GB1366075A - Bladed fluid flow machines - Google Patents
Bladed fluid flow machinesInfo
- Publication number
- GB1366075A GB1366075A GB4417770A GB4417770A GB1366075A GB 1366075 A GB1366075 A GB 1366075A GB 4417770 A GB4417770 A GB 4417770A GB 4417770 A GB4417770 A GB 4417770A GB 1366075 A GB1366075 A GB 1366075A
- Authority
- GB
- United Kingdom
- Prior art keywords
- platforms
- sept
- clearance
- bolts
- casing
- 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
- 239000012530 fluid Substances 0.000 title 1
- 229920002430 Fibre-reinforced plastic Polymers 0.000 abstract 1
- 238000013016 damping Methods 0.000 abstract 1
- 239000011151 fibre-reinforced plastic Substances 0.000 abstract 1
- 230000000717 retained effect Effects 0.000 abstract 1
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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Turbines (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB4417770A GB1366075A (en) | 1970-09-16 | 1970-09-16 | Bladed fluid flow machines |
| DE2145230A DE2145230C3 (de) | 1970-09-16 | 1971-09-09 | Leitschaufelbefestigung mit Torsionsschwingungsdämpfung für die inneren Enden der Leitschaufelblätter bei Axialströmungsmaschinen |
| FR7133353A FR2106561B1 (cs) | 1970-09-16 | 1971-09-16 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB4417770A GB1366075A (en) | 1970-09-16 | 1970-09-16 | Bladed fluid flow machines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1366075A true GB1366075A (en) | 1974-09-11 |
Family
ID=10432128
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB4417770A Expired GB1366075A (en) | 1970-09-16 | 1970-09-16 | Bladed fluid flow machines |
Country Status (3)
| Country | Link |
|---|---|
| DE (1) | DE2145230C3 (cs) |
| FR (1) | FR2106561B1 (cs) |
| GB (1) | GB1366075A (cs) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2227192A (en) * | 1988-12-29 | 1990-07-25 | Gen Electric | Damped gas turbine engine airfoil row |
| EP1531234A1 (de) * | 2003-11-17 | 2005-05-18 | Rolls-Royce Deutschland Ltd & Co KG | Innendeckband für die Statorschaufeln des Verdichters einer Gasturbine |
| JP2009121460A (ja) * | 2007-11-09 | 2009-06-04 | Snecma | 取付け部品を覆瓦状に配置することによる径方向アームの円形フェルールへの接続 |
| US20160290146A1 (en) * | 2015-03-31 | 2016-10-06 | Ansaldo Energia Ip Uk Limited | Multi-airfoil guide vane unit |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4950129A (en) * | 1989-02-21 | 1990-08-21 | General Electric Company | Variable inlet guide vanes for an axial flow compressor |
| FR2680384B1 (fr) * | 1991-08-13 | 1995-03-10 | Plastiremo | Couronne d'aubage a montage simplifie et aube pour sa realisation. |
| US5704762A (en) * | 1993-11-08 | 1998-01-06 | Alliedsignal Inc. | Ceramic-to-metal stator vane assembly |
| DE69815815T2 (de) * | 1998-05-01 | 2004-05-13 | Techspace Aero, Milmort | Leitbeschaufelung für eine Turbomaschine |
| FR2993804B1 (fr) * | 2012-07-30 | 2015-02-20 | Snecma | Soudage par friction des redresseurs et bras creux sur le carter intermediaire d'une turbomachine |
-
1970
- 1970-09-16 GB GB4417770A patent/GB1366075A/en not_active Expired
-
1971
- 1971-09-09 DE DE2145230A patent/DE2145230C3/de not_active Expired
- 1971-09-16 FR FR7133353A patent/FR2106561B1/fr not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2227192A (en) * | 1988-12-29 | 1990-07-25 | Gen Electric | Damped gas turbine engine airfoil row |
| EP1531234A1 (de) * | 2003-11-17 | 2005-05-18 | Rolls-Royce Deutschland Ltd & Co KG | Innendeckband für die Statorschaufeln des Verdichters einer Gasturbine |
| US7287957B2 (en) | 2003-11-17 | 2007-10-30 | Rolls-Royce Deutschland Ltd & Co Kg | Inner shroud for the stator blades of the compressor of a gas turbine |
| JP2009121460A (ja) * | 2007-11-09 | 2009-06-04 | Snecma | 取付け部品を覆瓦状に配置することによる径方向アームの円形フェルールへの接続 |
| US20160290146A1 (en) * | 2015-03-31 | 2016-10-06 | Ansaldo Energia Ip Uk Limited | Multi-airfoil guide vane unit |
Also Published As
| Publication number | Publication date |
|---|---|
| DE2145230B2 (de) | 1974-01-31 |
| DE2145230C3 (de) | 1974-08-22 |
| FR2106561A1 (cs) | 1972-05-05 |
| DE2145230A1 (de) | 1972-03-23 |
| FR2106561B1 (cs) | 1975-09-26 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed | ||
| PLE | Entries relating assignments, transmissions, licences in the register of patents | ||
| PE20 | Patent expired after termination of 20 years |