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CHAPTER 22
SEAL TECHNOLOGY
Bruce M. Steinetz
NASA Lewis Research Center
Cleveland, Ohio
22.1 INTRODUCTION
629
22.3 DYNAMICSEALS
638
22.3.1 Initial Seal Selection
638
22.2 STATICSEALS
629
22.3.2 Mechanical Face Seals
642
22.2.1 Gaskets
629
22.3.3 Emission Concerns
644
22.2.2 O-Rings
634
22.3.4 Noncontacting Seals for
High-Speed/Aerospace
Applications
22.2.3 Packings and Braided
Rope Seals
637
646
22.3.5 Labyrinth Seals
650
22.3.6 Honeycomb Seals
653
22.3.7 Brush Seals
654
22.1 INTRODUCTION
Seals are required to fulfill critical needs in meeting the ever-increasing system-performance re-
quirements of modern machinery. Approaching a seal design, one has a wide range of available seal
choices. This chapter aids the practicing engineer in making an initial seal selection and provides
current reference material to aid in the final design and application.
This chapter provides design insight and application for both static and dynamic seals. Static seals
reviewed include gaskets, O-rings, and selected packings. Dynamic seals reviewed include mechanical
face, labyrinth, honeycomb, and brush seals. For each of these seals, typical configurations, materials,
and applications are covered. Where applicable, seal flow models are presented.
22.2 STATICSEALS
22.2.1 Gaskets
Gaskets are used to effect a seal between two mating surfaces subjected to differential pressures.
Gasket types and materials are limited only by one's imagination. Table 22.1 lists some common
gasket materials and Table 22.2 1 lists common elastomer properties. The following gasket character-
istics are considered important for good sealing performance. 2 Selecting the gasket material that has
the best balance of the following properties will result in the best practical gasket design.
Chemical compatibility
Heat resistance
Compressibility
Microconformability (asperity sealing)
Recovery
Creep relaxation
Erosion resistance
Compressive strength (crush resistance)
Tensile strength (blowout resistance)
Shear strength (flange shearing movement)
Removal or "Z" strength
Mechanical Engineers' Handbook, 2nd ed., Edited by Myer Kutz.
ISBN 0-471-13007-9 © 1998 John Wiley & Sons, Inc.
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Table 22.1 Common Gasket Materials, Gasket Factors (m) and Minimum Design Seating
Stress (y) (Table 2-5.1 ASME Code for Pressure Vessels, 1995)
Min.
Design
Seating
Stress y,
psi
Gasket
Factor
m
Gasket Material
Sketches
Self-energizing types (O-rings,
metallic, elastomer, other
gasket types considered as self-
sealing)
Elastomers without fabric or high
percent of asbestos fiber:
Below 75A Shore Durometer
75A or higher Shore Durometer
Asbestos with suitable binder for
operating conditions:
Vs in. thick
Vi6 in. thick
!/32 in. thick
Elastomers with cotton fabric
insertion
O
O
0.50
1.00
O
200
2.00
2.75
3.50
1.25
1600
3700
6500
400
Elastomers with asbestos fabric
insertion (with or without wire
reinforcement):
3-ply
2.25
2200
2.50
2-ply
1-ply
2900
3700
2.75
Vegetable fiber
1.75
1100
Spiral-wound metal, asbestos
filled:
Carbon
Stainless, Monel, and nickel-
base alloys
Corrugated metal, asbestos
inserted, or corrugated metal,
jacketed asbestos filled:
Soft aluminum
Soft copper or brass
Iron or soft steel
Monel or 4%-6% chrome
Stainless steels and nickel-base
alloys
Corrugated metal:
Soft aluminum
Soft copper or brass
Iron or soft steel
Monel or 4%-6% chrome
Stainless steels and nickel-base
alloys
2.50
3.00
10,000
10,000
2.50
2.75
3.00
3.25
3.50
2900
3700
4500
5500
6500
2.75
3.00
3.25
3.50
3.75
3700
4500
5500
6500
7600
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Table 22.1 (Continued)
Min.
Design
Seating
Stress y,
psi
Gasket
Factor
/77
Gasket Material
Flat metal, jacketed asbestos
filled:
Soft aluminum
Soft copper or brass
Iron or soft steel
Monel
4%-6% chrome
Stainless steels and nickel-base
alloys
Grooved metal:
Soft aluminum
Soft copper or brass
Iron or soft steel
Monel or 4%-6% chrome
Stainless steels and nickel-base
alloys
Solid flat metal:
Soft aluminum
Soft copper or brass
Iron or soft steel
Monel or 4%— 6% chrome
Stainless steels and nickel-base
alloys
Ring joint:
Iron or soft steel
Monel or 4%-6% chrome
Stainless steels and nickel-base
alloys
Sketches
3.25
3.50
3.75
3.50
3.75
3.75
5500
6500
7600
8000
9000
9000
5500
6500
7600
9000
10,100
3.25
3.50
3.75
3.75
4.25
4.00
4.75
5.50
6.00
6.50
8800
13,000
18,000
21,800
26,000
5.50
6.00
6.50
18,000
21,800
26,000
• Antistick
• Heat conductivity
• Acoustic isolation
• Dimensional stability
Nonmetallic Gaskets. Most nonmetallic gaskets consist of a fibrous base held together with
some form of an elastomeric binder. A gasket is formulated to provide the best load-bearing properties
while being compatible with the fluid being sealed.
Nonmetallic gaskets are often reinforced to improve torque retention and blowout resistance for
more severe service requirements. Some types of reinforcements include perforated cores, solid cores,
perforated skins, and solid skins, each suited for specific applications. After a gasket material has
been reinforced by either material additions or laminating, manufacturers can emboss the gasket
raising a sealing lip, which increases localized pressures, thereby increasing scalability.
Metallic Gaskets. Metallic gaskets are generally used where either the joint temperature or load
is extreme or in applications where the joint might be exposed to particularly caustic chemicals. A
good seal capable of withstanding very high temperature is possible if the joint is designed to yield
locally over a narrow location with application of bolt load. Some of the most common metallic
gaskets range from soft varieties, such as copper, aluminum, brass, and nickel, to highly alloyed
steels. Noble metals, such as platinum, silver, and gold, also have been used in difficult locations.
Metallic gaskets are available in both standard and custom designs. Since there is such a wide
variety of designs and materials used, it is recommended that the reader directly contact metallic
gasket suppliers for design and sealing information.
Required Bolt Load
ASME Method. The ASME Code for Pressure Vessels, Section VIII, Div. 1, App. 2, is the most
commonly used design method for gasketed joints where important joint properties, including flange
thickness, bolt size and pattern, are specified. Because of the absence of leakage considerations, it
815046965.006.png
should be noted that the ASME is currently evaluating the Pressure Vessel Research Council's method
for gasket design. It is likely that a nonmandatory appendix to the Code will appear first (see dis-
cussion in Ref. 3).
An integral part of the AMSE Code revolves around two gasket factors:
1. An m factor, often called the gasket-maintenance factor, is associated with the hydrostatic
end force and the operation of the joint.
2. The y factor is a rough measure of the minimum seating stress associated with a particular
gasket material. The y factor pertains only to the initial assembly of the joint.
The ASME Code makes use of two basic equations to calculate bolt load, with the larger calculated
load being used for design:
W ml = H + H p = - G 2 P + 2TTbGmP
W m2 = H y = TTbGy
where W ml = minimum required bolt load from maximum operating or working conditions, Ib
W m2 = minimum required initial bolt load for gasket seating (atmospheric-temperature con-
ditions) without internal pressure, Ib
H = total hydrostatic end force, Ib [(TrM)G 2 P]
H p = total joint-contact-surface compression load, Ib
Hy = total joint-contact-surface seating load, Ib
G = diameter at location of gasket load reaction; generally defined as follows: When b 0 <
1 A in., G = mean diameter of gasket contact face, in.; When b Q > 14 in., G = outside
diameter of gasket contact face less 2b, in.
P = maximum internal design pressure, psi
b = effective gasket or joint-contact-surface seating width, in.
b = b 0 when b 0 ^ 1 A in.
b = 0.5Vb 0 when b 0 > 1 A in.
2b = effective gasket or joint-contact-surface pressure width, in.
b Q = basic gasket seating width per ASME Table 2-5.2. The table defines b 0 in terms of
flange finish and type of gasket, usually from one-half to one-fourth gasket contact
width
m = gasket factor per ASME Table 2-5.1 (repeated here as Table 22.1).
y = gasket or joint-contact-surface unit seating load, per ASME Table 2-5.1 (repeated here
as Table 22.1), psi
The factor m provides a margin of safety to be applied when the hydrostatic end force becomes
a determining factor. Unfortunately, this value is difficult to obtain experimentally since it is not a
constant. The equation for W m2 assumes that a certain unit stress is required on a gasket to make it
conform to the sealing surfaces and be effective. The second empirical constant y represents the
gasket yield-stress value and is very difficult to obtain experimentally.
Practical Considerations
Flange Surfaces. Preparing the flange surfaces is paramount for effecting a good gasket seal.
Surface finish affects the degree of scalability. The rougher the surface, the more bolt load required
to provide an adequate seal. Extremely smooth finishes can cause problems for high operating pres-
sures, as lower frictional resistance leads to a higher tendency for blowout. Surface finish lay is
important in certain applications to mitigate leakage. Orienting finish marks transverse to the normal
leakage path will generally improve scalability.
Flange Thickness. Flange thickness must also be sized correctly to transmit bolt clamping load
to the area between the bolts. Maintaining seal loads at the midpoint between the bolts must be kept
constantly in mind. Adequate thickness is also required to minimize the bowing of the flange. If the
flange is too thin, the bowing will become excessive and no bolt load will be carried to the midpoint,
preventing sealing.
Bolt Pattern. Bolt pattern and frequency are critical in effecting a good seal. The best bolt
clamping pattern is invariably a combination of the maximum practical number of bolts, optimum
spacing, and positioning.
One can envision the bolt loading pattern as a series of straight lines drawn from bolt to adjacent
bolt until the circuit is completed. If the sealing areas lie on either side of this pattern, it will likely
be a potential leakage location. Figure 22.1 shows an example of the various conditions. 2 If bolts
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Fig. 22.1 Bolting pattern indicating poor sealing areas. (From Ref. 2.)
cannot be easily repositioned on a problematic flange, Fig. 22.2 illustrates techniques to improve
gasket effectiveness through reducing gasket face width where bolt load is minimum. Note that gasket
width is retained in the vicinity of the bolt to support local bolt loads and minimize gasket tearing.
Gasket Thickness and Compressibility. Gasket thickness and compressibility must be matched
to the rigidity, roughness, and unevenness of the mating flanges. An effective gasket seal is achieved
only if the stress level imposed on the gasket at installation is adequate for the specific gasket and
joint requirements.
Original gasket:
Redesigned gasket
gasket identical
to casting flange
Fig. 22.2 Original vs. redesigned gasket for improved sealing. (From Ref. 2.)
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