GB8619742D0 - Turbine rotor assembly - Google Patents
Turbine rotor assemblyInfo
- Publication number
- GB8619742D0 GB8619742D0 GB868619742A GB8619742A GB8619742D0 GB 8619742 D0 GB8619742 D0 GB 8619742D0 GB 868619742 A GB868619742 A GB 868619742A GB 8619742 A GB8619742 A GB 8619742A GB 8619742 D0 GB8619742 D0 GB 8619742D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotor assembly
- turbine rotor
- turbine
- assembly
- rotor
- 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.)
- Withdrawn
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
- F01D11/005—Sealing means between non relatively rotating elements
- F01D11/006—Sealing the gap between rotor blades or blades and rotor
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
- F01D5/3015—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB08619742A GB2194000A (en) | 1986-08-13 | 1986-08-13 | Turbine rotor assembly with seal plates |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB08619742A GB2194000A (en) | 1986-08-13 | 1986-08-13 | Turbine rotor assembly with seal plates |
Publications (2)
Publication Number | Publication Date |
---|---|
GB8619742D0 true GB8619742D0 (en) | 1987-03-18 |
GB2194000A GB2194000A (en) | 1988-02-24 |
Family
ID=10602676
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB08619742A Withdrawn GB2194000A (en) | 1986-08-13 | 1986-08-13 | Turbine rotor assembly with seal plates |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2194000A (en) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6171058B1 (en) * | 1999-04-01 | 2001-01-09 | General Electric Company | Self retaining blade damper |
US7097429B2 (en) * | 2004-07-13 | 2006-08-29 | General Electric Company | Skirted turbine blade |
US7918265B2 (en) * | 2008-02-14 | 2011-04-05 | United Technologies Corporation | Method and apparatus for as-cast seal on turbine blades |
DE102011077501A1 (en) | 2011-06-14 | 2012-12-20 | Rolls-Royce Deutschland Ltd & Co Kg | Rotor device for a jet engine with a disc wheel and a plurality of blades |
US9140136B2 (en) | 2012-05-31 | 2015-09-22 | United Technologies Corporation | Stress-relieved wire seal assembly for gas turbine engines |
US9511418B2 (en) | 2012-10-01 | 2016-12-06 | United Technologies Corporation | Method of casting parts using heat reservoir, gating used by such method, and casting made thereby |
EP2955328B1 (en) * | 2014-06-11 | 2019-02-06 | Ansaldo Energia Switzerland AG | Rotor assembly for gas turbine with a sealing wire |
FR3024491B1 (en) * | 2014-08-01 | 2018-12-07 | Safran Aircraft Engines | ROTARY ASSEMBLY FOR TURBOMACHINE WITH DEVICE FOR PLACING AUBES |
EP3034795B1 (en) * | 2014-12-17 | 2019-02-27 | Ansaldo Energia Switzerland AG | Lock plate with radial grooves |
GB201516657D0 (en) | 2015-09-21 | 2015-11-04 | Rolls Royce Plc | Seal-plate anti-rotation in a stage of a gas turbine engine |
US10458244B2 (en) * | 2017-10-18 | 2019-10-29 | United Technologies Corporation | Tuned retention ring for rotor disk |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1295003A (en) * | 1971-06-15 | 1972-11-01 | ||
US3936222A (en) * | 1974-03-28 | 1976-02-03 | United Technologies Corporation | Gas turbine construction |
-
1986
- 1986-08-13 GB GB08619742A patent/GB2194000A/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
GB2194000A (en) | 1988-02-24 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |