This invention relates to gaskets and seals for providing sealed connections between components.
Seals and gaskets are employed in various components to prevent fluids from leaking outside of the component and to prevent contaminants from entering the component. The performance of a seal depends upon the geometry of the seal and the material comprising the seal. Accordingly, a seal geometry that meets performance objectives with one material may not meet performance objectives with another material. Exemplary performance objectives include contact pressure, contact width, and strain limits.
A seal includes a seal body having an outer surface that conforms to a profile tolerance of 0.2 millimeters of an ideal surface geometry. The ideal surface geometry has first, second, third, fourth, fifth, and sixth points thereon. The ideal surface geometry also has first, second, third, fourth, and fifth segments, and is characterized by a first plane of symmetry and a second plane of symmetry. The first plane of symmetry intersects the ideal surface geometry at the first point, and the second plane of symmetry, which is substantially perpendicular to the first plane of symmetry, intersects the ideal surface geometry at the sixth point.
The first segment is an arc that has a radius of 17.50 millimeters and that connects the first point and the second point. The second segment is linear, has a length of 1.68 millimeters, and connects the second point to the third point. The third segment is an arc that has a radius of 2.40 millimeters, and that connects the third point to the fourth point. The fourth segment is an arc that has a radius of 0.66 millimeters, and that connects the fourth point to the fifth point. The fifth segment is an arc that has a radius of 2.20 millimeters, and that connects the fifth point to the sixth point.
The seal provided herein meets performance objectives for at least twenty-five different elastomer compositions and formulations. Accordingly, the seal provided herein provides a standardized design that may be used across a wide variety of applications and in a wide variety of operating environments, thereby eliminating the engineering and testing costs that may be associated with prior art seals.
According to another aspect of the disclosure, a seal body has an outer surface that conforms to a profile tolerance of 0.2 millimeters of an ideal surface geometry. The ideal surface geometry has first, second, third, fourth, fifth, sixth, and seventh points thereon, and has first, second, third, fourth, fifth, and sixth segments. A first plane of symmetry intersects the ideal surface geometry at the first point, and a second plane of symmetry, which is substantially perpendicular to the first plane of symmetry, intersects the ideal surface geometry at the seventh point.
The first segment is linear, has a length of 1.220 millimeters, and connects the first point and the second point. The second segment is an arc having a radius of 3.000 millimeters, and connects the second point to the third point. The third segment is linear, has a length of 1.450 millimeters, and connects the third point to the fourth point. The fourth segment is an arc having a radius of 1.430 millimeters, and connects the fourth point to the fifth point. The fifth segment is an arc having a radius of 0.645 millimeters, and connects the fifth point to the sixth point. The sixth segment is an arc having a radius of 1.890 millimeters, and connects the sixth point to the seventh point.
The above features and advantages and other features and advantages of the present invention are readily apparent from the following detailed description of the best modes for carrying out the invention when taken in connection with the accompanying drawings.
Referring to
The first and second planes 26, 30 of symmetry are perpendicular to one another. The two points 34, 38 of the ideal surface geometry that are in plane 26 are 2.52 millimeters apart, i.e., the width of the seal 10 having the ideal surface geometry is 2.52 millimeters. The two points 40, 42 of the ideal surface geometry that are in plane 30 are 7.82 millimeters apart, i.e., the height of the seal 10 having the ideal surface geometry is 7.82 millimeters.
Referring to
The remainder of the ideal surface geometry can be determined by the ideal surface geometry between points 34 and 40 because of the symmetry about planes 26 and 30. More specifically, and with reference to
A segment 44C of the ideal surface geometry connects point 34 to point 46C, and is an arc characterized by a radius of 17.50 millimeters. Linear segment 48C of the ideal surface geometry connects point 46C to point 50C and is characterized by a length of 1.68 millimeters. Segment 52C of the ideal surface geometry connects point 50C to point 54C, and is an arc characterized by a radius of 2.4 millimeters. Segment 56C of the ideal surface geometry connects point 54C to point 58C and is an arc characterized by a radius of 0.66 millimeters. Segment 60C of the ideal surface geometry connects point 58C to point 42, and is an arc characterized by a radius of 2.20 millimeters.
Segment 44D of the ideal surface geometry connects point 38 to point 46D, and is an arc characterized by a radius of 17.50 millimeters. Linear segment 48D of the ideal surface geometry connects point 46D to point 50D and is characterized by a length of 1.68 millimeters. Segment 52D of the ideal surface geometry connects point 50D to point 54D, and is an arc characterized by a radius of 2.4 millimeters. Segment 56D of the ideal surface geometry connects point 54D to point 58D and is an arc characterized by a radius of 0.66 millimeters. Segment 60D of the ideal surface geometry connects point 58D to point 42, and is an arc characterized by a radius of 2.20 millimeters.
Referring to
Referring to
As shown in
Referring to
The first and second planes 26, 30 of symmetry are perpendicular to one another. Planes 26 and 30 bisect the seal 10A. Plane 26 intersects the surface 22A at two points 64, 68. Plane 30 intersects the surface 22A at two points, only one of which is shown at 72. The distance L3 from plane 26 to point 72 is 3.914 millimeters. Thus, seal 10A with the ideal surface geometry has a total height of 7.828 millimeters. The distance L4 from plane 30 to point 68 is 1.205 millimeters. Thus, the seal 10A with the ideal surface geometry has a total width of 2.410 millimeters.
A segment 76 of the ideal surface geometry connects point 68 to point 80. Segment 76 is linear and is characterized by a length L5 of 1.220 millimeters. Segment 84 of the ideal surface geometry connects point 88 to point 80, and is an arc characterized by a radius R5 of 3.000 millimeters. Linear segment 92 of the ideal surface geometry connects point 88 to point 96 and is characterized by a length L6 of 1.450 millimeters. Segment 100 of the ideal surface geometry connects point 96 to point 104, and is an arc characterized by a radius R6 of 1.430 millimeters. Segment 108 of the ideal surface geometry connects point 104 to point 112 and is an arc characterized by a radius R7 of 0.645 millimeters. Segment 116 of the ideal surface geometry connects point 112 to point 72, and is an arc characterized by a radius R8 of 1.890 millimeters. The ideal surface geometry at point 72 is substantially parallel to plane of symmetry 26. The remainder of the ideal surface geometry of seal 10A can be determined by the ideal surface geometry between points 68 and 72 because of the symmetry about planes 26 and 30.
The dimensions of the seals 10, 10A are such that the seals 10, 10A meet a wide variety of sealing performance objectives with a wide variety of elastomer material compositions. For example, seals 10, 10A may comprise ethylene propylene diene monomer (EPDM), fluoroelastomers, alkyl acrylate copolymer, nitrile butadiene rubber (NBR), ethylene acrylic elastomer, etc. Those skilled in the art will recognize other elastomers that may be employed within the scope of the claimed invention.
Referring to
Segment 132 is partially coextensive with line 142. Lines 136 and 142 intersect at point 146. Point 146 is a distance L7 of 1.330 millimeters from plane of symmetry 26. Segments 128 and 132 form an angle α1 of 135 degrees therebetween. A segment 150 of surface 22A is an arc that extends between segments 128 and 132. Segment 150 is characterized by a radius R9 of 0.500 millimeters. Segment 154 of surface 22A is an arc that extends on the opposite side of segment 132 from segment 150. Segment 154 is characterized by a radius R10 of 0.500 millimeters.
The retention feature 120 includes segments 128, 150, 132, and 154. The seal 10A is symmetrical about plane 26, and thus the geometry of the retention feature 120 on the opposite side of plane 26 can be determined by the geometry of segments 128, 150, 132, and 154. The seal 10A, being symmetrical about plane 30, includes two retention features, as shown in
Segment 162 is partially coextensive with line 170. Lines 166 and 170 intersect at point 174. Point 174 is a distance L9 of 1.680 millimeters from plane of symmetry 26. Segments 158 and 162 form an angle a2 of 135 degrees therebetween. A segment 178 of surface 22A is an arc that extends between segments 158 and 162. Segment 178 is characterized by a radius R11 of 0.500 millimeters. Segment 182 of surface 22A is an arc that extends on the opposite side of segment 162 from segment 178. Segment 182 is characterized by a radius R12 of 0.500 millimeters.
The stabilization feature 124 includes segments 158, 178, 162, and 182. The seal 10A is symmetrical about plane 26, and thus the geometry of the stabilization feature 124 on the opposite side of plane 26 can be determined by the geometry of segments 158, 178, 162, and 182. The seal 10A, being symmetrical about plane 30, includes two stabilization features on opposite sides of plane 30, as shown in
While the best modes for carrying out the invention have been described in detail, those familiar with the art to which this invention relates will recognize various alternative designs and embodiments for practicing the invention within the scope of the appended claims.