USRE34874E - Seal with two sealing portions having flange receiving opening therebetween - Google Patents

Seal with two sealing portions having flange receiving opening therebetween Download PDF

Info

Publication number
USRE34874E
USRE34874E US07/945,828 US94582892A USRE34874E US RE34874 E USRE34874 E US RE34874E US 94582892 A US94582892 A US 94582892A US RE34874 E USRE34874 E US RE34874E
Authority
US
United States
Prior art keywords
seal
spaced
sealing portions
opening
flange
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.)
Expired - Lifetime
Application number
US07/945,828
Inventor
Ira R. Newman
Kenneth N. Minshull
Kenneth J. McGilp
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.)
Precision Tube Bending Inc
Original Assignee
Precision Tube Bending Inc
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
Priority claimed from US06/673,581 external-priority patent/US4565380A/en
Application filed by Precision Tube Bending Inc filed Critical Precision Tube Bending Inc
Priority to US07/945,828 priority Critical patent/USRE34874E/en
Application granted granted Critical
Publication of USRE34874E publication Critical patent/USRE34874E/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L17/00Joints with packing adapted to sealing by fluid pressure
    • F16L17/02Joints with packing adapted to sealing by fluid pressure with sealing rings arranged between outer surface of pipe and inner surface of sleeve or socket
    • F16L17/025Joints with packing adapted to sealing by fluid pressure with sealing rings arranged between outer surface of pipe and inner surface of sleeve or socket the sealing rings having radially directed ribs
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/16Sealings between relatively-moving surfaces
    • F16J15/32Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings
    • F16J15/3204Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings with at least one lip
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L17/00Joints with packing adapted to sealing by fluid pressure
    • F16L17/02Joints with packing adapted to sealing by fluid pressure with sealing rings arranged between outer surface of pipe and inner surface of sleeve or socket
    • F16L17/03Joints with packing adapted to sealing by fluid pressure with sealing rings arranged between outer surface of pipe and inner surface of sleeve or socket having annular axial lips
    • F16L17/035Joints with packing adapted to sealing by fluid pressure with sealing rings arranged between outer surface of pipe and inner surface of sleeve or socket having annular axial lips the sealing rings having two lips parallel to each other

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Gasket Seals (AREA)

Abstract

An integral ring-shaped seal adapted to be carried at the end of a connector housing and provide two spaced-apart sealing portions, said two spaced-apart sealing portions being connected by a web, and said two spaced-apart sealing portions together with said web providing therebetween an opening adapted to receive a flange located in proximity to the end of the connector housing, at least one of said two spaced-apart sealing portions having a cut-out axially disposed away from said opening to provide increased resiliency and wear resistance.

Description

.Iadd.This is a continuation of application Ser. No. 07/641,651, filed on Jan. 1, 1991, now abandoned, which is reissue of 06/673,581, filed Nov. 21, 1984, and patented as U.S. Pat. No. 4,565,581, on Jan. 21, 1986. .Iaddend.
BACKGROUND OF THE INVENTION
Various ring seals for use at the end of connector housing have been used. Kramer U.S. Pat. No. 3,206,226 discloses an annular seal ring having radially inner and radially outer sides defining smoothly convex surfaces extending across the width thereof and convex axial sides forming a pair of radially outer corners and a pair of radially inner corners. Greenwald U.S. Pat. No. 3,698,727 pertains to a seal ring which in cross-section is essentially U-shaped or J-shaped and having an elastomeric or garter spring core. Kramer U.S. Pat. No. 3,918,726 relates to another flexible seal member having an insert membrane embodied therein to provide reinforcement of the balance of the flexible seal against deformation and resistance to abrasion. The disclosure of Shire and Newman U.S. Pat. No. 3,695,639 is characterized by two generally ring shaped cells mounted in spaced side by side relationship at the end of a connector housing. The outer seal is generally circular in cross-section and includes a first leg, and a second smaller leg connected together by a web portion. The end of the connector tube is provided with formations for holding the seals in the housing. These formations may include first and second counterbores for positioning the inner seal in the end of the connector housing. The base of the second counterbore is normally in spaced relation to the inner side of the second leg to permit the legs of the inner seal to flex when a pipe mounted in the connector pivots or vibrates.
The basic purposes of these annular rings is to maintain a tight seal over the wide range of temperatures and conditions encountered in use. The environment encountered is typically that found in the heating and air conditioning ducts of a modern commercial jet transport airplane. The individual lengths of connector tube are flexible due to thermal expansion and contraction, placing substantial and repeated stress on the ring seals.
The prior patents discussed above treat the problem of seal wear due to abrasion caused by repeated flexing in several ways. The seals of the Kramer patents lack sufficient flexibility and have been generally rejected for all practical purposes.
The other two patents endeavored to provide flexibility. However, the seals disclosed therein are rather complex in manufacture involving composite structures or a plurality of individual components. In any case, the complexity creates opportunity for error in manufacture and installation, as well as necessarily involving high cost.
The present invention for the first time presents an integral annular seal which provides excellent sealing, high flexibility and resistance to abrasion. The seal of this invention is simpler to make and install in a connector and is believed to represent a significant advance over the seals of the prior art. It is to be expected that this new seal will be widely adopted by the commercial jet transport industry.
SUMMARY OF THE INVENTION
Briefly, the present invention comprises an integral ring-shaped seal adapted to be carried at the end of a connector housing and provide two spaced-apart sealing portions, said two spaced-apart sealing portions being connected by a web, and said two spaced-apart sealing portions together with said web providing therebetween an opening adapted to receive a flange located in proximity to the end of the connector housing, at least one of said two spaced-apart sealing portions having a cut-out axially disposed away from said opening to provide increased resiliency and wear resistance.
This invention further comprehends the novel combination comprising telescoping connector housing sections one of which has an upstanding annular flange located in proximity to its open end, and an integral ring-shaped seal carried at the end of one of said connector housing, said seal having two spaced-apart sealing portions, said two spaced-apart sealing portions being connected by a web, and said two spaced-apart sealing portions together with said web providing therebetween an opening, said flange being received in said opening, at least one of said two spaced-apart sealing portions having a cut-out axially disposed away from said opening to provide increased resiliency and wear resistance.
Another feature of this invention is that the integral seal of this invention is held in position by one flange which is received in an opening of complementary size and shape within the seal, as stated above. Preferably, a second or end flange is also provided, as shown in the drawings. The flanges are "L" shaped and are usually welded to the connector wall. The length of the leg of either or both "L" shaped flanges abutting the connector wall can be cut to any size before welding and thereby adjust the space between flanges to accommodate any desired size of seal to vary the spacing between flanges. This features is highly desirable in providing a high degree of manufacturing flexibility and product variability from identical standard "L" shaped elements and is itself an improvement over the prior art.
It is an object of this invention to provide a novel annular ring seal.
It is a further object of this invention to provide an integral ring seal which is superior in manufacture and use than seals heretofore known in this art.
A related object of this invention is to provide a novel combination of connector sections and ring seal which is better adapted to manufacturing control and field use conditions.
These and other objects and advantages will be apparent to those skilled in the art from the more detailed description which follows, particularly when taken in conjunction with the accompanying drawings.
DESCRIPTION OF PREFERRED EMBODIMENTS
The following drawings are for purposes of illustration and further explanation.
Turning to the drawings:
FIG. 1 is a side sectional view of two telescoping ends of connector sections provided with one preferred embodiment of the novel integral annular seal of this invention, and is adapted to a ducting system which is in compression.
FIG. 2 is a plan view of the sealing ring shown installed in FIG. 1.
FIG. 3 is a section taken along line 3--3 in FIG. 2.
FIG. 4 is an enlarged view in section of the sealing ring of FIGS. 1 to 3.
FIG. 5 is a section taken along line 5--5 in FIG. 1.
FIGS. 6A through 6L are views similar to FIG. 4, showing a number of alternative embodiments of the ring seal of the present invention.
FIG. 7 is a sectional view of another embodiment of the present invention.
FIG. 8 is a plan view of the sealing ring shown as installed in FIG. 7.
FIG. 9 is a sectional view taken along the line 9--9 in FIG. 8.
FIG. 10 is an enlarged view in section of the sealing ring of FIGS. 7 to 9.
FIG. 11 is a greatly enlarged section showing the sealing ring and telescoping connector sections of FIG. 7.
FIGS. 12A to 12H are alternate embodiments of the sealing ring of FIGS. 7 to 11.
FIGS. 13A to 13L are partial sectional views of various connector ends provided with annular inwardly disposed flanges which are adapted to receive any of the sealing rings of FIGS. 1 through 12.
FIG. 14 and an ensuing Figures relate to important alternative embodiments of the invention wherein the annular flange is outwardly extending from the exterior of a connector section and the opening in the sealing ring is disposed so as to be able to receive an outwardly extending flange. FIG. 14 is a sectional view of one embodiment showing the sealing ring in the installed position, and is adapted to a ducting system which is in tension.
FIG. 15 shows in section another connector arrangement utilizing the sealing ring of FIG. 14.
FIG. 16 is an enlarged partial section of the sealing ring of FIGS. 14 and 15.
FIG. 17 is an enlarged partial section of the sealing ring of FIG. 16 which has been installed as per FIGS. 15 and 15.
FIGS. 18A through 18L are alternative embodiments in partial section of the sealing ring of FIGS. 14 to 17.
FIG. 19 is analogous to FIG. 7, differing in that the flange is outwardly rather than inwardly disposed on the connector end. FIG. 19 is a sectional view and shows another embodiment of this invention with the seal installed.
FIG. 20 is an enlarged partial section of the seal of FIG. 19.
FIG. 21 shows the seal, in partial enlarged section, of FIGS. 19 and 20, installed.
FIGS. 22A through 22H are alternate embodiments in partial section of the seal of FIGS. 19 through 21.
Considering the drawings in more detail, and using the embodiment of FIGS. 1 to 5 for purposes of illustration, connector end sections 10 and 12 telescope together as shown. Section 12 has two inwardly directed annular flanges 14 and 16 which are affixed to the body of section 12. The integral annular sealing ring 18 has two spaced-apart portions 20 and 22 interconnected by web 24. The opening 26 receives the flange 16. The portion 22 has a cut-out 28 which is axially disposed from opening 26.
When installed, the portion 22 is more resilient and flexible than portion 24 due to the presence of cut-out 28. The integral ring 18 is composed of an elastomer which is reinforced with a fiberous or filamentary material such as fiberglass. The entire ring 18 can be made in one molding operation. The engagement of flange 16 with opening 26 maintains the ring 18 in the proper position within the connector end over virtually any and all ranges of operating conditions. This structure has been found to be uniquely .[.resistance.]. .Iadd.resistant .Iaddend.of abrasion and wear as the connector ends 10 and 12 .[.intergo.]. .Iadd.undergo .Iaddend.flex due to thermal cycling and other stresses. The connector portions per se are normally made of titanium. However, the specific materials of construction do not bear on the present invention.
As can be seen in FIGS. 6A to 6L, the integral annular seal can have a variety of cross-sectional configurations including the embodiment wherein both portions which are interconnected by the web have axially disposed cut-out at opposite sides of the flange-receiving opening. The symmetrical configurations afford greater flexibility than the asymmetrical configurations.
The embodiments of FIGS. 7 to 12 illustrate the case where the flange-receiving opening and the axially displaced cut-out merge to form an L-shaped integral annular ring which has one leg adapted to abut the flange and the other leg adapted to abut the surface of one connector end on one of its sides and the free end of the flange on the other side.
The "L" shaped seal of FIGS. 7 through 12 is the same seal as shown in FIGS. 19 through 22. Thus, this version is characterized by exceptional versatility. It should also be noted that this seal affords far greater sealing area than the "J" seals of the prior art, and is superior in function and durability.
FIGS. 14 through 22 relate to the structure wherein the connector ends 100 and 102 are telescoping. Connector end 100 has outwardly disposed flanges 104 and 106. The integral annular seal 108 has two spaced-apart portions 110 and 112 with interconnecting web 112. The space 114 is adapted to receive flange 106. The axially disposed cut-out 116 functions as described hereinabove.
As is illustrated by FIG. 15 in particular, the invention is applicable to the full range of connector configurations.
The present invention provides numerous advantages some of which are as follows:
1. Longer sealing edge surface which provides longer service life.
2. Maintains its sealing capabilities under angulation and negative pressure.
3. Construction allows greater side loads.
4. Seal will not roll during installation.
5. Even if seal is installed beyond its design limits the web prevents the inner seal from disintegrating into the ducting system.
6. Design does not allow seal to be put into housing incorrectly.
7. Single seal design eliminates human error of omitting inner seal during installation.
8. "C" area of seal will accommodate "O" ring for additional squeeze if required, such as in cold air ducting.
9. Only required to stock one seal per joint, which is more cost effective resulting in less inventory.
10. Dimensionally the joint is used in a compression and tension system by changing the primary sealing surface of the seal from the housing to the sleeve.
It is to be understood that the present invention allows the use of the same general configuration of telescoping parts to be used in a compression or tension system, or a system that is mixed compression and tension.
It is also to be understood that the connector can be used as an integral part of a duct or separately as a reducer.
Having fully described the invention, it is intended that it be limited only by the lawful scope of the appended claims.

Claims (2)

    We claim: .[.1. An integral ring-shaped seal adapted to be carried at the end of a connector housing and provide two spaced-apart sealing portions, said two spaced-apart sealing portions being connected by a web, and said two spaced-apart sealing portions together with said web providing therebetween an opening adapted to receive a flange located in proximity to the end of the connector housing, at least one of said two spaced-apart sealing portions having a cut-out axially disposed away from said opening to provide increased resiliency and wear resistance..]. .[.2. The construction of claim 1 wherein said opening is a slot..]. .[.3. The construction of claim 1 wherein there are two symmetric axial cut-outs which open at opposite sides of the seal..]. .[.4. The construction of
  1. claim 1 wherein there is one axial cut-out..]. .[.5. The novel combination comprising telescoping connector housing sections one of which has an upstanding annular flange located in proximity to its open end, and an integral ring-shaped seal carried at the end of one of said connector housing, said seal having two spaced-apart sealing portions, said two spaced-apart sealing portions being connected by a web, and said two spaced-apart sealing portions together with said web providing therebetween an opening, said flange being received in said opening, at least one of said two spaced-apart sealing portions having a cut-out axially disposed away from said opening to provide increased resilency and wear resistance..]. .[.6. The construction of claim 5 wherein the seal has an L-shaped cross-section, one leg of which abuts the side of the flange and the other leg abuts the surface of one of its sides and the end of the flange on the other..]. .[.7. The construction of claim 5 wherein said opening is a slot..]. .[.8. The construction of claim 5 wherein there are two symmetric axial cut-outs which open at opposite sides of the seal..]. .[.9. The construction of claim 5 wherein there is one axial cut-out..]. .[.10. The construction of claim 5 where one of said telescoping sections has two adjacent "L" shaped flange sections, one of which is received in said opening in the seal and the other positioned to abut the end of said seal, both of said flange sections being adhered to the cylindrical surface of said telescoping section..]. .[.11. The construction of claim 10 wherein the flanges are on the interior of said telescoping section..]. .[.12. The construction of claim 10 wherein the flanges are on the
  2. exterior of said telescoping section..]. .Iadd.13. In the ducts of commercial jet aircraft, the improvement comprising:
    a novel combination forming part of said ducts and comprising telescoping flexible connector housing sections one of which has an upstanding annular flange located in proximity to the open end of the connector housing, and an integral, flexible, fiber-reinforced elastomeric ring-shaped seal carried at the end of one of said connector housing, said seal having two spaced-apart sealing portions, said two spaced-apart sealing portions being connected by a web, and said two spaced-apart sealing portions together with said web providing therebetween an opening, said flange being received in said opening, at least one of said two spaced-apart sealing portions having a cut-out axially disposed away from said opening to provide increased resiliency and wear resistance, said connector housing sections being adapted to undergo flex due to thermal cycling and other stresses. .Iaddend. .Iadd.14. The improvement of claim 13, wherein the seal has an L-shaped cross-section, one leg of which abuts the side of the flange and the other leg abuts the surface of one of its sides and the end of the flange on the other. .Iaddend. .Iadd.15. The improvement of claim 13, wherein said opening is a slot. .Iaddend. .Iadd.16. The improvement of claim 13, wherein there are two symmetric axial cut-outs which open at opposite sides of the seal. .Iaddend. .Iadd.17. The improvement of claim 13, wherein there is one axial cut-out. .Iaddend. .Iadd.18. The improvement of claim 13, wherein one of said telescoping sections has two adjacent "L" shaped flange sections, one of which is received in said opening in the seal and the other positioned to abut the end of said seal, both of said flange sections being adhered to the cylindrical surface of said telescoping section. .Iaddend. .Iadd.19. The improvement of claim 18, wherein the flanges are on the interior of said telescoping section. .Iaddend. .Iadd.20. The improvement of claim 18, wherein the flanges are on the exterior of said telescoping section. .Iaddend.
US07/945,828 1984-11-21 1992-09-16 Seal with two sealing portions having flange receiving opening therebetween Expired - Lifetime USRE34874E (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US07/945,828 USRE34874E (en) 1984-11-21 1992-09-16 Seal with two sealing portions having flange receiving opening therebetween

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US06/673,581 US4565380A (en) 1984-11-21 1984-11-21 Seal with two sealing portions having flange receiving opening therebetween
US64165191A 1991-01-15 1991-01-15
US07/945,828 USRE34874E (en) 1984-11-21 1992-09-16 Seal with two sealing portions having flange receiving opening therebetween

Related Parent Applications (2)

Application Number Title Priority Date Filing Date
US06/673,581 Reissue US4565380A (en) 1984-11-21 1984-11-21 Seal with two sealing portions having flange receiving opening therebetween
US64165191A Continuation 1984-11-21 1991-01-15

Publications (1)

Publication Number Publication Date
USRE34874E true USRE34874E (en) 1995-03-14

Family

ID=27093811

Family Applications (1)

Application Number Title Priority Date Filing Date
US07/945,828 Expired - Lifetime USRE34874E (en) 1984-11-21 1992-09-16 Seal with two sealing portions having flange receiving opening therebetween

Country Status (1)

Country Link
US (1) USRE34874E (en)

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10211635A1 (en) * 2002-03-15 2003-09-25 Behr Gmbh & Co Heat exchanger, e.g. for exhaust gas, has one part of first part of tube fitted radially outside one part of second part of tube
US20060290069A1 (en) * 2003-02-27 2006-12-28 Yasuhiro Ikeda Lip-type seal
US20080237994A1 (en) * 2007-03-27 2008-10-02 Rolls-Royce Plc Sealed joint
US20080258400A1 (en) * 2004-09-23 2008-10-23 Goran Anderberg Sealing System for Joints
US20090273181A1 (en) * 2008-05-01 2009-11-05 National Coupling Company, Inc. Probe seal having pressure-energized sealing elements for female hydraulic coupling member
US20100109260A1 (en) * 2008-10-31 2010-05-06 Ti Group Automotive Systems, L.L.C. Ring seal with insert
US20120068413A1 (en) * 2010-09-17 2012-03-22 Carl Freudenberg Kg Sealing profile
US20150065028A1 (en) * 2005-09-19 2015-03-05 Chatsworth Products, Inc. Ducted exhaust equipment enclosure
US9980400B2 (en) 2010-09-10 2018-05-22 Chatsworth Products, Inc. Rail seal for electronic equipment enclosure
US10123462B2 (en) 2005-09-19 2018-11-06 Chatsworth Products, Inc. Ducted exhaust equipment enclosure
US10356951B2 (en) 2013-12-17 2019-07-16 Chatsworth Products, Inc. Electronic equipment enclosure
US10595442B2 (en) 2013-01-11 2020-03-17 Chatsworth Products, Inc. Data processing equipment structure
EP3992512A1 (en) * 2020-10-30 2022-05-04 Poloplast GmbH & Co. KG Pipe sleeve
EP3998421A1 (en) * 2020-10-30 2022-05-18 Poloplast GmbH & Co. KG Pipe sleeve
US11985799B2 (en) 2021-07-31 2024-05-14 Chatsworth Products, Inc. Electronic equipment enclosure

Citations (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US727242A (en) * 1902-07-15 1903-05-05 Charles T White Faucet-coupling.
US1988652A (en) * 1933-01-07 1935-01-22 Chicago Rawhide Mfg Co Oil seal
US2049801A (en) * 1935-08-06 1936-08-04 Ellsworth D Gage Coupling for overhead irrigation pipes
US2213116A (en) * 1939-01-28 1940-08-27 Victor Mfg & Gasket Co Flexible oil seal
US2470925A (en) * 1946-01-16 1949-05-24 Crane Co Piston seal for flush valves
US2480116A (en) * 1945-10-03 1949-08-30 Brummer Olin Oil seal means or the like
US2542234A (en) * 1948-08-04 1951-02-20 Garlock Packing Co Oil seal
US2587405A (en) * 1947-01-15 1952-02-26 Sealol Corp Seal for relatively rotating members
DE1039325B (en) * 1956-10-31 1958-09-18 Schaeffler Ohg Industriewerk Reinforced sealing ring
DE1121891B (en) * 1956-07-23 1962-01-11 Stabey Appbau Ges M B H Sealing sleeve for pressurized pistons
GB1015302A (en) * 1962-04-27 1965-12-31 Ct De Rech S De Pont A Mousson Pipe joint incorporating a sealing ring
US3409357A (en) * 1965-06-21 1968-11-05 Xerox Corp Apparatus for an electrostatic machine
US3449021A (en) * 1966-05-09 1969-06-10 Conover & Co Inc C E Low friction resilient sealing ring
US3563558A (en) * 1968-11-04 1971-02-16 Scovill Manufacturing Co Piston seal with distortable ribs
DE1958378A1 (en) * 1969-09-11 1971-04-08 Pignone Sud Spa Compressed air regulator with force adjustment
US3680874A (en) * 1970-08-24 1972-08-01 Federal Mogul Corp Flexible pneumatic duct connectors assembled with internal seals
US3695639A (en) * 1970-08-07 1972-10-03 Gen Connector Corp Connector
US4111441A (en) * 1976-03-13 1978-09-05 Firma Carl Freudenberg Self-arresting sealing ring
US4219204A (en) * 1978-11-30 1980-08-26 Utex Industries, Inc. Anti-extrusion seals and packings
DE2947083A1 (en) * 1979-11-22 1981-05-27 Estel Hoesch Werke Ag, 4600 Dortmund INSERT SLEEVE CONNECTION FOR STEEL PIPES

Patent Citations (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US727242A (en) * 1902-07-15 1903-05-05 Charles T White Faucet-coupling.
US1988652A (en) * 1933-01-07 1935-01-22 Chicago Rawhide Mfg Co Oil seal
US2049801A (en) * 1935-08-06 1936-08-04 Ellsworth D Gage Coupling for overhead irrigation pipes
US2213116A (en) * 1939-01-28 1940-08-27 Victor Mfg & Gasket Co Flexible oil seal
US2480116A (en) * 1945-10-03 1949-08-30 Brummer Olin Oil seal means or the like
US2470925A (en) * 1946-01-16 1949-05-24 Crane Co Piston seal for flush valves
US2587405A (en) * 1947-01-15 1952-02-26 Sealol Corp Seal for relatively rotating members
US2542234A (en) * 1948-08-04 1951-02-20 Garlock Packing Co Oil seal
DE1121891B (en) * 1956-07-23 1962-01-11 Stabey Appbau Ges M B H Sealing sleeve for pressurized pistons
DE1039325B (en) * 1956-10-31 1958-09-18 Schaeffler Ohg Industriewerk Reinforced sealing ring
GB1015302A (en) * 1962-04-27 1965-12-31 Ct De Rech S De Pont A Mousson Pipe joint incorporating a sealing ring
US3409357A (en) * 1965-06-21 1968-11-05 Xerox Corp Apparatus for an electrostatic machine
US3449021A (en) * 1966-05-09 1969-06-10 Conover & Co Inc C E Low friction resilient sealing ring
US3563558A (en) * 1968-11-04 1971-02-16 Scovill Manufacturing Co Piston seal with distortable ribs
DE1958378A1 (en) * 1969-09-11 1971-04-08 Pignone Sud Spa Compressed air regulator with force adjustment
US3695639A (en) * 1970-08-07 1972-10-03 Gen Connector Corp Connector
US3680874A (en) * 1970-08-24 1972-08-01 Federal Mogul Corp Flexible pneumatic duct connectors assembled with internal seals
US4111441A (en) * 1976-03-13 1978-09-05 Firma Carl Freudenberg Self-arresting sealing ring
US4219204A (en) * 1978-11-30 1980-08-26 Utex Industries, Inc. Anti-extrusion seals and packings
US4219204B1 (en) * 1978-11-30 1985-02-26
DE2947083A1 (en) * 1979-11-22 1981-05-27 Estel Hoesch Werke Ag, 4600 Dortmund INSERT SLEEVE CONNECTION FOR STEEL PIPES

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
R. H. Warring: "Seals and Sealing Handbook", Jul. 1986, pp. 317-318.
R. H. Warring: Seals and Sealing Handbook , Jul. 1986, pp. 317 318. *

Cited By (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050224213A1 (en) * 2002-03-15 2005-10-13 Behr Gmbh & Co. Kg Heat exchanger
DE10211635A1 (en) * 2002-03-15 2003-09-25 Behr Gmbh & Co Heat exchanger, e.g. for exhaust gas, has one part of first part of tube fitted radially outside one part of second part of tube
US20060290069A1 (en) * 2003-02-27 2006-12-28 Yasuhiro Ikeda Lip-type seal
US7344140B2 (en) * 2003-02-27 2008-03-18 Eagle Industry Co., Ltd. Lip-type seal
US20080258400A1 (en) * 2004-09-23 2008-10-23 Goran Anderberg Sealing System for Joints
US8302972B2 (en) * 2004-09-23 2012-11-06 Huhnseal Ab Sealing system for joints
US20150065028A1 (en) * 2005-09-19 2015-03-05 Chatsworth Products, Inc. Ducted exhaust equipment enclosure
US10334761B2 (en) 2005-09-19 2019-06-25 Chatsworth Products, Inc. Method of venting heated air from electronic equipment enclosure
US10568239B2 (en) 2005-09-19 2020-02-18 Chatsworth Products, Inc. Method of venting heated air from electronic equipment enclosure
US10123462B2 (en) 2005-09-19 2018-11-06 Chatsworth Products, Inc. Ducted exhaust equipment enclosure
US10624232B2 (en) * 2005-09-19 2020-04-14 Chatsworth Products, Inc. Ducted exhaust equipment enclosure
US20080237994A1 (en) * 2007-03-27 2008-10-02 Rolls-Royce Plc Sealed joint
US7954859B2 (en) * 2008-05-01 2011-06-07 National Coupling Company, Inc. Probe seal having pressure-energized sealing elements for female hydraulic coupling member
US20090273181A1 (en) * 2008-05-01 2009-11-05 National Coupling Company, Inc. Probe seal having pressure-energized sealing elements for female hydraulic coupling member
US11464132B2 (en) 2008-09-08 2022-10-04 Chatsworth Products, Inc. Ducted exhaust equipment enclosure
US11706898B2 (en) 2008-09-08 2023-07-18 Chatsworth Products, Inc. Ducted exhaust equipment enclosure
US20100109260A1 (en) * 2008-10-31 2010-05-06 Ti Group Automotive Systems, L.L.C. Ring seal with insert
US8419021B2 (en) * 2008-10-31 2013-04-16 Ti Group Automotive Systems, L.L.C. Ring seal with insert
US10178784B2 (en) 2010-09-10 2019-01-08 Chatsworth Products, Inc. Rail seal for electronic equipment enclosure
US9980400B2 (en) 2010-09-10 2018-05-22 Chatsworth Products, Inc. Rail seal for electronic equipment enclosure
US20120068413A1 (en) * 2010-09-17 2012-03-22 Carl Freudenberg Kg Sealing profile
US10595442B2 (en) 2013-01-11 2020-03-17 Chatsworth Products, Inc. Data processing equipment structure
US11647610B2 (en) 2013-01-11 2023-05-09 Chatsworth Products, Inc. Modular thermal isolation barrier for data processing equipment structure
US10356951B2 (en) 2013-12-17 2019-07-16 Chatsworth Products, Inc. Electronic equipment enclosure
US10674634B2 (en) 2013-12-17 2020-06-02 Chatsworth Products, Inc. Electronic equipment enclosure
US11083108B2 (en) 2013-12-17 2021-08-03 Chatsworth Products, Inc. Electronic equipment enclosure
EP3992512A1 (en) * 2020-10-30 2022-05-04 Poloplast GmbH & Co. KG Pipe sleeve
EP3998421A1 (en) * 2020-10-30 2022-05-18 Poloplast GmbH & Co. KG Pipe sleeve
US11985799B2 (en) 2021-07-31 2024-05-14 Chatsworth Products, Inc. Electronic equipment enclosure

Similar Documents

Publication Publication Date Title
US4565380A (en) Seal with two sealing portions having flange receiving opening therebetween
USRE34874E (en) Seal with two sealing portions having flange receiving opening therebetween
US5468030A (en) Tube clamp and coupling
US5630593A (en) Pressure-energized sealing rings
US4893847A (en) Bearing seal for universal ball joint
US7883094B2 (en) Offset stacked sealing system
US4759555A (en) Split ring seal with slip joint
US4662598A (en) Sleeve valve with integral control chamber
US3695639A (en) Connector
US4589666A (en) Slip joint assembly for a split ring seal
KR950012732B1 (en) Butterfly valve construction having a composite seat and a composite seat
US20020024218A1 (en) Connector for flexible pipes having at least one resilient sealing ring
US20020121744A1 (en) Low leakage flexible cloth seals for turbine combustors
US6296282B1 (en) Articulated connecting element for piping elements
US6869082B2 (en) Turbine spring clip seal
US3129021A (en) Flexible joint
CA2224986C (en) Joint assembly and backing mechanism therefor
US4548415A (en) Articulated pipe joint seal assembly
US5112088A (en) Duct joint link assembly
US4116474A (en) Pipe coupling
US3198559A (en) Flexible coupling for rigid members
EP1403584B1 (en) Turbine spring clip seal
EP0084538A1 (en) Sealing assembly in fluid coupling.
US2933334A (en) Self-sealing pipe coupling
US2964343A (en) Gasket assembly

Legal Events

Date Code Title Description
FPAY Fee payment

Year of fee payment: 12