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 membersInfo
- 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
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
- F16J15/16—Sealings between relatively-moving surfaces
- F16J15/40—Sealings between relatively-moving surfaces by means of fluid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
- F01D11/025—Seal clearance control; Floating assembly; Adaptation means to differential thermal dilatations
-
- 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
- F16J15/16—Sealings between relatively-moving surfaces
- F16J15/34—Sealings between relatively-moving surfaces with slip-ring pressed against a more or less radial face on one member
- F16J15/3464—Mounting of the seal
- F16J15/3472—Means for centering or aligning the contacting faces
-
- 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
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.
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)
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)
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)
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 |
-
1952
- 1952-06-03 GB GB13996/52A patent/GB734685A/en not_active Expired
-
1953
- 1953-06-04 DE DEB25885A patent/DE974262C/en not_active Expired
Cited By (6)
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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