Series 7500 Formed Metal Bellows Catalog 974C

Similar documents
1. Introduction. 1.1 Overview of Study:

4. Objectives of Research work

External Pressure... Thermal Expansion in un-restrained pipeline... The critical (buckling) pressure is calculated as follows:

five Mechanics of Materials 1 ARCHITECTURAL STRUCTURES: FORM, BEHAVIOR, AND DESIGN DR. ANNE NICHOLS SUMMER 2017 lecture

Mechanics of Materials Primer

Technical Note PP TN Engineering Considerations for Temperature Change

Note to reviewers: See next page for basis for the change shown on this page. L-3160 TANGENTIAL CONTACT BETWEEN FLANGES OUTSIDE THE BOLT CIRCLE

For ASME Committee use only.

Guidelines for the Installation of SYGEF Pipes, Fittings and Valves

Design against fluctuating load

Glossary Innovative Measurement Solutions

SOLUTION (17.3) Known: A simply supported steel shaft is connected to an electric motor with a flexible coupling.

Module 7 Design of Springs. Version 2 ME, IIT Kharagpur

MODULE C: COMPRESSION MEMBERS

Where and are the factored end moments of the column and >.

U.S. Patents 6,290,217 6,244,579

MARINELLI BEAKERS CATALOG

Figure 1 Lifting Lug Geometry with Weld

411 Steel Couplings. 411 Steel Couplings--Standard Length Sleeves 1/2 thru 12 Steel Pipe Sizes. Sleeve Thk. X Lgth. In.

1.3 Working temperature T 200,0 1.4 Working environment. F... Guided seating. Light service. Cold formed springs. Music wire ASTM A228

THE EFFECT OF GEOMETRY ON FATIGUE LIFE FOR BELLOWS

Connector~Tech Providing Harsh Environment Connector

The Effects of Convolution Geometry and Boundary Condition on the Failure of Bellows

[5] Stress and Strain

flexible couplings for pipe repair

flexible couplings for pipe connections

Mechanics of Materials

Mechanics of Materials II. Chapter III. A review of the fundamental formulation of stress, strain, and deflection

MECHANICS OF MATERIALS. Prepared by Engr. John Paul Timola

MATERIALS FOR CIVIL AND CONSTRUCTION ENGINEERS

ME 243. Mechanics of Solids

THERMOWELL VIBRATION INVESTIGATION AND ANALYSIS

Sta-Saf. System. The. BSBsystems.com BSB.ie Visit our website for the most complete, up-to-date information. Reverse Buckling Technology

Part :Fill the following blanks (20 points)

Spacecraft Structures

NAME: Given Formulae: Law of Cosines: Law of Sines:

Failure in Flexure. Introduction to Steel Design, Tensile Steel Members Modes of Failure & Effective Areas

twenty one concrete construction: shear & deflection ARCHITECTURAL STRUCTURES: FORM, BEHAVIOR, AND DESIGN DR. ANNE NICHOLS SUMMER 2014 lecture

ROLLER BEARING FAILURES IN REDUCTION GEAR CAUSED BY INADEQUATE DAMPING BY ELASTIC COUPLINGS FOR LOW ORDER EXCITATIONS

Strength of Material. Shear Strain. Dr. Attaullah Shah

Downloaded from Downloaded from / 1

CWR track vibration characteristics varying with the change of supporting condition

Influence of residual stresses in the structural behavior of. tubular columns and arches. Nuno Rocha Cima Gomes

ENCE 455 Design of Steel Structures. III. Compression Members

Wake Frequency Calculations Solid Drilled Thermowells

IBV Series Z Alloy Steel Inverted Bucket Vertical Steam Trap

IBV Series C Carbon Steel Inverted Bucket Vertical Steam Trap

Parametric Study of Shaft Subjected To Pure Bending

Mechanical Properties of Materials

Steel Cross Sections. Structural Steel Design

Critical Load columns buckling critical load

UNIVERSITY OF SASKATCHEWAN ME MECHANICS OF MATERIALS I FINAL EXAM DECEMBER 13, 2008 Professor A. Dolovich

API 11E - Specification for Pumping Units

5 G R A TINGS ENGINEERING DESIGN MANUAL. MBG Metal Bar Grating METAL BAR GRATING MANUAL MBG METAL BAR GRATING NAAMM

four mechanics of materials Mechanics of Materials Mechanics of Materials Knowledge Required MECHANICS MATERIALS

EMA 3702 Mechanics & Materials Science (Mechanics of Materials) Chapter 3 Torsion

Coating Requirements for Pipelines Installed by Horizontal Directional Drilling John D. Hair, P.E.*

THREE HOLE SPLICE CLEVIS FOR B52 Standard finishes: ZN, GRN Wt./C 126 Lbs. (57.1 kg)

A Study on the Tube of Integral Propeller Shaft for the Rear-wheel Drive Automobile Using Carbon Composite Fiber

Mechanical Design in Optical Engineering. For a prismatic bar of length L in tension by axial forces P we have determined:

ME Final Exam. PROBLEM NO. 4 Part A (2 points max.) M (x) y. z (neutral axis) beam cross-sec+on. 20 kip ft. 0.2 ft. 10 ft. 0.1 ft.

Wet Tantalum Capacitors, High Energy, Ultra High Capacitance, -55 C to +125 C Operation

DEFLECTION OF BEAMS WlTH SPECIAL REFERENCE TO SHEAR DEFORMATIONS

HRN/HRN-C Series Hydraulic Vane Rotary Actuators

RESEARCH PROJECT NO. 26

DIVISION: METALS SECTION: METAL FASTENINGS SECTION: STEEL DECKING REPORT HOLDER: PNEUTEK, INC.

CIV 207 Winter For practice

PERIYAR CENTENARY POLYTECHNIC COLLEGE PERIYAR NAGAR - VALLAM THANJAVUR. DEPARTMENT OF MECHANICAL ENGINEERING QUESTION BANK

ME 2570 MECHANICS OF MATERIALS

Two Experiments to Teach Modulus of Elasticity and Modulus of Rigidity

Solid Mechanics Chapter 1: Tension, Compression and Shear

O Plus Dry Bushing 69 kv system, 350 kv BIL, 3000 A. Table of contents

Catalog # The Sta-Saf System. Reverse Buckling Technology A SME

SERVICEABILITY LIMIT STATE DESIGN

MIL-HDBK-5H 1 December 1998

Ball Reverser. Ball Reverser Actuator. FLENNOR Power Transmission Products. Patented

EXTERIOR FRAMING EXTERIOR FRAMING

The subject of this paper is the development of a design

M2 SERIES THERMOSTATS 0 F to 240 F, Narrow Differential, Hermetically Sealed ½

Structural Steelwork Eurocodes Development of A Trans-national Approach

five mechanics of materials Mechanics of Materials Mechanics of Materials Knowledge Required MECHANICS MATERIALS

4.MECHANICAL PROPERTIES OF MATERIALS

90/10 COPPER NICKEL ALLOY EUCARO 10 OFFSHORE APPLICATIONS

PLATE GIRDERS II. Load. Web plate Welds A Longitudinal elevation. Fig. 1 A typical Plate Girder

Symmetric Bending of Beams

Precision Leaded Resistors

Edward C. Robison, PE, SE. 02 January Architectural Metal Works ATTN: Sean Wentworth th ST Emeryville, CA 94608

Topic wise Tests. Complex Variables, Numerical Methods and Probability and Statistics.

Vacuum Chambers. Type DK /DK /DK

However, reliability analysis is not limited to calculation of the probability of failure.

Mechanical Forces Developed in Pianola Pneumatic Motors

Inventor 2019 lancering

D : SOLID MECHANICS. Q. 1 Q. 9 carry one mark each. Q.1 Find the force (in kn) in the member BH of the truss shown.

to introduce the principles of stability and elastic buckling in relation to overall buckling, local buckling

Quad 10GBASE-T to XAUI Converter

two structural analysis (statics & mechanics) APPLIED ACHITECTURAL STRUCTURES: DR. ANNE NICHOLS SPRING 2017 lecture STRUCTURAL ANALYSIS AND SYSTEMS

TECHNICAL CORRECTION July Process Industry Practices Structural. PIP STE03360 Heat Exchanger and Horizontal Vessel Foundation Design Guide

Lecture-08 Gravity Load Analysis of RC Structures

The University of Melbourne Engineering Mechanics

Design of Beams (Unit - 8)

Transcription:

Series 00 Formed Metal Bellows Catalog C

Innovators of the industry Bellows assemblies for safety valves, control valves, and regulators. When you look for a formed bellows which is reliable, has a long life expectancy, and is competitively priced, look to HYSPAN. Rigid quality control, modern facilities, and the fact that all operations are performed in our own plant means that you receive both quality and performance. HYSPAN Series 00 Formed Bellows are manufactured in standard sizes ranging from -inch to 0-feet inside, and for a broad spectrum of, temperature, flexibility, and movement requirements while conveying both corrosive and non-corrosive fluids. These bellows absorb axial extension and compression, parallel offset, angulation, or combinations of motions. But there s more. Our engineering assistance is available to you for your special applications or non-standard sizes. Cryogenic disconnect made from Alloy. Vacuum Applications Series 00 Bellows can be used for high-vacuum applications requiring leakage s less than x 0-0 STD ATM CC/SEC at base of x 0 - TORR. Since most of these applications require extremely flexible bellows, Hyspan recommends materials of 0.00 for inside s (I.D.) up to., 0.00 for I.D. up to.0, and 0.00 for I.D. up to. Any material Thickness can be used which has a maximum (Column on pages -) exceeding PSIG. Type stainless steel is preferred because of its weldability and availability; however, other alloys can be substituted. Bellows assembly designed to absorb expansion of oil. Beryllium Copper The beryllium copper alloys have high thermal and electrical conductivity similar to pure copper. It can be readily joined by resistance and fusion welding, brazing and soldering. The material is nonsparking, nonmagnetic; it has high galling resistance, and maintains its strength and ductility at cryogenic temperatures. Bellows can be used for high-vacuum applications. copyright 00 Hyspan Precision Products, Inc. Printed in the USA

Standard Bellows Nomenclature Hyspan Series 00 Neck Trims Thickness Neck convolution STANDARD TRIM I.D. NECK The neck and I.D. are equal to the nominal I.D Diameter (neck and convolution) Neck Trim Standard trim is 0." for " ID (#) through " ID (#) and.0" for all other sizes. Standard Tolerances Convoluted Length Outside Diameter Neck Convoluted Trim Diameter Number I.D. I.D. & O.D. Length Length - - 0.0 0.0 0.0 0.0. - - 0.0 0.0 0.0 0.0. - - 0.0 0.0 0.0 0.0. - - 0.0 0.0 0. 0.0 - - 0.0 0. 0. 0.0 0 - -0 0. 0. 0. 0. STYLE A O.D. NECK The neck O.D. is equal to the convolution O.D. STYLE B EXPANDED NECK The neck I.D. or O.D can be specified within the range of the I.D. to the convolution O.D. STYLE C O.D. TRIM The trim line is at the tangent point of the convolution O.D. STYLE D I.D. TRIM The trim line is at the tangent point of the convolution I.D. INSIDE BAND OUTSIDE BAND Tabulated tolerance is plus or minus for nominal Multiply or Laminated Bellows Any Standard-size bellows can be fabricated with multiply construction up to four plies of equal. The maximum,, and stability are increased in direct proportion to the of plies, but with the same axial deflection as a single ply. Multiply design permits a lower and a greater cycle life than a single ply configuration for an equivalent. This type of construction is recommended for applications with vibration or rapid cyclic motion because of the inherent damping provided by the relative movement of the plies. Multiply construction in not recommended for vacuum application requiring a mass spectrometer helium leak test because of possible out-gassing from an undetectable leak in an inner ply. Series 00 bellows with standard, Style A, or Style B neck trims can be specified with inside or outside bands which increase the from welding or added reinforcement. The band is approximately. times the bellows. The bands are attached by resistance seam welding for sizes through and by edge welding (GTAW) for larger sizes. Caution: The use of bands is not recommended for vacuum applications requiring a mass spectrometer helium leak test. Series 00

Explanation of Tabulated Data All dimensional data is applicable to tabulated single and multiply configurations with standard and optional materials. The tabulated performance parameters are for type stainless steel at room temperature; however, they apply to all austenitic stainless steels with minor variations. Variations for other materials are given for each column explanation. s & Properties The performance data tabulated in Columns through (pages -) was calculated for type stainless steel at 0ºF. These values are a function of the Modulus of Elasticity, strength, and fatigue life. If the service conditions are substantially different or an optional material is used, contact the factory for assistance. Optional materials can be substituted which include but are not limited to alloys 00,, 00,, Cb-0 and C-, Nickel 00, Beryllium Copper and weldable Aluminum alloys. Use of Tabulation The data included in this catalog was computed by generally accepted analytical methods and empirical data derived from tests. This data should be used as a design guide only. Consult the factory if you have an application requiring close control of these values. The following paragraph s refer to the column s of the tabulated data on pages through. Number A four or five digit identifies the nominal size (inside ), and a letter corresponds to the material. In order to fully specify the desired configuration refer to the Ordering Instructions on page. Diameter Nominal of the convolutions and the standard neck trim. Outside Diameter Nominal outside of the convolutions and maximum of Style A neck trim. Area The cross-sectional of the bellows based on the mean of convolutions. This multiplied by the equals the thrust force (Lbs.). Thickness The values tabulated are representative designs for each. Other may be available consult the factory. Convoluted Length These values are established by manufacturing limitations. Substantially longer s must be obtained by splicing two or more elements. Any shorter can be specified refer to the Ordering Instructions on page. Pressure The highest internal or external recommended with a corresponding test of. times this value. This is exclusive of the squirm or instability (Column ). The working for internally pressurized bellows is determined from the tabulated in Column, or the squirm calculated from Column whichever is lowest. For convenience Column and include a test factor of., i.e., a bellows can be pressurized to. times the tabulated in Column without permanent set, and the anticipated squirm is greater than. times the value calculated from Column. The working for internally pressurized bellows which are guided or supported to prevent squirm is determined from Column. The working for externally pressurized bellows is determined from Column squirm or instability does not occur. All bellows d at a (Column ) exceeding psi are satisfactory for Full Vacuum (internal) applications Caution This applies to the sections only and the standard neck trims. Long unsupported neck trims may collapse. Multiply or Laminated Construction multiply the values of Columns and times the of plies. copyright 00 Hyspan Precision Products, Inc. Printed in the USA

Squirm or Instability Pressure Internally pressurized bellows are unstable at the critical or squirm. In most instances this condition is characterized by the centerline of individual convolutions deviating from a common centerline analogous to buckling of a long column under compression. This condition occurs when the is long relative to the inside over or. times. There is also a less familiar type of squirm which occurs when the plane of the individual convolutions deviates from parallel planes. Either condition represents a maximum and failure will occur if is increased. The tabulated values (Column ) are the maximum recommended internal to avoid squirm for one inch of. The values are based on a test. times the tabulated. The for other s can be calculated by dividing the tabulated value by the square of the. The Column values do not need to be corrected for other materials which have a modulus of elasticity in the range of 0 x 0 psi. For multiply construction multiply the tabulated value by the of plies. Axial Spring Rate The force (Lbs.) per inch of axial extension or compression resulting from the material and configuration constant is tabulated for one inch of. The for other s is determined by dividing the tabulated values by the. Multiply this value by the of plies for multiply construction. 0 Lateral Spring Rate The force (Lbs.) per inch of the lateral offset resulting from the material and configuration constant is tabulated for one inch of. This movement occurs when the ends remain parallel to each other and perpendicular to the longitudinal centerline, but the centerline displaces laterally. The lateral for bellows other than one inch is calculated by dividing the cube of the. For multiply construction multiply by the of plies. Caution The tabulated values must be multiplied by the 000 except as noted to obtain the true. Bellows Movements Axial Deflection The allowable axial extension or compression for one inch of is tabulated for 000 cycles of movement from the nominal to the tabulated value. The movement for other s are obtained by multiplying by the required. Since these values are determined by the metal fatigue due to the bending stress produced by movement it is unchanged for multiply construction. The tabulated values can be corrected for other s of cycles (at 0ºF.) by applying the following factors: Cycles to Failure Multiply by 00.0,000.0,000.00,000 0.,000 0. 0,000 0.0 AXIAL Extension or compression from the manufactured along the longitudinal centerline with ends parallel. LATERAL Displacement perpendicular to the longitudinal centerline with the ends parallel. ANGULAR Rotation of the longitudinal centerline about the perpendicular axis. COMBINED Axial, lateral, and angular movements can be combined within the d movements. TORSION OR TWISTING AROUND THE CENTERLINE (Not recommended.) Series 00

O.D. 0 deflection,000 cycles B 0.00 0 0. 0. D 0.00 0 0 0. 0...0 G 0.00 0. 0. J 0.00 0. 0. B 0.00 0 0. 0. D 0.00 0 0. 0..0.. G 0.00 0. 0. J 0.00 0. 0. B 0.00 0 0. 0. D 0.00 0 0. 0..0.. G 0.00 0. 0. J 0.00. 0. D 0.00 0 0. 0. G 0.00 0. 0.... J 0.00. 0. K 0.0. 0. D 0.00 0 0. 0. G 0.00. 0.... J 0.00 0. 0.0 K 0.0 0. 0. D 0.00 0 0. 0. G 0.00. 0.... J 0.00 0 0. 0.0 K 0.0 0. 0. D 0.00 0 0. 0. G 0.00. 0.... J 0.00 0. 0.0 K 0.0 0. 0. 0D 0.00 0. 0. 0G 0.00.0 0.... 0J 0.00 0. 0. 0K 0.0 0 0.0 0. D 0.00 0. 0. G 0.00 0.0 0. J... 0.00.0 0. K 0.0 0. 0. L 0.0 00 0. 0. D 0.00 0 0.0 0. G 0.00. 0. J.. 0.00 0.0 0.0 K 0.0. 0. L 0.0 0. 0.0 D 0.00 0 0. 0. G 0.00. 0. J... 0.00 0. 0.0 K 0.0 00 0. 0. L 0.0 0. 0.0 copyright 00 Hyspan Precision Products, Inc. Printed in the USA

O.D. 0 deflection,000 cycles D 0.00 0. 0. G 0.00.0 0. J... 0.00. 0. K 0.0 00. 0. L 0.0 0. 0. D 0.00.00 0. G 0.00. 0. J... 0.00 0. 0. K 0.0 0.0 0. L 0.0 0 0. 0. D 0.00 0. 0. G 0.00.0 0. J... 0.00. 0. K 0.0 0. 0. L 0.0 0 0. 0. D 0.00 0 0. 0. G 0.00. 0. J... 0.00 0. 0. K 0.0. 0. L 0.0. 0. D 0.00 00 0. 0. G 0.00 00.0 0. J.. 0.00 0 00 0. 0. K 0.0 0 00. 0. L 0.0 00 0 0.0 0. D 0.00 00 0. 0. G 0.00 00 0. 0. J... 0.00 0 00. 0. K 0.0 0 000. 0. L 0.0 00 0. 0. 0D 0.00 00. 0. 0G 0.00 00.0 0. 0J... 0.00 0 00. 0. 0K 0.0 0 00. 0. 0L 0.0 00 0.0 0. D 0.00 00. 0. G 0.00 00 0.0 0. J 0.00 00. 0...0. 0 K 0.0 0 00 0. 0. L 0.0 00.0 0. N 0.0 00 0. D 0.00 00. 0. G 0.00 00 0.0 0. J 0.00 00. 0.... 0 K 0.0 0 00. 0. L 0.0 00. 0. N 0.0 00. Note *() Columns,, 0 & apply to. Refer to the explanation of tables (page ) for correction to a specific. () For the correct value of lateral (Column 0) multiply the tabulated value by 000 and apply the correction for explained on page. Series 00

O.D. 0 deflection,000 cycles D 0.00 00. 0. G 0.00 00 0.0 0. J 0.00 00. 0.... 0 K 0.0 0 00. 0. L 0.0 00 0. 0. N 0.0 00. 0. D 0.00 00. 0. G 0.00 00 0. 0. J 0.00 00.0 0.... 0 K 0.0 0 00 00.0 0. L 0.0 000. 0. N 0.0 00 0.0 0. D 0.00 00. 0. G 0.00 0 00.0 0.0 J 0.00 00. 0.... 0 K 0.0 00. 0. L 0.0 0 00 0. 0.0 N 0.0 00 0. 0. D 0.00 00 0. 0. G 0.00 00.0 0. J 0.00 00. 0.0.. 0 K 0.0 0 00. 0. L 0.0 00. 0. N 0.0 0 0. 0. D 0.00 00. 0. G 0.00 0. 0. J 0.00 0.0 0.... 0 K 0.0 0 00 0. 0. L 0.0 00 0. 0. N 0.0 0 00. 0. D 0.00 00 0. 0. G 0.00 00.0 0. J 0.00 0 00. 0...0 0. 0 K 0.0 000 0 0. 0. L 0.0 00 0. 0. N 0.0 00. 0.0 D 0.00 00. 0. G 0.00 0 00. 0. J 0.00 0 00. 0.... 0 K 0.0 00 0. 0. L 0.0 00. 0. N 0.0 00. 0.0 0D 0.00 00. 0. 0G 0.00 0 00 0. 0. 0J 0.00 0 00. 0. 0K... 0.0 0 00. 0. 0L 0.0 00. 0. 0N 0.0 00. 0. 0R 0.0 00 0. 0. copyright 00 Hyspan Precision Products, Inc. Printed in the USA

O.D. 0 deflection,000 cycles D 0.00.0 0. G 0.00 0 0. 0. J 0.00. 0. K... 0.0 0 00 0. 0. L 0.0.0 0.0 N 0.0.0 0. R 0.0 00 0. 0. D 0.00 00. 0. G 0.00 00.0 0. J 0.00 00.0 0. K... 0.0 0 000. 0. L 0.0 00.00 0.0 N 0.0 00.0 0. R 0.0 00 0.0 0. D 0.00 00 0. 0. G 0.00 00. 0. J 0.00 00. 0. K... 0.0 0 00. 0. L 0.0 00. 0.0 N 0.0 00. 0. R 0.0 000. 0. D 0.00 00 0. 0. G 0.00 00.0 0. J 0.00 00 0. 0. K. 0.0 0 00 0. 0. L 0.0 00. 0. N 0.0 00.0 0. R 0.0 00.0 0. D 0.00 00 0. 0. G 0.00 00. 0. J 0.00 00.0 0. K... 0.0 0 00 0.0 0. L 0.0 00.0 0. N 0.0 00. 0. R 0.0 00 0. 0. D 0.00 00 0. 0. G 0.00 00. 0. J 0.00 00. 0. K... 0.0 0 00 0. 0. L 0.0 00 0 0. 0. N 0.0 00. 0. R 0.0 00. 0. D 0.00 00 0. 0. G 0.00 00. 0. J 0.00 00. 0. K... 0.0 0 00. 0. L 0.0 00.0 0. N 0.0 000 0. 0. R 0.0 00. 0. Note *() Columns,, 0 & apply to. Refer to the explanation of tables (page ) for correction to a specific. () For the correct value of lateral (Column 0) multiply the tabulated value by 000 and apply the correction for explained on page. Series 00

O.D. 0 deflection,000 cycles G 0.00 00 0 0. 0. J 0.00 00 0.0 0. K 0.0 00 0 0. 0.... 0 L 0.0 00. 0. N 0.0 00 00. 0. R 0.0 00. 0. G 0.00 00 0. 0. J 0.00 00. 0. K 0.0 000. 0... 0. 0 L 0.0 00. 0. N 0.0 00 0. 0. R 0.0 00. 0. 0G 0.00 00. 0. 0J 0.00 00. 0. 0K 0.0 000. 0.... 0 0L 0.0 00. 0. 0N 0.0 00 0.0 0. 0R 0.0 00. 0. G 0.00 00. 0. J 0.00 00. 0. K 0.0 000. 0.... 0 L 0.0 00 0.0 0. N 0.0 00. 0. R 0.0 00. 0. G 0.00 00. 0. J 0.00 00.0 0. K 0.0 000 0 0. 0.. 0 L 0.0 00. 0. N 0.0 00.0 0. R 0.0 00 0. 0. G 0.00 00. 0. J 0.00 00. 0. K 0.0 00. 0. L... 0.0 0 0 00. 0. N 0.0 00 0 0. 0. R 0.0 00 0. 0. S 0.00 00 0.0 0. G 0.00 00. 0. J 0.00 00. 0. K 0.0 00.0 0.0 L... 0.0 0 0 00. 0. N 0.0 00.0 0. R 0.0 00 0.0 0. S 0.00 00. 0. G 0.00 0. 0. J 0.00 0.0 0. K 0.0 00 0. 0.0 L... 0.0 0 0 00. 0. N 0.0 00. 0. R 0.0 000 0.0 0. S 0.00 00. 0. 0 copyright 00 Hyspan Precision Products, Inc. Printed in the USA

O.D. 0 deflection,000 cycles G 0.00 00.0 0. J 0.00 0 00. 0. K 0.0 00 0 0. 0. L.. 0. 0.0 0 00. 0. N 0.0 000. 0. R 0.0 000 0.0 0. S 0.00 00 00. 0. G 0.00 00. 0. J 0.00 00. 0. K 0.0 00 0. 0. L.. 0.0 0 00 0. 0. N 0.0 0 00 0. 0. R 0.0 000. 0. S 0.00 00. 0. G 0.00 00 0. 0. J 0.00 00. 0. K 0.0 00 0.0 0. L... 0.0 0 00. 0. N 0.0 0 00. 0. R 0.0 000 0. 0. S 0.00 00 0.0 0. G 0.00 00.0 0. J 0.00 00.0 0. K 0.0 00 0. 0. L.. 0.0 0 000.0 0. N 0.0 0 000 0. 0. R 0.0 000 00. 0. S 0.00 00. 0. 0G 0.00 00. 0. 0J 0.00 00 0. 0. 0K 0.0 00. 0. 0L.. 0. 0.0 0 000. 0. 0N 0.0 0 00 0. 0. 0R 0.0 000 0 0. 0. 0S 0.00 00 0. 0. G 0.00 00 0.0 0. J 0.00 00. 0. K 0.0 00. 0. L... 0.0 0 000. 0. N 0.0 0 00. 0. R 0.0 000. 0. S 0.00 00 0. 0. G 0.00 00. 0. J 0.00 00. 0. K 0.0 00 00. 0. L.. 0.0 0 00. 0. N 0.0 0 00 0.0 0. R 0.0 00 0. 0. S 0.00 000 0. 0. Note *() Columns,, 0 & apply to. Refer to the explanation of tables (page ) for correction to a specific. () For the correct value of lateral (Column 0) multiply the tabulated value by 000 and apply the correction for explained on page. Series 00

O.D. 0 deflection,000 cycles G 0.00 00 0. 0. J 0.00 00. 0. K 0.0 000. 0. L.. 0. 0.0 0 00. 0. N 0.0 00. 0. R 0.0 00. 0. S 0.00 0 00. 0. G 0.00 00 0. 0. J 0.00 00. 0. K 0.0 000 0 0. 0. L.. 0.0 0 00 0.0 0. N 0.0 00. 0. R 0.0 00. 0. S 0.00 00. 0. G 0.00 00 0. 0. J 0.00 00. 0. K 0.0 00. 0. L... 0.0 0 00. 0. N 0.0 00. 0. R 0.0 00 000. 0. S 0.00 00 0.0 0. G 0.00 00. 0. J 0.00 00 0. 0. K 0.0 00. 0. L... 0.0 0 00 0. 0. N 0.0 00 00. 0. R 0.0 00 0. 0. S 0.00 00 00.0 0. G 0.00 00 0. 0. J 0.00 00. 0. K 0.0 00 00.0 0. L... 0.0 0 00.0 0. N 0.0 00.0 0. R 0.0 00 0. 0. S 0.00 00.0 0. J 0.00 00 0. 0. K 0.0 00 0. 0. L 0.0 00 0. 0.. 0 0 N 0.0 00. 0. R 0.0 00.0 0. S 0.00 000 0. 0. J 0.00 00. 0. K 0.0 00 0. 0. L 0.0 00 0. 0. 0.. 0 N 0.0 00.0 0. R 0.0 00 0. 0. S 0.00 000 00. 0. 0J 0.00 00 00. 0. 0K 0.0 00 0. 0. 0L 0.0 00 0. 0.. 0. 0. 0 0N 0.0 00.0 0. 0R 0.0 00 0.0 0. 0S 0.00 00. 0. copyright 00 Hyspan Precision Products, Inc. Printed in the USA

O.D. 0 deflection,000 cycles J 0.00 0. 0. K 0.0 0. 0. L 0.0 0 0.0 0. 0. N 0.0 0. 0. R 0.0 0. 0. S 0.00 0.0 0. J 0.00 0.0 0. K 0.0 0. 0. L 0.0 0.0 0. 0.. N 0.0 0. 0. R 0.0 0 0. 0. S 0.00. 0. J 0.00 0 0. 0. K 0.0 0. 0. L 0.0 0. 0. 0.. N 0.0. 0. R 0.0 0. 0. S 0.00. 0. J 0.00. 0. K 0.0.0 0. L 0.0 0 0. 0. N 0. 0 0.0. 0. R 0.0 00 0. 0. S 0.00 0 0. 0. T 0.0 00 0 0. 0. J 0.00 0. 0. K 0.0 0. 0. L 0.0 0. 0. N. 0 0.0 0 0. 0. R 0.0 0 0 0. 0. S 0.00 0.0 0. T 0.0 00. 0. J 0.00. 0. K 0.0 0.0 0. L 0.0 0 00. 0. N.. 0.0 00. 0. R 0.0 0 0. 0. S 0.00 0 0. 0. T 0.0 00 0. 0. J 0.00.0 0. K 0.0 0. 0. L 0.0 0 0. 0. N. 0.0 0. 0. R 0.0 0 00. 0. S 0.00. 0. T 0.0 00. 0. Note *() Columns,, 0 & apply to. Refer to the explanation of tables (page ) for correction to a specific. () For the correct value of lateral (Column 0) multiply the tabulated value by 000 and apply the correction for explained on page. Series 00

O.D. 0 deflection,000 cycles J 0.00 0 0 0. 0. K 0.0 00. 0. L 0.0 00. 0. N.. 0 0.0 000 0. 0. R 0.0 00 0.0 0. S 0.00 00 0.0 0. T 0.0 00 0.0 0. J 0.00. 0. K 0.0.0 0. L 0.0 0 0.0 0. N. 0.0 0. 0. R 0.0 0. 0. S 0.00. 0. T 0.0 000. 0. 0J 0.00. 0. 0K 0.0.0 0. 0L 0.0. 0. 0N.. 0.0. 0. 0R 0.0 00. 0. 0S 0.00 0.0 0. 0T 0.0 0 00 0. 0. N 0.0 0 00 0. 0. R 0.0 0. 0. S. 0 0.00 00. 0. T 0.0.0 0. W 0.0 000.00 0.0 N 0.0 0 0 0 0. R 0.0 00 0. S. 0 0.00 0 0 0. T 0.0 0 0. X 0.0 0 0 0.0 N 0.0 0. R 0.0 0. S 0.00 0. 0. T 0.0 0 0. W 0.00 0 0 0 0. X 0.0 0 0. N 0.0 0 0 0. R 0.0 0 0 0. S 0.00 0 0.0 T 0. 0.0 00 0 0. W 0.00 0. X 0.0 0 0. Z 0.00 0 0 0. Note *() Columns,, 0 & apply to. Refer to the explanation of tables (page ) for correction to a specific. () For the correct value of lateral (Column 0) multiply the tabulated value by 000 and apply the correction for explained on page. copyright 00 Hyspan Precision Products, Inc. Printed in the USA

O.D. 0 deflection,000 cycles N 0.0 0. R 0.0 0 0 0. S 0.00 0 00 0. T. 0.0 0 0 0. W 0.00 0 0. X 0.0 00 0 0. Z 0.00 0. N 0.0 00 0 0. R 0.0 0 0. S 0.00 0 00 0. T. 00 0.0 0 0. W 0.00 0 0. X 0.0 0. Z 0.00 0 0. N 0.0 00 0. R 0.0 00 0. S 0.00 0 0 0. T. 0.0 00 0 0. W 0.00 00 0 0. X 0.0 0 0. Z 0.00 0 0 0. N 0.0 0 0 0. R 0.0 0. S 0.00 0 0 0. T 0. 0.0 0. W 0.00 0 0 0. X 0.0 0.0 Z 0.00 0 0 0 0. N 0.0 0 0. R 0.0 0 00 0. S 0.00 0 0.0 T 0. 0.0 0 0 0. W 0.00 00 0.0 X 0.0 0. Z 0.00 00 0. 0N 0.0 0 0 0. 0R 0.0 0 0. 0S 0.00 000 0.0 0T. 0.0 0 0. 0W 0.00 0 0 0. 0X 0.0 0. 0Z 0.00 0 0. N 0.0 0 0. R 0.0 0. S 0.00 0.0 T. 0.0 00 0 0. W 0.00 00 0 0. X 0.0 00 00 0. Z 0.00 0 0 0. Series 00

O.D. 0 deflection,000 cycles N 0.0 00 0. R 0.0 0 0. S 0.00 0 0 0.0 T. 0 0.0 0 0 0. W 0.00 00 0 0. X 0.0 00 0. Z 0.00 00 0. N 0.0 00 0 0. R 0.0 00 0 0. S 0.00 0.0 T 0. 0.0 000 0 0 0. W 0.00 00 0 0. X 0.0 0 0. Z 0.00 0 0 0. N 0.0 00 0 0. R 0.0 00 0 0. S 0.00 00 0.0 T 0. 0.0 0 0. W 0.00 0 0 0 0. X 0.0 0 0 0. Z 0.00 0 0 0. N 0.0 00 0 0. R 0.0 0 0. S 0.00 0.0 T. 0.0 0 0. W 0.00 00 00 0 0. X 0.0 0 0. Z 0.00 0 00 00 0. R 0.0 0 0 0. S 0.00 0 0 0.0 T 0.0 00 0.. W 0.00 0 0. X 0.0 0 0. Z 0.00 0 0 0. R 0.0 0 0. S 0.00 0. T 0.0 0 0.. W 0.00 0 0. X 0.0 00 00 0. Z 0.00 0 0 0. R 0.0 00 0. S 0.00 0. T 0.0 0 0. W 0.00 000 0 0 0. X 0.0 00 0 0. Z 0.00 00 0 0.0 S 0.00 0. T 0.0 0 0. W 0 0 0.00 0 0. X 0.0 0 0. Z 0.00 0 0 0.0 Note **() Columns,, 0 & apply to. Refer to the explanation of tables (page ) for correction to a specific. **() For the correct value of lateral (Column 0) multiply the tabulated value by 000 and apply the correction for explained on page. **() For the correct value of lateral multiply these values by 0,000 and apply the correction for explained on page. copyright 00 Hyspan Precision Products, Inc. Printed in the USA

O.D. 0 deflection,000 cycles 00S 0.00 00 0. 00T 0.0 0. 00W 0.00 0. 00X 0.0 0 0 00 0. 00Z 0.00 0 0.0 0S 0.00 00 0. 0T 0.0 00 0. 0W 0.00 0 0 0. 0X 0.0 0 00 00 0. 0Z 0.00 00 0.0 0S 0.00 00 0. 0T 0.0 0 00 0. 0W 0.00 0 0 0. 0X 0.0 000 0 0. 0Z 0.00 0 0.0 0S 0.00 0 0 0. 0T 0.0 0 0. 0W 0 0.00 0. 0X 0.0 0 0. 0Z 0.00 0 00 0.0 0S 0.00 0 0. 0T 0.0 0 0. 0W 0.00 0 0. 0X 0.0 0 00 0 0. 0Z 0.00 00 0 0** 0.0 0S 0.00 0 0. 0T 0.0 00 0. 0W 0.00 0 0 00 0. 0X 0.0 0. 0Z 0.00 ** 0.0 0S 0.00 0 0. 0T 0.0 0 0. 0W 0 0.00 0. 0X 0.0 0. 0Z 0.00 ** 0. 0S 0.00 0 0. 0T 0.0 0 00 0. 0W 0 0.00 0. 0X 0.0 00 00 0. 0Z 0.00 0 0. 0S 0.00 00 0 0. 0T 0.0 00 0 0. 0W 0 0.00 00 0. 0X 0.0 00 00 0. 0Z 0.00 00 0 ** 0. 0S 0.00 00 0. 0T 0.0 00 0. 0W 00 0.00 00 0. 0X 0.0 00 0 0. 0Z 0.00 00 0** 0. Series 00

Three bellows and linkage designed to react thrust while allowing axial, lateral, and angular motion. This design is referred to as a In-Line Pressure Balanced Universal Gimbal, and is patented by Hyspan (U.S. Patent No. 0). This design is referred to as a gimbaled joint. A single assembly is capable of angular motion, two assemblies in tandem allow lateral and angular displacement, and the addition of a third assembly allows universal movement. The assembly shown was used in a laser research project. Bellows are commonly used in engine manifolds to absorb the thermal expansion between the rigid branch connections. The manifold shown is for a diesel engine. The thrust of the large in-line bellows is balanced by the thrust of the four bellows capsules. This configuration is capable of axial extension or compression without thrust. It was designed for a laser research application. Bellows assembly designed for medical devices. Stainless steel bellows and flanges. The center flange is floating and made of copper. Series 00

Hyspan Precision Products, Inc. Brandywine Avenue Chula Vista, CA Tel: () - Fax: () -0 www.hyspan.com