GB643604A - Improvements in or relating to glands for rotary machines - Google Patents
Improvements in or relating to glands for rotary machinesInfo
- Publication number
- GB643604A GB643604A GB857048A GB857048A GB643604A GB 643604 A GB643604 A GB 643604A GB 857048 A GB857048 A GB 857048A GB 857048 A GB857048 A GB 857048A GB 643604 A GB643604 A GB 643604A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ring
- housing
- radial
- wall
- lugs
- 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
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
- F16J15/44—Free-space packings
- F16J15/441—Free-space packings with floating ring
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
Abstract
643,604. Stuffing-box substitutes. HALL, J. S., GARLAND, J., and METROPOLITAN-VICKERS ELECTRICAL CO., Ltd. March 23, 1948, No. 8570. [Class 122(v)] A gland for a rotary pump or turbine machine comprises a labyrinth gland ring 1 mounted on the machine shaft 9 and located against an end wall 11 of the machine casing by an annular housing 12 adapted to be secured against the end wall 11 in pressure tight relationship therewith by a detachable or integrally formed flange member 21, the ring 1 having a plurality of peripheral projections 6 which extend into complementary recesses 17 in the housing in a manner to permit relative radial displacement of the ring and housing, and the ring also having a radial face '3 for cooperating with a corresponding radial face 16 on the housing 12 to provide a pressure tight seal between the ring and the housing. Four lugs 6 equi-spaced on a circumferential flange 2 on the ring 1 extend with radial and axial clearance into the complementary recesses 17 in the housing 1 which is prevented from rotating by two slots in it engaging corresponding studs fitted in the wall 11. Flexibility between the ring and housing may be provided by a pair of spring-tensioned piston members which slide in circumferentially directed bores in one radial wall of each of the lugs 6 and carry a flat plate which is forced against the opposite side wall of the recess 17.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB857048A GB643604A (en) | 1948-03-23 | 1948-03-23 | Improvements in or relating to glands for rotary machines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB857048A GB643604A (en) | 1948-03-23 | 1948-03-23 | Improvements in or relating to glands for rotary machines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB643604A true GB643604A (en) | 1950-09-20 |
Family
ID=9855019
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB857048A Expired GB643604A (en) | 1948-03-23 | 1948-03-23 | Improvements in or relating to glands for rotary machines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB643604A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1187874B (en) * | 1962-05-23 | 1965-02-25 | Licentia Gmbh | Non-contact shaft seal for turbo machines |
US3529904A (en) * | 1968-10-28 | 1970-09-22 | Westinghouse Electric Corp | Diaphragm seal structure |
US4330133A (en) * | 1979-02-17 | 1982-05-18 | Rolls-Royce Limited | Dual-ring seal with temperature compensation |
WO2004101957A1 (en) * | 2003-05-08 | 2004-11-25 | Mtu Aero Engines Gmbh | Hub-centered brush seal arrangement for use in a gas turbine |
-
1948
- 1948-03-23 GB GB857048A patent/GB643604A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1187874B (en) * | 1962-05-23 | 1965-02-25 | Licentia Gmbh | Non-contact shaft seal for turbo machines |
US3529904A (en) * | 1968-10-28 | 1970-09-22 | Westinghouse Electric Corp | Diaphragm seal structure |
US4330133A (en) * | 1979-02-17 | 1982-05-18 | Rolls-Royce Limited | Dual-ring seal with temperature compensation |
WO2004101957A1 (en) * | 2003-05-08 | 2004-11-25 | Mtu Aero Engines Gmbh | Hub-centered brush seal arrangement for use in a gas turbine |
US7516962B2 (en) | 2003-05-08 | 2009-04-14 | Mtu Aero Engines Gmbh | Spoke-centered brush seal arrangement for use in a gas turbine |
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