1/2 2.283 2 2.913 2-1/2 3.425 3 4.173 3-1/2 4.685 4 5.256 5 6.378 6 7.500 8 9.567 10 11.693 12 13.858 14 15.098 16 17.205 18 19.567 20 21.575 24 25.728 150lb 1.874 2.252 2.626 3.000 3.374 4.126 4.874 5.374 6.374 6.874 7.752 8.752 10.996 13.374 16.126 17.752 20.252 21.626 23.874 28.252 300lb 2.126 2.626 2.874 3.252 3.752 4.374 5.126 5.874 6.500 7.126 8.500 9.874 12.126 14.252 16.626 19.126 21.252 23.500 25.752 30.500 400lb 2.126 2.626 2.874 3.252 3.752 4.374 5.126 5.874 6.500 7.000 8.374 9.752 12.000 14.126 16.500 19.000 21.126 23.374 25.500 30.252 Seal OD (A) 600lb 2.126 2.626 2.874 3.252 3.752 4.374 5.126 5.874 6.374 7.626 9.500 10.500 12.626 15.752 18.000 19.374 22.252 24.126 26.874 31.126 900lb 2.500 2.752 3.122 3.500 3.874 5.626 6.500 6.626 N/A 8.126 9.752 11.413 14.126 17.126 19.626 20.500 22.626 25.126 27.500 32.996 1500lb 2.500 2.752 3.122 3.500 3.874 5.626 6.500 6.874 N/A 8.252 10.000 11.126 13.874 17.126 20.500 22.752 25.252 27.752 29.752 35.500 2500lb 2.752 3.000 3.374 4.126 4.626 5.752 6.626 7.752 N/A 9.252 11.000 12.500 15.252 18.760 21.626 N/A N/A N/A N/A N/A Note: Consult our engineering staff for other available sizes and materials. For Additional Information, Please Consult Our Engineering Staff 1-800-233-1722 9 Calculation Data - U.S. Customary HELIUM SEALING Jacket Material Aluminum Silver Copper, Soft Iron, Mild Steels Nickel, Monel, Tantalum Stainless Steel, Inconel, Titanium 10 BUBBLE SEALING Cross Section In 0.063 0.075 0.087 0.098 0.118 0.138 0.157 0.177 0.197 0.217 0.236 0.276 0.315 e2 in 0.024 0.028 0.028 0.028 0.031 0.031 0.035 0.035 0.035 0.035 0.039 0.039 0.039 eC Y2 Y1 Pu68°F Pu 392°F in lbs/inch lbs/inch PSI PSI 0.028 857 114 7250 N/A 0.033 914 114 7540 N/A 0.035 942 114 7685 N/A 0.035 999 114 7975 725 0.039 1056 143 7975 1450 0.039 1085 143 7975 2030 0.043 1142 143 8700 2465 0.047 1199 143 8700 2900 0.055 1256 171 9135 3190 0.063 1313 171 9425 3480 0.071 1399 200 9715 3625 0.087 1542 228 10150 4060 0.102 1656 286 10440 4640 0.063 0.075 0.087 0.098 0.118 0.138 0.157 0.177 0.197 0.217 0.236 0.276 0.315 0.020 0.024 0.024 0.028 0.031 0.031 0.031 0.031 0.031 0.031 0.035 0.035 0.035 0.024 0.028 0.031 0.035 0.039 0.039 0.043 0.043 0.051 0.055 0.067 0.079 0.094 1142 1256 1313 1370 1485 1599 1713 1827 1941 2056 2284 2512 2798 171 171 200 257 286 286 314 343 343 371 400 457 514 9425 9425 10150 10875 12325 13775 15225 16675 18125 19575 21750 23200 24650 Pu 482°F N/A N/A N/A 1160 2030 3190 3915 4495 5220 5800 6815 7830 8700 857 857 914 971 1028 1085 1142 1256 1313 1428 1542 1713 1999 171 171 171 228 257 257 286 286 286 343 343 371 400 0.063 0.075 0.087 0.098 0.118 0.138 0.157 0.177 0.197 0.217 0.236 0.276 0.315 0.020 0.024 0.024 0.028 0.028 0.028 0.031 0.031 0.031 0.031 0.035 0.035 0.035 0.024 0.028 0.031 0.035 0.039 0.039 0.043 0.043 0.051 0.055 0.067 0.079 0.094 1485 1599 1713 1827 1999 2227 2455 2684 2912 3141 3597 4225 4911 228 286 343 400 457 457 514 571 628 685 799 914 1085 7250 7250 7975 8700 9425 10150 10150 11600 12325 13050 13775 14500 15950 Pu 572°F 1450 1595 1885 2465 2900 3335 3915 4350 4785 5220 5800 6525 7105 1085 1142 1256 1313 1428 1542 1656 1827 1884 2056 2284 2627 3026 0.063 0.075 0.087 0.098 0.118 0.138 0.157 0.177 0.197 0.217 0.236 0.276 0.315 0.016 0.020 0.020 0.024 0.024 0.024 0.028 0.028 0.028 0.028 0.031 0.031 0.031 0.020 0.024 0.028 0.031 0.035 0.035 0.039 0.039 0.043 0.051 0.063 0.071 0.083 1827 1999 2227 2512 2512 2798 3312 4111 4454 4625 N/A N/A N/A 457 10150 457 10440 514 11020 571 11890 628 12615 685 13485 799 13920 857 15225 1028 15950 1142 16675 N/A N/A N/A N/A N/A N/A Pu 662°F 1595 2320 3045 3915 4930 5800 6525 7540 8265 8990 N/A N/A N/A 0.063 0.075 0.087 0.098 0.118 0.138 0.157 0.177 0.197 0.217 0.236 0.276 0.315 0.016 0.020 0.020 0.024 0.024 0.024 0.028 0.028 0.028 0.028 0.031 0.031 0.031 0.020 0.024 0.028 0.031 0.035 0.035 0.039 0.039 0.043 0.051 0.063 0.071 0.083 1999 2284 2570 2855 3283 3769 4283 4711 N/A N/A N/A N/A N/A 571 571 628 685 742 857 971 1256 N/A N/A N/A N/A N/A Pu 752°F 3625 3915 4205 4640 5220 5655 6090 6525 N/A N/A N/A N/A N/A 13050 13195 13340 14065 14500 15080 15515 15950 N/A N/A N/A N/A N/A Y2 Y1 Pu68°F Pu 392°F lbs/inch lbs/inch PSI PSI 514 114 5075 N/A 571 114 5800 N/A 600 114 5800 N/A 657 114 6090 725 742 114 6525 1450 799 114 6815 2030 857 114 7250 2465 914 114 7540 2900 971 143 7975 3190 1028 143 8265 3480 1113 171 8700 3625 1171 200 9425 4060 1285 228 9860 4495 Max Temp °F 302 302 356 428 482 482 536 536 572 608 644 644 680 5800 5800 5800 6525 7250 7975 8700 10150 11600 13050 15950 18125 20300 Pu 482°F N/A N/A 580 725 1305 1885 2320 2755 3190 3625 4350 5220 6090 464 464 536 536 572 572 662 698 698 752 842 842 932 171 228 286 343 400 400 457 457 514 571 571 628 742 5075 5075 5075 5800 5800 6525 6525 6525 7250 7250 7975 8700 9425 Pu 572°F 725 870 1160 1450 1740 2175 2465 2755 3045 3335 3770 4205 4640 662 662 680 716 716 752 788 842 842 896 968 968 1022 1142 1256 1313 1542 1713 1941 2170 2398 2627 2855 3198 3712 4168 343 343 400 400 457 514 571 628 628 685 742 857 914 5800 6090 6380 6815 7250 7830 8265 8700 9425 9715 10440 11310 12035 Pu 662°F 1015 1305 1740 2320 2900 3335 3915 4350 4785 5365 5945 6525 7250 716 716 788 842 896 932 1022 1112 1202 1202 1202 1202 1202 1713 1827 1999 2170 2427 2684 2969 3198 3426 3712 4111 4568 5139 457 457 514 571 628 742 857 1028 1085 1142 1256 1485 1656 6815 7250 7540 8265 8990 9715 10440 11165 11890 12615 13630 14790 15660 Pu 752°F 870 1160 1595 2175 2900 3625 4350 4930 5365 6090 6815 7540 8410 788 788 896 932 932 1022 1112 1202 1292 1292 1292 1292 1292 For Additional Information, Please Consult Our Engineering Staff 1-800-233-1722 HELIUM SEALING Calculation Data - Metric Jacket Material Aluminum Silver Copper, Soft Iron, Mild Steels Nickel, Monel, Tantalum Stainless Steel, Inconel, Titanium BUBBLE SEALING Cross Section mm 1.6 1.9 2.2 2.5 3.0 3.5 4.0 4.5 5.0 5.5 6.0 7.0 8.0 e2 mm 0.6 0.7 0.7 0.7 0.8 0.8 0.9 0.9 0.9 0.9 1.0 1.0 1.0 eC Y2 Y1 Pu20°C Pu 200°C mm daN/cm daN/cm daN/cm2 daN/cm2 0.7 150 20 50 N/A 0.85 160 20 52 N/A 0.9 165 20 53 N/A 0.9 175 20 55 5 1.0 185 25 55 10 1.0 190 25 55 14 1.1 200 25 60 17 1.2 210 25 60 20 1.4 220 30 63 22 1.6 230 30 65 24 1.8 245 35 67 25 2.2 270 40 70 28 2.6 290 50 72 32 Y2 Y1 Pu20°C Pu 200°C daN/cm daN/cm daN/cm2 daN/cm2 90 20 35 N/A 100 20 40 N/A 105 20 40 N/A 115 20 42 5 130 20 45 10 140 20 47 14 150 20 50 17 160 20 52 20 170 25 55 22 180 25 57 24 195 30 60 25 205 35 65 28 225 40 68 31 Max Temp °C 150 150 180 220 250 250 280 280 300 320 340 340 360 1.6 1.9 2.2 2.5 3.0 3.5 4.0 4.5 5.0 5.5 6.0 7.0 8.0 0.5 0.6 0.6 0.7 0.8 0.8 0.8 0.8 0.8 0.8 0.9 0.9 0.9 0.6 0.7 0.8 0.9 1.0 1.0 1.1 1.1 1.3 1.4 1.7 2.0 2.4 200 220 230 240 260 280 300 320 340 360 400 440 490 30 30 35 45 50 50 55 60 60 65 70 80 90 65 65 70 75 85 95 105 115 125 135 150 160 170 Pu 250°C N/A N/A 6 8 14 22 27 31 36 40 47 54 60 150 150 160 170 180 190 200 220 230 250 270 300 350 30 30 30 40 45 45 50 50 50 60 60 65 70 40 40 40 45 50 55 60 70 80 90 110 125 140 Pu 250°C N/A N/A 4 5 9 13 16 19 22 25 30 36 42 240 240 280 280 300 300 350 370 370 400 450 450 500 1.6 1.9 2.2 2.5 3.0 3.5 4.0 4.5 5.0 5.5 6.0 7.0 8.0 0.5 0.6 0.6 0.7 0.7 0.7 0.8 0.8 0.8 0.8 0.9 0.9 0.9 0.6 0.7 0.8 0.9 1.0 1.0 1.1 1.1 1.3 1.4 1.7 2.0 2.4 260 280 300 320 350 390 430 470 510 550 630 740 860 40 50 60 70 80 80 90 100 110 120 140 160 190 50 50 55 60 65 70 70 80 85 90 95 100 110 Pu 300°C 10 11 13 17 20 23 27 30 33 36 40 45 49 190 200 220 230 250 270 290 320 330 360 400 460 530 30 40 50 60 70 70 80 80 90 100 100 110 130 35 35 35 40 40 45 45 45 50 50 55 60 65 Pu 300°C 5 6 8 10 12 15 17 19 21 23 26 29 32 350 350 360 380 380 400 420 450 450 480 520 520 550 1.6 1.9 2.2 2.5 3.0 3.5 4.0 4.5 5.0 5.5 6.0 7.0 8.0 0.4 0.5 0.5 0.6 0.6 0.6 0.7 0.7 0.7 0.7 0.8 0.8 0.8 0.5 0.6 0.7 0.8 0.9 0.9 1.0 1.0 1.1 1.3 1.6 1.8 2.1 320 350 390 440 440 490 580 720 780 810 N/A N/A N/A 80 80 80 100 110 120 140 150 180 200 N/A N/A N/A 70 72 76 82 87 93 96 105 110 115 N/A N/A N/A Pu 350°C 11 16 21 27 34 40 45 52 57 62 N/A N/A N/A 200 220 230 270 300 340 380 420 460 500 560 650 730 60 60 70 70 80 90 100 110 110 120 130 150 160 40 42 44 47 50 54 57 60 65 67 72 78 83 Pu 350°C 7 9 12 16 20 23 27 30 33 37 41 45 50 380 380 420 450 480 500 550 600 650 650 650 650 650 1.6 1.9 2.2 2.5 3.0 3.5 4.0 4.5 5.0 5.5 6.0 7.0 8.0 0.4 0.5 0.5 0.6 0.6 0.6 0.7 0.7 0.7 0.7 0.8 0.8 0.8 0.5 0.6 0.7 0.8 0.9 0.9 1.0 1.0 1.1 1.3 1.6 1.8 2.1 350 400 450 500 575 660 750 825 N/A N/A N/A N/A N/A 100 100 110 120 130 150 170 220 N/A N/A N/A N/A N/A 90 91 92 97 100 104 107 110 N/A N/A N/A N/A N/A Pu 400°C 25 27 29 32 36 39 42 45 N/A N/A N/A N/A N/A 300 320 350 380 425 470 520 560 600 650 720 800 900 80 80 90 100 110 130 150 180 190 200 220 260 290 47 50 52 57 62 67 72 77 82 87 94 102 108 Pu 400°C 6 8 11 15 20 25 30 34 37 42 47 52 58 420 420 480 500 500 550 600 650 700 700 700 700 700 For Additional Information, Please Consult Our Engineering Staff 1-800-233-1722 11 Cavity Design - Axial Pressure RADIAL COMPRESSION G +- 0.002 0.000 E + 0.51 - 0.00 B +- 0.000 0.002 ± 0.002 ± 0.51 + 0.00 - 0.51 A ± 0.002 ± 0.51 CS 6° CALCULATIONS Cavity OD (G) Shaft OD (E) Cavity Finish Axial Load = Seal OD (B) = Seal ID (A) +2 e3 < 32 RMS (0.8 um) = Ya Note: For best results, the cavity should be lubricated with a product that is compatible with the medium to be sealed. CHARACTERISTIC VALUES CS in 0.063 0.102 0.118 0.157 0.200 0.260 mm 1.60 2.60 3.00 4.00 5.10 6.60 Aluminum Jacket e3 in 0.012 0.014 0.016 0.020 0.020 0.024 mm 0.30 0.35 0.40 0.50 0.50 0.60 Ya daN/ lb/in cm 109 19 137 24 154 27 183 32 206 36 235 41 CS in 0.063 0.102 0.122 0.165 0.205 0.244 mm 1.60 2.60 3.10 4.20 5.20 6.20 Silver Jacket e3 in 0.010 0.012 0.014 0.018 0.018 0.020 mm 0.25 0.30 0.35 0.45 0.45 0.50 Ya daN/ lb/in cm 170 30 195 34 206 36 228 40 263 46 308 54 Nickel Jacket e3 CS in 0.063 0.102 0.126 0.165 0.205 0.252 mm 1.60 2.60 3.20 4.20 5.20 6.40 in 0.008 0.010 0.012 0.016 0.016 0.018 Dimensions in inches The technical data contained herein is by way of example and should not be relied on for any specific application. Garlock Helicoflex will be pleased to provide specific technical data or specifications with respect to any customer’s particular applications. Use of the technical data or specifications contained herein without the express written approval of Garlock Helicoflex is at user’s risk and Garlock Helicoflex Garlock Helicoflex PO Box 9889 2770 The Boulevard Columbia, SC 29290 USA Phone: 1-803-783-1880 Toll Free: 1-800-233-1722 Fax: 1-803-783-4279 www.helicoflex.com www.garlock.net Cefilac, S .A. 90 rue de la Roche-du-Geai 42029 Saint-Etienne, FRANCE Phone: 011-33-4-77-43-51-00 Fax: 011-33-4-77-43-51-52 expressly disclaims responsibility for such use and the situations which may result therefrom. Garlock Helicoflex makes no warranty, express or implied, that utilization of the technology or products disclosed herein will not infringe any industrial or intellectual property rights of third parties. Garlock Helicoflex is constantly involved in engineering and development. Accordingly, Garlock Helicoflex reserves the mm 0.20 0.25 0.30 0.40 0.40 0.45 Ya daN/ lb/in cm 228 40 308 54 343 60 434 76 525 92 640 112 Dimensions in mm right to modify, at any time, the technology and product specifications contained herein. All technical data, specifications and other information contained herein is deemed to be the proprietary intellectual property of Garlock Helicoflex. No reproduction, copy or use thereof may be made without the express written consent of Garlock Helicoflex. Garlock Sealing Technologies Palmyra, NY, USA 1-315-597-4811 Paragould, AR, USA 1-870-239-4051 Houston, TX USA 1-281-459-7200 Sydney, Australia 61-2-9793-2511 S~ ao Paulo, Brazil 55-11-884-9680 Oakville, Canada 1-905-829-3200 Berkshire, England 44-1635-38509 Neuss, Germany 49-2131-3490 Seoul, Korea 822-554-6341 Mexico City, Mexico 52-5-567-7011 Singapore 65-284-7873 Fax: 1-315-597-3216 Fax: 1-870-239-4054 Fax: 1-281-458-0502 Fax: 61-2-9793-2544 Fax: 55-11-884-9680 Fax: 1-905-829-3333 Fax: 44-1635-569573 Fax: 49-2131-349-222 Fax: 822-554-6343 Fax: 52-5-368-0418 Fax: 65-284-6089 Catalog Reference: HEL 1
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