GB734685A - Improvements in or relating to sealing devices between two relatively movable members - Google Patents

Improvements in or relating to sealing devices between two relatively movable members

Info

Publication number
GB734685A
GB734685A GB13996/52A GB1399652A GB734685A GB 734685 A GB734685 A GB 734685A GB 13996/52 A GB13996/52 A GB 13996/52A GB 1399652 A GB1399652 A GB 1399652A GB 734685 A GB734685 A GB 734685A
Authority
GB
United Kingdom
Prior art keywords
pressure
gap
piston
force
low
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
Application number
GB13996/52A
Inventor
Neville Raymond Lloyd Quinn
Basil Davenport Blackwell
Alexander Scott
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.)
Bristol Aeroplane Co Ltd
Original Assignee
Bristol Aeroplane Co Ltd
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 Bristol Aeroplane Co Ltd filed Critical Bristol Aeroplane Co Ltd
Priority to GB13996/52A priority Critical patent/GB734685A/en
Priority to CH320055D priority patent/CH320055A/en
Priority to DEB25885A priority patent/DE974262C/en
Publication of GB734685A publication Critical patent/GB734685A/en
Expired legal-status Critical Current

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
    • F16J15/00Sealings
    • F16J15/16Sealings between relatively-moving surfaces
    • F16J15/40Sealings between relatively-moving surfaces by means of fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/02Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
    • F01D11/025Seal clearance control; Floating assembly; Adaptation means to differential thermal dilatations
    • 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
    • F16J15/34Sealings between relatively-moving surfaces with slip-ring pressed against a more or less radial face on one member
    • F16J15/3464Mounting of the seal
    • F16J15/3472Means for centering or aligning the contacting faces
    • 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
    • F16J15/44Free-space packings

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Compressor (AREA)
  • Sealing Devices (AREA)

Abstract

734,685. Stuffing-box substitutes; turbines. BRISTOL AEROPLANE CO., Ltd. May 27, 1953 [June 3, 1952], No. 13996/52. Classes 110 (3) and 122 (5). A sealing device for use in power machines operated by compressible fluid pressure comprises maintaining between zero and a maximum dimension a peripheral gap located between two members movable towards and away from one another and separating a zone of high pressure P (high) from a zone of low pressure P (low) by providing (a) a pair of mutually opposed peripheral surfaces on the members defining the gap which converges from the high pressure to the low pressure zone; (b) means for urging the members together with a force which is less than P (high) times the projected area of the opposed surfaces in a direction normal to the force and is not less than the force exerted on the projected area when the gap is open to its maximum dimension ; and (c) means to control the force as a function of P (high) such that the force does not increase due to closure of the gap. An annular piston 4 slidably supported on piston rings 36 in a cylinder 35 formed in a compressor housing 31 has a face 7 separated from an opposed face 6 on the compressor rotor 30 by a gap 8 converging from the higher pressure P (high) to the lower pressure P (low) side of the piston 4 which is urged toward the rotor 30 by fluid admitted from the high-pressure side to the cylinder 35 through a passage 11 and discharged therefrom to the low-pressure side through a nozzle 12, preferably " choked " so that the pressure behind the piston is independent of P (low). The piston 4 is urged away from the rotor 30 by a force equal to the annular area of the face 7 multiplied by the mean pressure in the gap 8 which pressure increases or decreases as the gap decreases or increases ; the gap is thus automatically maintained between predetermined limits. In a modification the cylinder 35 is replaced by a flexible bellows secured to the piston and the housing and the pressure may be admitted to the interior of the bellows from the high-pressure side P (high) through a conduit having its inlet end close to the face 6 to form an entry port therewith which decreases in size as the gap 8 diminishes and thereby produces a fall in the pressure in the bellows. In a further modification the cylinder 35 is formed by a pair of concentric flexible rings attached to the housing and in sliding contact with the piston 4 and having axial slots therein to act as inlet and discharge passages to the space behind the piston.
GB13996/52A 1952-06-03 1952-06-03 Improvements in or relating to sealing devices between two relatively movable members Expired GB734685A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB13996/52A GB734685A (en) 1952-06-03 1952-06-03 Improvements in or relating to sealing devices between two relatively movable members
CH320055D CH320055A (en) 1952-06-03 1953-06-03 Sealing device
DEB25885A DE974262C (en) 1952-06-03 1953-06-04 Gap seal with automatic adjustment of the gap width

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
GB320055X 1952-06-03
GB974262X 1952-06-03
GB13996/52A GB734685A (en) 1952-06-03 1952-06-03 Improvements in or relating to sealing devices between two relatively movable members
GB270553X 1953-05-27

Publications (1)

Publication Number Publication Date
GB734685A true GB734685A (en) 1955-08-03

Family

ID=29407912

Family Applications (1)

Application Number Title Priority Date Filing Date
GB13996/52A Expired GB734685A (en) 1952-06-03 1952-06-03 Improvements in or relating to sealing devices between two relatively movable members

Country Status (2)

Country Link
DE (1) DE974262C (en)
GB (1) GB734685A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4471966A (en) * 1981-08-06 1984-09-18 Jeumont Schneider Apparatus forming a pressure seal for separating two chambers containing fluid placed under different pressures
EP0221198A1 (en) * 1984-11-01 1987-05-13 SKF Nova AB Seal with pressure fluid feed
GB2553565A (en) * 2016-09-09 2018-03-14 Rolls Royce Plc Air riding seal arrangement
WO2019045590A1 (en) * 2017-08-31 2019-03-07 Siemens Aktiengesellschaft Pressure actuated seal arrangement

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1158334B (en) * 1956-05-16 1963-11-28 Garrett Corp Gap seal
DE1650061B2 (en) * 1967-08-30 1969-09-04 Klein Schanzlin & Becker Ag Non-contact mechanical seal

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE164915C (en) *
DE520226C (en) * 1931-03-16 Siemens Schuckertwerke Akt Ges Device to compensate for the axial thrust of an overpressure turbine
DE157512C (en) * 1900-01-01
DE163010C (en) *
DE161322C (en) *
AT73531B (en) * 1913-07-22 1917-07-10 Stefan Von Roeck Seal for piston and piston valve.
AT133039B (en) * 1922-01-12 1933-04-25 Franz Ing Hauber Metal packing.
DE451079C (en) * 1926-10-14 1928-01-17 Georg Stauber Dr Ing Gap seal for centrifugal machines, especially for gas turbines with auxiliary fluid
US1840127A (en) * 1928-03-27 1932-01-05 Westinghouse Electric & Mfg Co Sealing gland for rotatable shafts
DE524515C (en) * 1930-01-04 1931-05-08 Georg Stauber Dr Ing Gap seal for centrifugal machines, especially for gas turbines, with auxiliary fluid
AT142156B (en) * 1934-07-03 1935-06-25 Felix Wankel Sealing body with additional sealing means for openings in machine parts that rub against each other.
DE823238C (en) * 1950-05-21 1951-12-03 Svenska Turbinfab Ab Shaft seal, especially labyrinth seal

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4471966A (en) * 1981-08-06 1984-09-18 Jeumont Schneider Apparatus forming a pressure seal for separating two chambers containing fluid placed under different pressures
EP0221198A1 (en) * 1984-11-01 1987-05-13 SKF Nova AB Seal with pressure fluid feed
GB2553565A (en) * 2016-09-09 2018-03-14 Rolls Royce Plc Air riding seal arrangement
GB2553565B (en) * 2016-09-09 2019-04-10 Rolls Royce Plc Air riding seal arrangement
US10316974B2 (en) 2016-09-09 2019-06-11 Rolls-Royce Plc Air riding seal arrangement
WO2019045590A1 (en) * 2017-08-31 2019-03-07 Siemens Aktiengesellschaft Pressure actuated seal arrangement

Also Published As

Publication number Publication date
DE974262C (en) 1960-11-10

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