WO1998017930A1 - Piston and cylinder device with resilient seal - Google Patents

Piston and cylinder device with resilient seal Download PDF

Info

Publication number
WO1998017930A1
WO1998017930A1 PCT/GB1997/002865 GB9702865W WO9817930A1 WO 1998017930 A1 WO1998017930 A1 WO 1998017930A1 GB 9702865 W GB9702865 W GB 9702865W WO 9817930 A1 WO9817930 A1 WO 9817930A1
Authority
WO
WIPO (PCT)
Prior art keywords
piston
metal
bore
skirt
cylinder
Prior art date
Application number
PCT/GB1997/002865
Other languages
French (fr)
Inventor
James Brian Wilson
Original Assignee
Abb Offshore Systems Limited
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 Abb Offshore Systems Limited filed Critical Abb Offshore Systems Limited
Priority to BR9711938-5A priority Critical patent/BR9711938A/en
Priority to AU47127/97A priority patent/AU4712797A/en
Publication of WO1998017930A1 publication Critical patent/WO1998017930A1/en
Priority to NO991804A priority patent/NO991804D0/en

Links

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
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J1/00Pistons; Trunk pistons; Plungers
    • F16J1/04Resilient guiding parts, e.g. skirts, particularly for trunk pistons

Definitions

  • the invention relates to a piston and cylinder device for use in harsh conditions
  • a piston and cylinder device used in this environment typically has high water pressure applied to one face of its resilient seal and a high oil pressure applied to
  • a device comprising a metal cylinder defining a bore which has a resilient seal mounted within the bore and a metal piston arranged to fit
  • the piston comprises a resiliently flexible skirt which
  • the skirt extends from the piston, the skirt being arranged to fit within the bore and to engage the
  • the skirt is dimensioned to form the metal-to-metal seal in a region
  • metal seal forms a barrier protecting the resilient seal from the environment outside the
  • an outer surface of the skirt is formed with a thin walled portion
  • the piston only requires a slight travel and provides a reaction point for the axial piston
  • the stop is provided by an external cylindrical flange of the
  • Both the piston and the cylinder are formed preferably from the same metal
  • Figure 1 is a transverse section through a two-part connector for pressurised fluid
  • Figure 2 illustrates the engaged position of the two-part connector shown in
  • FIGS 1 and 2 illustrate a two part connector 10 as described in our co-pending
  • the connector 10 comprises a metal cylinder 11, 12 which defines a bore 13, 14 and a metal piston 15, 16 having a skirt 17, 18 engaging a resilient seal 19, 20 mounted within
  • Each cylinder 11, 12 has a mating surface 21, 22 located at a head of
  • a pre-loaded compression coil spring 29, 30 reacts between each piston 15, 16 and
  • the resilient seals 19 and 20 provide secondary seals which are superseded by
  • Each piston skirt 17 and 18 is
  • each thin walled portion 34 and 35 are preferably controlled by the position of
  • metal-to-metal seals 33, 36 and 37 are sealed against the external environment by metal-to-metal seals 33, 36 and 37.

Abstract

A metal piston (15, 16) has a skirt (17, 18) which engages a resilient seal (19, 20) mounted within a bore (13, 14) of a metal cylinder (11, 12). The skirt (17, 18) has a thin walled portion (34, 35) which is resiliently flexible and is dimensioned relative to the bore (13, 14) such that, whenever fluid pressure acting on the piston (15, 16) exceeds a predetermined value, the thin walled portion (34, 35) will be deformed to provide a secondary metal-to-metal seal (36, 37) protecting the resilient seal (19, 20) from the external ambient environment. In this manner the clearance space between the piston skirt (17, 18) and the cylinder (11, 12) is closed by the outward deformation of the thin walled portion (34, 35) due to the increasing fluid pressure. This inhibits corrosion of the engaged metal surfaces and denies space for the accretion of marine growth or sediment.

Description

PISTON AND CYLINDER DEVICE WITH RESILIENT SEAL
The invention relates to a piston and cylinder device for use in harsh
environments which may cause deterioration of the conventional resilient seal between
the skirt of the piston and the bore of the cylinder.
One particular harsh environment is the ocean floor where subsea oil field apparatus are typically exposed externally to high water pressures and internally to high
oil pressures. A piston and cylinder device used in this environment typically has high water pressure applied to one face of its resilient seal and a high oil pressure applied to
the opposite face of the resilient seal. Such conditions can cause progressive
deterioration of the material from which the resilient seal is formed. Furthermore the face of the resilient seal exposed to the sea water is positioned within the clearance space
between the piston skirt and the cylinder bore which can be affected by corrosion and
by the accretion of marine growth and can cause the piston to jam or may otherwise
damage the resilient seal during piston movement.
Other harsh environment exist in many industrial processes such as chemical
plants and foundries.
It is known to provide a device comprising a metal cylinder defining a bore which has a resilient seal mounted within the bore and a metal piston arranged to fit
within the bore.
It is an object of the present invention to provide a piston and cylinder device in
which the resilient piston seal can be protected from such a harsh environment.
According to the invention the piston comprises a resiliently flexible skirt which
extends from the piston, the skirt being arranged to fit within the bore and to engage the
resilient seal, the cylinder and piston are arranged to define a fluid connection to admit pressurised fluid between the piston and cylinder so as to generate an axial movement
of the piston and the skirt is dimensioned relative to the bore such that whenever pressure of the fluid exceeds a predetermined value the skirt will deform to provide a
metal-to-metal seal with the bore. In this manner, after a predetermined load has been applied to the piston, the clearance space between the skirt and the cylinder is closed by
the outward deformation of the skirt due to the increasing fluid pressure. This prevents
corrosion of the engaged metal surfaces, provided that they are the same material, and
denies space for the accretion of marsh growth or sediment.
Preferably the skirt is dimensioned to form the metal-to-metal seal in a region
lying between the resilient seal and a head of the piston. In this manner the metal-to-
metal seal forms a barrier protecting the resilient seal from the environment outside the
cylinder and also protects that part of the skirt which will slide through the resilient seal
when the piston is eventually relocated into the cylinder. Preferably an outer surface of the skirt is formed with a thin walled portion
which distorts into an external land to form the metal-to-metal seal with the bore. The
use of this land defines the exact position of where the metal-to-metal seal will be
formed and limits the amount of the skirt that need to be machined to a fine tolerance
relative to the cylinder bore.
Desirably axial movement of the piston out of the bore is limited by a stop to
prevent the piston being ejected from the cylinder. This is particularly useful where
the piston only requires a slight travel and provides a reaction point for the axial piston
load as the pressure of the fluid is increased to cause the skirt to expand and grip the cylinder bore. Preferably, the stop is provided by an external cylindrical flange of the
piston and a retaining ring secured within the bore.
Both the piston and the cylinder are formed preferably from the same metal
which would normally be chosen to be highly resistant to corrosion by the ambient
environment.
The invention will now be described, by way of example only, with reference
to the accompanying drawings, in which: -
Figure 1 is a transverse section through a two-part connector for pressurised fluid
illustrating their disengaged position; Figure 2 illustrates the engaged position of the two-part connector shown in
Figure 1;
Figures 1 and 2 illustrate a two part connector 10 as described in our co-pending
British Applications GB 9621770.8A and GB 9621768.2A, the whole contents of each
Application being incorporated herein by reference.
Referring to Figure 1, as described in our co-pending Applications, each part of
the connector 10 comprises a metal cylinder 11, 12 which defines a bore 13, 14 and a metal piston 15, 16 having a skirt 17, 18 engaging a resilient seal 19, 20 mounted within
the bore 13, 14. Each cylinder 11, 12 has a mating surface 21, 22 located at a head of
the piston 15, 16 which is arranged to engage the mating surface 21, 22 of the other part
of the connector 10.
Movement of each piston 15, 16 axially out of its bore 13, 14 is limited by a stop
comprising an external cylindrical flange 23, 24 arranged to abut the inner end of a
retaining ring 25, 26 that is secured within the bore 13, 14 by a threaded connection 27,
28. A pre-loaded compression coil spring 29, 30 reacts between each piston 15, 16 and
cylinder 11, 12 to bias the position of the piston 15, 16 towards its retaining ring 25, 26
such that the flange 23, 24 is held against its respective retaining ring 25, 26.
The mating surfaces 21, 22 when in a engaged position, as illustrated in Figure 2, allow fluid pressure to be communicated between respective lines 31, 32 defined
within the cylinders 11, 12 and pistons 15, 16. The fluid pressure acts on the effective
areas of each piston 15, 16 to press their mating surfaces 21, 22 firmly together to
provide metal-to-metal seal 33.
The resilient seals 19 and 20 provide secondary seals which are superseded by
secondary metal-to-metal seals in the following manner. Each piston skirt 17 and 18 is
formed with a respective thin walled portion 34 and 35 which is resiliently flexible and
dimensioned relative to the respective bore 13 and 14 such that, whenever the fluid pressure exceeds a predetermined value, the thin walled portions 34 and 35 of the skirts
17 and 18 will be deformed to provide secondary metal-to-metal seals 36, 37 protecting
the resilient seals 19 and 20 from the external ambient environment. The dimensions of each thin walled portion 34 and 35 are preferably controlled by the position of
external cylindrical lands 38 and 39, thereby limiting the fine tolerances to a very small
portion of each piston 15, 16 and determining precisely where each secondary metal-to-
metal seal 36, 37 is positioned. In this manner the two-part connector 10 is completely
sealed against the external environment by metal-to-metal seals 33, 36 and 37.

Claims

1. A device (10), comprising
a metal cylinder (11, 12) defining a bore (13, 14) and having a resilient seal (19,
20) mounted within the bore (13, 14),
a metal piston (15, 16) arranged to fit within the bore (13, 14),
characterised in that,
the piston (15, 16) comprises a resiliently flexible skirt (17, 18) which extends
from the piston (15, 16), the skirt being arranged to fit within the bore (13, 14) and to engage the resilient seal (19, 20),
the cylinder (11, 12) and piston (15, 16) are arranged to define a fluid connection
to admit pressurised fluid between the piston (15, 16) and cylinder (11, 12) so
as to generate an axial movement of the piston (15, 16), and
the skirt (17, 18) is dimensioned relative to the bore (13, 14) such that whenever
pressure of the fluid exceeds a predetermined value the skirt (17, 18) will deform
to provide a metal-to-metal seal (36, 37) with the bore (13, 14).
2. A device, according to Claim 1, characterised in that the skirt (17, 18) is
dimensioned to form the metal-to-metal seal (36, 37) in a region lying between
the resilient seal (19, 20) and a head of the piston (15, 16).
3. A device, according to Claim 1 or 2, characterised in that an outer surface of the
skirt (17, 18) is formed with a thin walled portion (34, 35) which distorts into an external cylindrical land (38, 39) to form the metal-to-metal seal (36, 37) with
the bore (13, 14).
4. A device, according to any of Claims 1 to 3, characterised in that axial
movement of the piston (15, 16) out of the bore (13, 14) is limited by a stop.
5. A device, according to Claim 4, characterised in that the stop is provided by an
external cylindrical flange (23, 24) of the piston (15, 16) and a retaining ring
(25, 26) secured within the bore (13, 14).
PCT/GB1997/002865 1996-10-18 1997-10-17 Piston and cylinder device with resilient seal WO1998017930A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
BR9711938-5A BR9711938A (en) 1996-10-18 1997-10-17 Piston and cylinder device with elastic seal.
AU47127/97A AU4712797A (en) 1996-10-18 1997-10-17 Piston and cylinder device with resilient seal
NO991804A NO991804D0 (en) 1996-10-18 1999-04-15 Piston / cylinder assembly with resilient seal

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB9621769.0 1996-10-18
GBGB9621769.0A GB9621769D0 (en) 1996-10-18 1996-10-18 Piston and cylinder device

Publications (1)

Publication Number Publication Date
WO1998017930A1 true WO1998017930A1 (en) 1998-04-30

Family

ID=10801652

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/GB1997/002865 WO1998017930A1 (en) 1996-10-18 1997-10-17 Piston and cylinder device with resilient seal

Country Status (5)

Country Link
AU (1) AU4712797A (en)
BR (1) BR9711938A (en)
GB (2) GB9621769D0 (en)
NO (1) NO991804D0 (en)
WO (1) WO1998017930A1 (en)

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3326579A (en) * 1964-05-27 1967-06-20 Rockwell Mfg Co Multiple conduit connection
US3693133A (en) * 1969-10-08 1972-09-19 Inst Francais Du Petrole Fluid tight electric connector
US4460156A (en) * 1981-05-01 1984-07-17 Nl Industries, Inc. Wellhead connector with check valve
USRE31645E (en) * 1977-08-01 1984-08-14 Regan Offshore International, Inc. Safety apparatus for automatically sealing hydraulic lines within a sub-sea well casing
GB2180107A (en) * 1985-09-14 1987-03-18 British Petroleum Co Plc Underwater electrically conductive coupling
US4703875A (en) * 1986-07-24 1987-11-03 S. C. Johnson & Son, Inc. Low mass piston for aerosol container
US4741402A (en) * 1986-10-14 1988-05-03 Hughes Tool Company Subsea hydraulic connector with multiple ports
US4749043A (en) * 1986-06-25 1988-06-07 Otis Engineering Corp. Subsurface safety valves and seals
US5058489A (en) * 1989-06-20 1991-10-22 Atsugi Unisia Corporation Piston structure for internal combustion engine
US5143483A (en) * 1991-05-06 1992-09-01 Shell Offshore Inc. Hydraulic stab subassembly for remotely operated vehicle vertical interface tool
US5284205A (en) * 1992-04-01 1994-02-08 Halliburton Company Metal to metal seal for well safety valve
GB2273396A (en) * 1992-08-29 1994-06-15 Martin Robin Bowman Electrical connector
US5476076A (en) * 1994-12-06 1995-12-19 Zhou; Zhishan Internal combustion piston engine utilizing interference movable fit technology

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2197425B (en) * 1986-11-12 1990-02-28 Metal Box Plc Pistons for pressure-dispensing containers

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3326579A (en) * 1964-05-27 1967-06-20 Rockwell Mfg Co Multiple conduit connection
US3693133A (en) * 1969-10-08 1972-09-19 Inst Francais Du Petrole Fluid tight electric connector
USRE31645E (en) * 1977-08-01 1984-08-14 Regan Offshore International, Inc. Safety apparatus for automatically sealing hydraulic lines within a sub-sea well casing
US4460156A (en) * 1981-05-01 1984-07-17 Nl Industries, Inc. Wellhead connector with check valve
GB2180107A (en) * 1985-09-14 1987-03-18 British Petroleum Co Plc Underwater electrically conductive coupling
US4749043A (en) * 1986-06-25 1988-06-07 Otis Engineering Corp. Subsurface safety valves and seals
US4703875A (en) * 1986-07-24 1987-11-03 S. C. Johnson & Son, Inc. Low mass piston for aerosol container
US4741402A (en) * 1986-10-14 1988-05-03 Hughes Tool Company Subsea hydraulic connector with multiple ports
US5058489A (en) * 1989-06-20 1991-10-22 Atsugi Unisia Corporation Piston structure for internal combustion engine
US5143483A (en) * 1991-05-06 1992-09-01 Shell Offshore Inc. Hydraulic stab subassembly for remotely operated vehicle vertical interface tool
US5284205A (en) * 1992-04-01 1994-02-08 Halliburton Company Metal to metal seal for well safety valve
GB2273396A (en) * 1992-08-29 1994-06-15 Martin Robin Bowman Electrical connector
US5476076A (en) * 1994-12-06 1995-12-19 Zhou; Zhishan Internal combustion piston engine utilizing interference movable fit technology

Also Published As

Publication number Publication date
AU4712797A (en) 1998-05-15
BR9711938A (en) 2000-01-18
GB9722056D0 (en) 1997-12-17
NO991804L (en) 1999-04-15
NO991804D0 (en) 1999-04-15
GB2318403A (en) 1998-04-22
GB9621769D0 (en) 1996-12-11

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