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WO2015069829A1 - Joint d'étanchéité à matériaux dissemblables - Google Patents

Joint d'étanchéité à matériaux dissemblables Download PDF

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Publication number
WO2015069829A1
WO2015069829A1 PCT/US2014/064226 US2014064226W WO2015069829A1 WO 2015069829 A1 WO2015069829 A1 WO 2015069829A1 US 2014064226 W US2014064226 W US 2014064226W WO 2015069829 A1 WO2015069829 A1 WO 2015069829A1
Authority
WO
WIPO (PCT)
Prior art keywords
profile
gasket
track
recess
joining portion
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/US2014/064226
Other languages
English (en)
Inventor
Christopher M. Cook
Kelly D. PUCKETT
Dakota W. FOSTER
Jason D. WIMBERLEY
Justin R. KNOTT
James W. Hodges
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Dana Automotive Systems Group LLC
Original Assignee
Dana Automotive Systems Group LLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Dana Automotive Systems Group LLC filed Critical Dana Automotive Systems Group LLC
Publication of WO2015069829A1 publication Critical patent/WO2015069829A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16J—PISTONS; CYLINDERS; SEALINGS
    • F16J15/00—Sealings
    • F16J15/02—Sealings between relatively-stationary surfaces
    • F16J15/06—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces
    • F16J15/10—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with non-metallic packing
    • F16J15/102—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with non-metallic packing characterised by material
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16J—PISTONS; CYLINDERS; SEALINGS
    • F16J15/00—Sealings
    • F16J15/02—Sealings between relatively-stationary surfaces
    • F16J15/06—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces
    • F16J15/10—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with non-metallic packing
    • F16J15/104—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with non-metallic packing characterised by structure

Definitions

  • the present invention relates to a gasket with dissimilar materials. More particularly, the invention relates to a gasket having dissimilar materials at different sealing locations.
  • Gaskets are well-known devices for creating a seal between two parts.
  • one kind of gasket material is preferable over another material for certain applications.
  • the preference for one material over another might be because of the performance characteristics of the gasket material.
  • the higher performing gasket material is more expensive.
  • the resulting gasket is often entirely constructed of the more expensive, higher performing material.
  • a gasket comprises two dissimilar materials.
  • the first material has a first and second profile, which are different from one another, and the second material has a first and a second profile, which are different from one another.
  • the first material first profile and the second material first profile are the same.
  • the first material second profile and the second material second profile combine to form the same shape as the first material first profile or the second material first profile.
  • the two dissimilar materials are provided with complementary joining portions.
  • the first material joining portion uses a series of planes with a male portion extending from two of the planes.
  • the second material joining portion uses a series of complementary planes with a recess between two planes for receiving the male portion.
  • Fig. 1 is a schematic, perspective view of an air intake and a cam cover for a vehicle utilizing two dissimilar gasket materials;
  • Fig. 1 A is a detail of a feature from Fig. 1 ;
  • Fig. 2 is a schematic, perspective view of a cutaway portion of Fig. 1 ;
  • Fig. 2A is a schematic, perspective view of a cutaway portion of Fig. 1 with a mating part;
  • Fig. 3 is a schematic, perspective view of a detail of Fig. 1 ;
  • Fig. 4 is also a schematic, perspective view of a cutaway detail of Fig. 1 ;
  • Fig. 5 is a schematic, perspective view of another embodiment of two joined dissimilar materials
  • Fig. 6 is a schematic, perspective view of the materials in a channel with a mating part
  • Fig. 7 is a schematic, top view of the embodiment depicted in Fig. 5;
  • Fig. 8 is a schematic, perspective view in cutaway of the embodiment depicted in Fig. 5;
  • Fig. 9 is a schematic, perspective view in cutaway of the embodiment depicted in Fig. 5 located in a cam cover;
  • Fig. 10 is a schematic, perspective view of one part of the gasket depicted in Fig. 5;
  • Fig. 11 is a schematic, perspective view of a second part of the gasket depicted in Fig. 5;
  • Fig. 12 is a schematic, side view of the parts in Figs. 10 and 11.
  • a cam cover 20 with an integrated air intake 22 is depicted.
  • Those skilled in the art know that these can be separate pieces, or they can be one piece and integrally formed like that shown in Fig. 1. It is also important to appreciate that the cam cover 20 and air intake 22 merely provide one environment for the device described below and the device is not limited to use with just a cam cover 20 and/or an air intake 22.
  • the cam cover 20 has an interior portion 24 bounded by an upstanding perimeter wall 26.
  • An upper surface 28 of the wall 26 has a continuous groove 30 located therein.
  • a gasket, or seal, is located within the groove 30 to seal the cam cover 20.
  • the air intake 22 portion forms a part of the perimeter wall 26.
  • the air intake portion 22 defines three openings 32, each opening 32 is separated by a land 34.
  • the openings 32 are bounded by continuous walls
  • the perimeter groove 30 splits at each opening 32.
  • a first part 38 of the perimeter groove 30 extends around one side of an opening 32 and a second part 40 of the perimeter groove 30 extends around the other side.
  • the first part 38 extends inwardly into the cam cover interior portion 24, and the second part 40 extends outwardly or away from the cam cover interior portion 24.
  • the two groove parts 38, 40 come back together adjacent the land 34, extend as one through the land 34 and then split again at the next opening 32.
  • the air intake openings 32 and the cam cover 20 need to be sealed so a gasket, or seal, is located about the openings 32.
  • the air intake openings 32 are sealed with a first material 42 and the cam cover 20 is sealed with a second, different material 44.
  • the first material 42 that is used about the air intake openings 32 may be such as FKM or FPM.
  • FPM is the international abbreviation according to DIN/ISO
  • FKM is the short form for the fluoroelastomer category according to the American standard ASTM.
  • FKM perfluoro-elastomers
  • FEPM tetrafluoro ethylene/propylene rubbers
  • All FKMs contain vinylidene fluoride as a monomer. Fluoroelastomers are more expensive than neoprene or nitrile rubber elastomers. They provide additional heat and chemical resistance. FKMs can be divided into different classes on the basis of their chemical composition, their fluorine content or their crosslinking mechanism.
  • the second material 44 that is used about the cam cover 20 may be such as AEM or ACM.
  • AEM rubber also abbreviated AECM (ISO 1629), is an ethylene acrylic rubber.
  • ACM is acrylic rubber, known by the chemical name alkyl acrylate copolymer. It is a type of rubber that has good resistance to hot oil, ozone and oxidation and it has a low permeability to gases. It has a high continuous working temperature in the range of 300 degrees F.
  • Fig. 1 depicts a portion of the first material 42 extending about one of the air intake openings 32 and a portion of the second material 44 extending about the cam cover 20.
  • the first material 42 extends continuously, without breaks or interruption about the air intake opening 32.
  • the second material 44 extends continuously, without breaks or interruption about the cam cover 20. It is desirable to use the first material 42 about the air intake openings 32 because of its performance characteristics. The first material 42 can be expensive and thus it is undesirable to extend it about the cam cover 20.
  • the second material 44 is preferred to use the second material 44 about the cam cover 20 since it is less expensive and it has performance characteristics adequate for the conditions therein.
  • the groove 30 has a single, mostly, if not entirely, constant width along its entire course.
  • the gaskets depicted and described herein may be used.
  • the first material 42 that extends about the air intake openings 32 has a first profile 46 that extends about the first part 38 of the groove 30 about an air intake opening 32 and a second profile 48 that extends about the second part 40 of the groove 30 about an air intake opening 32.
  • the second profile 48 is located adjacent the second material 44.
  • the first profile 46 has a generally T-shaped cross section as seen in Fig. 2.
  • the cross-section comprises a base portion 50 with an inner arm 52 and an outer arm 54 extending from an upper portion 56 of the base portion 50.
  • the inner arm 52 extends along an inner perimeter 58 of the first material 42 and the outer arm 54 extends along an outer perimeter 60 of the first material 42.
  • the arms 52, 54 are located across from one another on the base portion 50 and extend generally transversely from the base portion 50.
  • the arms 52, 54 taper upwardly to form an upper track 62 on the first profile 46.
  • the first profile 46 of the first material 42 transitions to the second profile 48, as seen in Figs. 3 and 4. More particularly, the outer arm 54 tapers out of existence into the base portion 50. Additionally, the material from an inside edge 64 of the upper track 62 and extending vertically downward is removed from the second profile 48. The removed material results in a planar side 66, as shown in Fig. 2.
  • the second profile 48 thus comprises the upper track 62, the inner arm 52 and a portion, such as approximately half, of the base portion 50.
  • the second material 44 has a first and second profile 68, 70 as well, as shown in Fig. 2.
  • the second profile 70 is the same as the first profile 46 for the first material 42.
  • the second material second profile 70 comprises a generally T-shaped cross section, as shown in Fig. 1 A.
  • the cross-section comprises a base portion 72 with an inner arm 74 and an outer arm 76 extending from an upper portion 78 of the base portion 72.
  • the arms 74, 76 are located across from one another on the base portion 72 and extend generally transversely from the base portion 72.
  • the arms 74, 76 taper upwardly to form an upper track 82 on the first profile 68.
  • the first profile 68 of the second material 44 transitions to the second profile 70, which can be appreciated from Figs. 2-4. More particularly, the outer arm 76 tapers out of existence into the base portion 72. Additionally, the material from an outside edge 84 of the upper track 82 and extending vertically downward through the base portion 72 is removed from the second profile 70. The removed material results in a planar side 86.
  • the second profile 70 thus comprises the upper track 82, the outer arm 76 and a portion, such as approximately half, of the base portion 72.
  • planar sides 66, 86 of the first material 42 and the second material 44 abut one another in a continuous fashion from the upper tracks 62, 82 and along the base portions 50, 72 of the materials.
  • the planar sides 66, 86 abut one another in a continuous fashion at least along their length in the groove 30 from one land 34 to the next land 34.
  • the two second profiles 48, 70 of the two different gasket materials 42, 44 combine to result in a single profile that is the same as the two first profiles 46, 68.
  • the two second profile 48, 70 when located together, fit within the same single groove 30 as the first profiles 46, 68, and have the same general shape. This can be appreciated from Fig. 2.
  • the groove 30 be slightly wider where the two materials 42, 44 combine in order to accommodate them, which can be seen in Fig. 3. It is also within the scope of the present invention that the two materials 42, 44 can combine to create different shapes than the two first profiles 46, 68 put together.
  • a mating part 88, or parts, is located against the air intake 22 and cam cover 20 to enclose them, as shown in Fig. 2A. For convenience, only a single mating part 88 will be referred to in the following description.
  • the mating part 88 is located in direct contact with the upper track 62 of the first material 42 as it extends around the periphery of the air intake 22, which can be appreciated in Fig. 2A.
  • the mating part is also located in direct contact with the upper track 82 of the second material 44 about the periphery of the cam cover 20.
  • the mating part 88 is located in direct contact with the upper tracks 62, 82 of the first and second materials 42, 44 when they are located adjacent one another in the groove 30, such as in the first part 38 of the groove, which can be appreciated in Fig. 2A.
  • a seal is formed between the upper tracks 62, 82 and the mating part 88, as seen in Fig. 2A.
  • each base portion 50, 72 is located in direct contact with a bottom surface 102 of the groove 30 to form a seal.
  • Figs. 5-11 depict yet another embodiment of a gasket comprised of two dissimilar materials.
  • This gasket may be used in the application as described above, such as for providing sealing between an integrated cam cover 20 and air intake 22 and a mating part 88, as shown in Fig. 6 and appreciated from Figs. 1 and 2A.
  • the gasket is preferably located in the groove 30 as described above. It should be understood, however, that the gasket can be used in any application and it not restricted to the parts or the particular groove as depicted and described herein.
  • the gasket is comprised of the first material 42 and the second material 44, as described above.
  • the second material 44 extends around the cam cover 20 perimeter. It is desirable to use the first material 42 about the air intake 22 openings 32.
  • the second material 44 extends to the land area 34 where a joining portion 104 for connecting with the first material 42 is located.
  • the second material 44 prior to the land area 34, the second material 44 has the same shape and features as described above. Namely, the second material 44 has an upper track 82, inner and outer arms 74,76 and base portion 72. In, or adjacent, the land area 34, the second material 44 widens to form the joining portion 104, as seen in Figs. 5, 6, 7, 8 and 9. More particularly, the upper track 82 splits into a first track 106 and a second track 108. The two tracks 106, 108 initially diverge from one another. The tracks 106, 108 are separated from one another by a first recess 110. The inner arm 74 and the outer arm 76 diverge from one another on their respective tracks 106, 108.
  • a first downwardly extending plane 112 interrupts the first recess 110 and both tracks 106, 108.
  • the first plane 112 transitions to a second plane 114.
  • the second plane 114 has an upward angle associated with it.
  • the second plane 114 transitions to a third plane 116, where the third plane 116 extends downwardly. The transitions may occur between 1/3 and 2/3 the gasket thickness.
  • transitions between planes in the figures are depicted as having radii, but it is permissible to have radii other than as shown, or the transitions may be at sharp angles with respect to one another.
  • a second recess 118 is located in the second plane 114 and extends through to the third plane 116.
  • a base 120 of the second recess 118 is parallel with the upper track 82.
  • the second recess 118 is generally centered in the second 114 and third 116 planes.
  • Two feet 122 extend downwardly from beneath the joining portion 104, as shown in Fig. 9.
  • the feet 122 are separated by a third recess 124.
  • Cross- pieces 126 extend transverse to the feet 122 across the third recess 124.
  • the cross-pieces 126 are shown in Fig. 8.
  • the cross-pieces 126 may be the same height as the feet 122 or they may be a lesser dimension.
  • the cross-pieces 126 add strength to the feet 122 and prevent them from buckling inwardly.
  • the entirety of the second material 44 is one-piece, integrally formed and unitary. It is within the scope of the invention, however, for any of the above-described features of the gasket to be separately formed and then joined together.
  • the first material 42 has a complementary shaped joining portion 128 to the second material 44 joining portion 104, which can be appreciated from at least Figs. 5, 8 10, 11 and 12.
  • the first material 42 approaches the joining portion 128 with a profile as described above. Namely, the first material 42 has an upper track 62, inner and outer arms 52, 54 and a base portion 50.
  • the first material 42 widens to form the joining portion 128, as shown in Figs. 5, 6, 7 and 10. More particularly, the upper track 62 splits into a first track 130 and a second track 132, as shown in Figs. 5 and 6.
  • the two tracks 130, 132 diverge from one another.
  • the tracks 130, 132 are separated from one another by a first recess 134.
  • the inner arm 52 and the outer arm 54 diverge from one another on their respective tracks 130, 132.
  • At least one, and preferably two, cross-pieces 136 extend across the first recess 134.
  • the cross-pieces 136 extend from the diverged tracks 130, 132 continuously across the first recess 134 equidistant from one another.
  • the cross-pieces 136 are substantially transverse to the diverged tracks 130, 132.
  • the cross-pieces 136 may be the same height as the tracks 130, 132 or they may be a lesser dimension, as shown in Fig. 8.
  • the cross-pieces 136 add strength to the tracks 130, 132 and prevent them from buckling inwardly.
  • a first downwardly extending plane 138 interrupts the first recess 134 and both tracks 130, 132, as shown in Figs. 8, 10, 11 and 12.
  • the first plane 138 transitions to a second plane 140.
  • the second plane 140 has an upward angle associated with it.
  • the second plane 140 transitions to a third plane 142, where the third plane 142 extends downwardly. The transitions may occur between 1/3 and 2/3 the gasket thickness.
  • a male portion 144 is located in the second plane 140 and extends through to the third plane 142, as shown in Fig. 10.
  • the male portion 144 is axially aligned with the base portion 50 of the first material 46.
  • the male portion 144 has a complementary shape and location to the second recess 118 in the second material 44.
  • the male portion 144 fits within the second recess 118 to help secure the two materials 42, 44 together.
  • a second recess 146 in the first material 42 extends into the third plane, as shown in Fig. 10.
  • the second recess 146 results in two downwardly extending feet 148 being formed in the first material 42, best seen in Figs. 10 and 11.
  • the two feet 148 are formed in a unitary fashion with the base portion 50 of the first material 46.
  • the two feet 148 match in size, shape and are aligned with the two feet 122 in the second material 44.
  • the entirety of the first material 42 is one-piece, integrally formed and unitary. It is within the scope of the invention, however, for any of the above-described features of the first material 42 to be separately formed and then joined together.
  • the plane shapes 112, 138, 114, 140, 116, 142 of the first material 42 and the second material 44 increase the surface area of the materials 42, 44 at the joining portions 104, 128.
  • the increased surface area, the resulting zig-zag shape of the joining portions 104, 128, and the male portion 144 and mating recess 118, result in a stable, firm joint that forms a tight and strong seal between the two materials 42, 44.
  • the zig-zag shape created by the planes has the added benefit of permitting the materials 42, 44 to compress against one another for better sealing.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Gasket Seals (AREA)

Abstract

L'invention porte sur un joint d'étanchéité, qui comporte deux matériaux dissemblables (42, 44). Les deux matériaux différents sont utilisés pour communiquer des caractéristiques d'étanchéité différentes. Dans un mode de réalisation, les matériaux d'étanchéité différents se réunissent pour créer un profil (46, 48) identique ou similaire au profil des matériaux individuels. Dans un autre mode de réalisation, les différents matériaux d'étanchéité ont le même profil (68, 70), mais ont des parties de jonction qui sont complémentaires entre elles là où les deux matériaux sont réunis l'un à l'autre.
PCT/US2014/064226 2013-11-06 2014-11-06 Joint d'étanchéité à matériaux dissemblables Ceased WO2015069829A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201361900486P 2013-11-06 2013-11-06
US61/900,486 2013-11-06

Publications (1)

Publication Number Publication Date
WO2015069829A1 true WO2015069829A1 (fr) 2015-05-14

Family

ID=51952018

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2014/064226 Ceased WO2015069829A1 (fr) 2013-11-06 2014-11-06 Joint d'étanchéité à matériaux dissemblables

Country Status (1)

Country Link
WO (1) WO2015069829A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018019722A1 (fr) * 2016-07-28 2018-02-01 Mahle International Gmbh Élément d'étanchéité

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1302707A2 (fr) * 2001-10-09 2003-04-16 Dana Corporation Joint thermoplastique avec ouvertures revêtues de caoutchouc et manchons de positionnement
US20030107187A1 (en) * 2000-12-07 2003-06-12 Toshitsugu Yajima Seal member, and substrate storage container using the same
FR2863677A1 (fr) * 2003-12-16 2005-06-17 Amkey Mgt Profile d'etancheite
WO2007024212A1 (fr) * 2005-08-19 2007-03-01 Freudenberg-Nok General Partnership Garniture barriere
WO2011114800A1 (fr) * 2010-03-16 2011-09-22 日本メクトロン株式会社 Élément d'étanchéité
US20110227295A1 (en) * 2008-11-25 2011-09-22 Nok Corporation Two-material composite gasket
WO2013143721A1 (fr) * 2012-03-28 2013-10-03 Robert Bosch Gmbh Joint en matériau élastomère à plusieurs constituants, boîtier, module d'éléments de batterie et véhicule à moteur

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030107187A1 (en) * 2000-12-07 2003-06-12 Toshitsugu Yajima Seal member, and substrate storage container using the same
EP1302707A2 (fr) * 2001-10-09 2003-04-16 Dana Corporation Joint thermoplastique avec ouvertures revêtues de caoutchouc et manchons de positionnement
FR2863677A1 (fr) * 2003-12-16 2005-06-17 Amkey Mgt Profile d'etancheite
WO2007024212A1 (fr) * 2005-08-19 2007-03-01 Freudenberg-Nok General Partnership Garniture barriere
US20110227295A1 (en) * 2008-11-25 2011-09-22 Nok Corporation Two-material composite gasket
WO2011114800A1 (fr) * 2010-03-16 2011-09-22 日本メクトロン株式会社 Élément d'étanchéité
WO2013143721A1 (fr) * 2012-03-28 2013-10-03 Robert Bosch Gmbh Joint en matériau élastomère à plusieurs constituants, boîtier, module d'éléments de batterie et véhicule à moteur

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018019722A1 (fr) * 2016-07-28 2018-02-01 Mahle International Gmbh Élément d'étanchéité
JP2019523372A (ja) * 2016-07-28 2019-08-22 マーレ インターナショナル ゲゼルシャフト ミット ベシュレンクテル ハフツングＭＡＨＬＥ Ｉｎｔｅｒｎａｔｉｏｎａｌ ＧｍｂＨ シーリング要素
CN110192051A (zh) * 2016-07-28 2019-08-30 马勒国际有限公司 密封元件
US10927955B2 (en) 2016-07-28 2021-02-23 Mahle International Gmbh Sealing element

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