GB933944A - Improved sealing arrangement - Google Patents

Improved sealing arrangement

Info

Publication number
GB933944A
GB933944A GB475561A GB475561A GB933944A GB 933944 A GB933944 A GB 933944A GB 475561 A GB475561 A GB 475561A GB 475561 A GB475561 A GB 475561A GB 933944 A GB933944 A GB 933944A
Authority
GB
United Kingdom
Prior art keywords
shaft
ring
contact
urged
pin
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
GB475561A
Inventor
Lindsay Grahame Dawson
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB475561A priority Critical patent/GB933944A/en
Publication of GB933944A publication Critical patent/GB933944A/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
    • F16J15/44Free-space packings

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
  • Sealing Devices (AREA)

Abstract

933,944. Stuffing-box substitutes. ROLLSROYCE Ltd. Jan. 31, 1962 [Feb. 8, 1961], No. 4755/61. Class 122 (5). Sealing means for a rotatable shaft 18 comprises a resilient split sealing ring 20 urged axially by means, e.g. fluid pressure into contact with a radial face 15 on the shaft housing 13 and urged radially by its own resilience into contact with the shaft, means being provided to prevent the ring rotating with the shaft. A pin 30 fixed to the shaft housing extends into a gap 27, Fig. 5, between overlapping end portions 25, 26 of the ring so that any tendency of the ring to rotate with the shaft brings the pin 20 into contact with shoulder 28 or 29 to thereby open the ring slightly and release it from the shaft. The invention is shown applied to a gas-turbine shaft, the ring 30, which may be of cast iron, being urged against the face 15 by a differential pressure.
GB475561A 1961-02-08 1961-02-08 Improved sealing arrangement Expired GB933944A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB475561A GB933944A (en) 1961-02-08 1961-02-08 Improved sealing arrangement

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB475561A GB933944A (en) 1961-02-08 1961-02-08 Improved sealing arrangement

Publications (1)

Publication Number Publication Date
GB933944A true GB933944A (en) 1963-08-14

Family

ID=9783167

Family Applications (1)

Application Number Title Priority Date Filing Date
GB475561A Expired GB933944A (en) 1961-02-08 1961-02-08 Improved sealing arrangement

Country Status (1)

Country Link
GB (1) GB933944A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116624271A (en) * 2023-07-24 2023-08-22 成都中科翼能科技有限公司 Bearing oil baffle assembly of gas turbine shaft

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116624271A (en) * 2023-07-24 2023-08-22 成都中科翼能科技有限公司 Bearing oil baffle assembly of gas turbine shaft
CN116624271B (en) * 2023-07-24 2023-09-15 成都中科翼能科技有限公司 Bearing oil baffle assembly of gas turbine shaft

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