GB820708A - Improvements relating to labyrinth seals - Google Patents
Improvements relating to labyrinth sealsInfo
- Publication number
- GB820708A GB820708A GB15031/58A GB1503158A GB820708A GB 820708 A GB820708 A GB 820708A GB 15031/58 A GB15031/58 A GB 15031/58A GB 1503158 A GB1503158 A GB 1503158A GB 820708 A GB820708 A GB 820708A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ring
- pins
- rotary
- springs
- flange
- 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
- 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
Abstract
820,708. Stuffing-box substitutes. GENERAL MOTORS CORPORATION. May 9, 1958 [May 14, 1957], No. 15031/58. Class 122 (5). A labyrinth seal between rotor and stator parts of an axial-flow compressor comprises rotary and non-rotary rings 31, 34, the latter ring being mounted so that it can move transversely of the rotational axis against resilient frictional resistance effected by springs 46 which are carried on circumferentially-spaced pins 42 passing through clearance holes 43. The pins 42 are secured to a stator part 39 and pass through the clearance holes 43 provided in a flange 37 formed on a ring 36 to which the sealing ring 34 is brazed or welded. The springs 46 are held between collars 47 retained on the pins 42 by pins or keys 48. The thickness of the ring 36 and the distance between the ring 34 and flange 37 are such that, in operation, heat generated by the contact of the ring 34 with ribs 33 formed on the rotary ring 31 is slow to dissipate thereby causing the ring 34 to expand and provide a small working clearance between the two rings.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US820708XA | 1957-05-14 | 1957-05-14 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB820708A true GB820708A (en) | 1959-09-23 |
Family
ID=22168877
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB15031/58A Expired GB820708A (en) | 1957-05-14 | 1958-05-09 | Improvements relating to labyrinth seals |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB820708A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1277680B (en) * | 1966-08-29 | 1968-09-12 | Entwicklungsring Sued G M B H | Jet pipe, especially for aircraft, with at least two pipe sections which can be rotated against one another via a roller bearing |
US4103899A (en) * | 1975-10-01 | 1978-08-01 | United Technologies Corporation | Rotary seal with pressurized air directed at fluid approaching the seal |
-
1958
- 1958-05-09 GB GB15031/58A patent/GB820708A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1277680B (en) * | 1966-08-29 | 1968-09-12 | Entwicklungsring Sued G M B H | Jet pipe, especially for aircraft, with at least two pipe sections which can be rotated against one another via a roller bearing |
US4103899A (en) * | 1975-10-01 | 1978-08-01 | United Technologies Corporation | Rotary seal with pressurized air directed at fluid approaching the seal |
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