FR2402765A1 - Dispositif pour reduire les pertes par interstices qui se produisent avec des aubes directrices reglables de turbo-machines, notamment de propulseurs pour turbines a gaz - Google Patents
Dispositif pour reduire les pertes par interstices qui se produisent avec des aubes directrices reglables de turbo-machines, notamment de propulseurs pour turbines a gazInfo
- Publication number
- FR2402765A1 FR2402765A1 FR7824444A FR7824444A FR2402765A1 FR 2402765 A1 FR2402765 A1 FR 2402765A1 FR 7824444 A FR7824444 A FR 7824444A FR 7824444 A FR7824444 A FR 7824444A FR 2402765 A1 FR2402765 A1 FR 2402765A1
- Authority
- FR
- France
- Prior art keywords
- interstices
- occur
- gas turbine
- blade
- reducing losses
- 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
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
- 238000005096 rolling process Methods 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
-
- 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
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
- F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
- F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/08—Sealings
- F04D29/083—Sealings especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/54—Fluid-guiding means, e.g. diffusers
- F04D29/56—Fluid-guiding means, e.g. diffusers adjustable
- F04D29/563—Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/4932—Turbomachine making
- Y10T29/49321—Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
a. Dispositif pour réduire les pertes par interstices qui se produisent avec des aubes directrices réglables de turbo-machines, notamment de propulseurs pour turbines à gaz. b. Dispositif caractérisé en ce que des rainures disposées dans la paroi extérieure du canal de circulation au-dessus d'une arête inférieure de pale d'aube, antérieure et/ou postérieure, sont remplies avec une garniture de roulement pour aube qui est souple, et à partir de laquelle, au moyen d'un outil ou simulateur d'aube, sont pratiquées des encoches se situant tout juste au-dessus du plan de pivotement des arêtes inférieures d'aubes considérées. c. L'invention trouve son application dans le domaine des turbines à gaz.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE2740192A DE2740192C2 (de) | 1977-09-07 | 1977-09-07 | Spaltdichtung für eine um ihre Längsachse verstellbare, axial umströmte Leitschaufel einer Strömungsmaschine |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2402765A1 true FR2402765A1 (fr) | 1979-04-06 |
FR2402765B3 FR2402765B3 (fr) | 1981-04-30 |
Family
ID=6018274
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7824444A Granted FR2402765A1 (fr) | 1977-09-07 | 1978-08-23 | Dispositif pour reduire les pertes par interstices qui se produisent avec des aubes directrices reglables de turbo-machines, notamment de propulseurs pour turbines a gaz |
Country Status (4)
Country | Link |
---|---|
US (1) | US4195964A (fr) |
DE (1) | DE2740192C2 (fr) |
FR (1) | FR2402765A1 (fr) |
GB (1) | GB2003984B (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2021224558A1 (fr) * | 2020-05-06 | 2021-11-11 | Safran Helicopter Engines | Compresseur de turbomachine comportant une paroi fixe pourvue d'un traitement de forme |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2835349C2 (de) * | 1978-08-11 | 1979-12-20 | Mtu Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen | Verstelleitgitter für hochbelastete Verdichter, insbesondere von Gasturbinentriebwerken |
US4307994A (en) * | 1979-10-15 | 1981-12-29 | General Motors Corporation | Variable vane position adjuster |
FR2646467A1 (fr) * | 1989-04-26 | 1990-11-02 | Snecma | Aube de stator a calage variable a coupelle rapportee |
DE10016745B4 (de) | 2000-04-04 | 2005-05-19 | Man B & W Diesel Ag | Axialströmungsmaschine mit einem eine Reihe von verstellbaren Leitschaufeln umfassenden Leitapparat |
US6409471B1 (en) | 2001-02-16 | 2002-06-25 | General Electric Company | Shroud assembly and method of machining same |
US8033782B2 (en) * | 2008-01-16 | 2011-10-11 | Elliott Company | Method to prevent brinelling wear of slot and pin assembly |
US9638212B2 (en) * | 2013-12-19 | 2017-05-02 | Pratt & Whitney Canada Corp. | Compressor variable vane assembly |
US20170044927A1 (en) * | 2014-04-30 | 2017-02-16 | Borgwarner Inc. | Lock-up prevention vane for variable geometry turbocharger |
US20160010488A1 (en) * | 2014-07-08 | 2016-01-14 | MTU Aero Engines AG | Wear protection arrangement for a turbomachine, process and compressor |
BE1024523B1 (fr) * | 2016-08-30 | 2018-03-29 | Safran Aero Boosters S.A. | Stator a aubes ajustables pour compresseur de turbomachine axiale |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL67182C (fr) * | ||||
US1478053A (en) * | 1923-12-18 | Guide vane eor hydraulic turbines | ||
US1817654A (en) * | 1930-08-27 | 1931-08-04 | Newport News S & D Co | Adjustable seal for hydraulic turbine gates and the like |
GB578034A (en) * | 1944-08-10 | 1946-06-12 | William Warren Triggs | Improvements in and relating to hydraulic turbines applicable also to centrifugal pumps |
GB1049080A (en) * | 1963-12-02 | 1966-11-23 | Gen Electric | Improvements in adjustable stator vanes |
US3547455A (en) * | 1969-05-02 | 1970-12-15 | Gen Electric | Rotary seal including organic abradable material |
GB1276720A (en) * | 1969-12-19 | 1972-06-07 | English Electric Co Ltd | Drives to adjustable stator blades for turbomachinery |
US3788763A (en) * | 1972-11-01 | 1974-01-29 | Gen Motors Corp | Variable vanes |
US3995971A (en) * | 1975-06-02 | 1976-12-07 | United Technologies Corporation | Rotatable vane seal |
-
1977
- 1977-09-07 DE DE2740192A patent/DE2740192C2/de not_active Expired
-
1978
- 1978-08-14 US US05/933,191 patent/US4195964A/en not_active Expired - Lifetime
- 1978-08-23 FR FR7824444A patent/FR2402765A1/fr active Granted
- 1978-09-07 GB GB7835984A patent/GB2003984B/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2021224558A1 (fr) * | 2020-05-06 | 2021-11-11 | Safran Helicopter Engines | Compresseur de turbomachine comportant une paroi fixe pourvue d'un traitement de forme |
FR3109959A1 (fr) * | 2020-05-06 | 2021-11-12 | Safran Helicopter Engines | Compresseur de turbomachine comportant une paroi fixe pourvue d’un traitement de forme |
Also Published As
Publication number | Publication date |
---|---|
FR2402765B3 (fr) | 1981-04-30 |
DE2740192A1 (de) | 1979-03-08 |
DE2740192C2 (de) | 1981-11-12 |
US4195964A (en) | 1980-04-01 |
GB2003984A (en) | 1979-03-21 |
GB2003984B (en) | 1982-02-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |