GB2001692A - Honeycomb structures: gas turbines - Google Patents
Honeycomb structures: gas turbinesInfo
- Publication number
- GB2001692A GB2001692A GB7828646A GB7828646A GB2001692A GB 2001692 A GB2001692 A GB 2001692A GB 7828646 A GB7828646 A GB 7828646A GB 7828646 A GB7828646 A GB 7828646A GB 2001692 A GB2001692 A GB 2001692A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas turbines
- honeycomb structures
- strips
- honeycomb
- abutting areas
- 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.)
- Granted
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
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
- F01D11/127—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with a deformable or crushable structure, e.g. honeycomb
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/28—Three-dimensional patterned
- F05D2250/283—Three-dimensional patterned honeycomb
Abstract
A honeycomb structure for use in gas turbine engines is made from a plurality of shaped strips (12a, b, etc.) connected together to form the cells, the structure being brazed to a backing sheet 15. Non-abutting areas are formed between the connecting faces (e.g. 14a, 14b) of adjacent strips to prevent capillary flow of molten braze metal to the surface of the honeycomb. The non-abutting areas may be at the top surface, as fig. 1, or intermediate the edges of the strips (fig. 4), <IMAGE>
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB7828646A GB2001692B (en) | 1977-07-29 | 1978-07-03 | Honeycomb structures |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3207177 | 1977-07-29 | ||
GB7828646A GB2001692B (en) | 1977-07-29 | 1978-07-03 | Honeycomb structures |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2001692A true GB2001692A (en) | 1979-02-07 |
GB2001692B GB2001692B (en) | 1982-01-27 |
Family
ID=26261198
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB7828646A Expired GB2001692B (en) | 1977-07-29 | 1978-07-03 | Honeycomb structures |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2001692B (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0081010A2 (en) * | 1981-08-10 | 1983-06-15 | George T. Straza | Interrupted cell honeycomb structure |
GB2128261A (en) * | 1982-09-30 | 1984-04-26 | John R Plautz | Honeycomb structure, e.g. for a turbine shroud |
US4449714A (en) * | 1983-03-22 | 1984-05-22 | Gulf & Western Industries, Inc. | Turbine engine seal and method for repair thereof |
FR2539479A1 (en) * | 1983-01-13 | 1984-07-20 | Campbell James | HONEYCOMB JOINT STRUCTURE |
US7105219B2 (en) | 2004-05-27 | 2006-09-12 | Mitsubishi Heavy Industries, Ltd. | Brazing construction and method of brazing an abradable sealing material |
EP3135869A1 (en) * | 2015-08-25 | 2017-03-01 | Rolls-Royce Deutschland Ltd & Co KG | Sealing element for a turbomachine, corresponding turbomachine and manufacturing process |
-
1978
- 1978-07-03 GB GB7828646A patent/GB2001692B/en not_active Expired
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0081010A2 (en) * | 1981-08-10 | 1983-06-15 | George T. Straza | Interrupted cell honeycomb structure |
EP0081010A3 (en) * | 1981-08-10 | 1983-08-03 | George T. Straza | Interrupted cell honeycomb structure |
GB2128261A (en) * | 1982-09-30 | 1984-04-26 | John R Plautz | Honeycomb structure, e.g. for a turbine shroud |
FR2539479A1 (en) * | 1983-01-13 | 1984-07-20 | Campbell James | HONEYCOMB JOINT STRUCTURE |
US4449714A (en) * | 1983-03-22 | 1984-05-22 | Gulf & Western Industries, Inc. | Turbine engine seal and method for repair thereof |
EP0119343A1 (en) * | 1983-03-22 | 1984-09-26 | Gulf And Western Industries, Inc. | Turbine engine seal and method for repair thereof |
US7105219B2 (en) | 2004-05-27 | 2006-09-12 | Mitsubishi Heavy Industries, Ltd. | Brazing construction and method of brazing an abradable sealing material |
EP3135869A1 (en) * | 2015-08-25 | 2017-03-01 | Rolls-Royce Deutschland Ltd & Co KG | Sealing element for a turbomachine, corresponding turbomachine and manufacturing process |
US10480340B2 (en) | 2015-08-25 | 2019-11-19 | Rolls-Royce Deutschland Ltd & Co Kg | Sealing element for a turbo-machine, turbo-machine comprising a sealing element and method for manufacturing a sealing element |
Also Published As
Publication number | Publication date |
---|---|
GB2001692B (en) | 1982-01-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |