CA2199875C - Purgeur et diffuseur annulaire combines pour conduite intercompresseur de turbine a gaz - Google Patents
Purgeur et diffuseur annulaire combines pour conduite intercompresseur de turbine a gaz Download PDFInfo
- Publication number
- CA2199875C CA2199875C CA002199875A CA2199875A CA2199875C CA 2199875 C CA2199875 C CA 2199875C CA 002199875 A CA002199875 A CA 002199875A CA 2199875 A CA2199875 A CA 2199875A CA 2199875 C CA2199875 C CA 2199875C
- Authority
- CA
- Canada
- Prior art keywords
- flaps
- duct
- wall
- air
- gas turbine
- 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 - Fee Related
Links
- 238000007789 sealing Methods 0.000 claims abstract description 11
- 230000000740 bleeding effect Effects 0.000 claims abstract description 9
- 238000011144 upstream manufacturing Methods 0.000 claims description 7
- 230000001105 regulatory effect Effects 0.000 claims 1
- 238000000926 separation method Methods 0.000 description 6
- 238000009826 distribution Methods 0.000 description 5
- 238000000034 method Methods 0.000 description 5
- 238000009792 diffusion process Methods 0.000 description 4
- 230000005611 electricity Effects 0.000 description 2
- 230000007704 transition Effects 0.000 description 2
- 230000002411 adverse Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 description 1
- 230000035945 sensitivity Effects 0.000 description 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
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/105—Final actuators by passing part of the fluid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/16—Control of working fluid flow
- F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/02—Surge control
- F04D27/0207—Surge control by bleeding, bypassing or recycling fluids
- F04D27/0215—Arrangements therefor, e.g. bleed or by-pass valves
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/02—Surge control
- F04D27/0207—Surge control by bleeding, bypassing or recycling fluids
- F04D27/023—Details or means for fluid extraction
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Turbines (AREA)
Abstract
La présente invention concerne un moteur à turbine à gaz à plusieurs étages comportant un conduit inter-compresseur reliant un compresseur basse pression à un étage compresseur suivant. Ce moteur présente un perfectionnement de l'organe de purge (161) permettant de purger le conduit d'une quantité variable d'air lorsque le moteur fonctionne à charge partielle. L'organe de purge (161) comporte, d'une part un dispositif d'ouverture disposé en périphérie de la paroi externe du conduit, et d'autre part des déflecteurs d'air articulés (161) détournant vers l'extérieur le flux d'air intérieur du conduit, au travers d'ouvertures dans la paroi externe du conduit. Selon la présente invention, les déflecteurs d'air sont des volets (161) formant un alignement circonférentiel, des éléments d'obturation étanches suivant le mouvement des volets et reliant les rives latérales de volets consécutifs (161) de façon à empêcher l'écoulement radial de l'air entre des volets consécutifs.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA002199875A CA2199875C (fr) | 1994-10-06 | 1995-10-05 | Purgeur et diffuseur annulaire combines pour conduite intercompresseur de turbine a gaz |
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA002133793A CA2133793A1 (fr) | 1994-10-06 | 1994-10-06 | Purgeur-diffuseur annulaire a geometrie variable pour conduits jumeles de compresseur |
| CA2,133,793 | 1994-10-06 | ||
| PCT/CA1995/000552 WO1996011340A1 (fr) | 1994-10-06 | 1995-10-05 | Soupape de purge et diffuseur annulaire combines pour conduit inter-compresseur de turbine a gaz |
| CA002199875A CA2199875C (fr) | 1994-10-06 | 1995-10-05 | Purgeur et diffuseur annulaire combines pour conduite intercompresseur de turbine a gaz |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2199875A1 CA2199875A1 (fr) | 1996-04-18 |
| CA2199875C true CA2199875C (fr) | 2002-01-29 |
Family
ID=25677555
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002199875A Expired - Fee Related CA2199875C (fr) | 1994-10-06 | 1995-10-05 | Purgeur et diffuseur annulaire combines pour conduite intercompresseur de turbine a gaz |
Country Status (1)
| Country | Link |
|---|---|
| CA (1) | CA2199875C (fr) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB0229307D0 (en) | 2002-12-17 | 2003-01-22 | Rolls Royce Plc | A diffuser arrangement |
| US7147426B2 (en) | 2004-05-07 | 2006-12-12 | Pratt & Whitney Canada Corp. | Shockwave-induced boundary layer bleed |
| EP2305960B1 (fr) * | 2009-09-28 | 2013-07-31 | Techspace Aero S.A. | Valve de purge dans le canal primaire du compresseur et procédé correspondant de suppression de phénomène de pompage |
| DE102014217831A1 (de) * | 2014-09-05 | 2016-03-10 | Rolls-Royce Deutschland Ltd & Co Kg | Vorrichtung zur Entnahme von Zapfluft und Flugzeugtriebwerk mit mindestens einer Vorrichtung zur Entnahme von Zapfluft |
| FR3059366B1 (fr) * | 2016-11-25 | 2020-10-30 | Safran Aircraft Engines | Turbomachine a double flux equipee d'un systeme de decharge |
-
1995
- 1995-10-05 CA CA002199875A patent/CA2199875C/fr not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| CA2199875A1 (fr) | 1996-04-18 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US5845482A (en) | Combined bleed valve and annular diffuser for gas turbine inter compressor duct | |
| US11391240B2 (en) | Gas turbine engine bifurcation located fan variable area nozzle | |
| US8662417B2 (en) | Gas turbine engine fan variable area nozzle with swivable insert system | |
| US10519898B2 (en) | Fan variable area nozzle for a gas turbine engine fan nacelle with sliding actuation system | |
| EP2504552B1 (fr) | Rail de support pour buse de soufflante à section variable | |
| CN108930557B (zh) | 用于压缩机导叶前缘辅助导叶的方法及系统 | |
| US8365515B2 (en) | Gas turbine engine with fan variable area nozzle, nacelle assembly and method of varying area of a fan nozzle | |
| US20120124964A1 (en) | Gas turbine engine with improved fuel efficiency | |
| US20090097967A1 (en) | Gas turbine engine with variable geometry fan exit guide vane system | |
| US20120233981A1 (en) | Gas turbine engine with low fan pressure ratio | |
| CN104011361B (zh) | 具有用于低风扇压力比的风扇可变面积喷嘴的燃气涡轮发动机 | |
| JPS6039866B2 (ja) | 分割フアン型ガスタービンエンジン | |
| US10794272B2 (en) | Axial and centrifugal compressor | |
| US5311736A (en) | Variable cycle propulsion engine for supersonic aircraft | |
| US20090288387A1 (en) | Gas turbine engine bifurcation located in a fan variable area nozzle | |
| JP2005256835A (ja) | 分岐形の出口ガイドベーン | |
| EP3604741B1 (fr) | Conduit de transition de turbomachines pour larges plages de rapport de dérivation | |
| US20120222398A1 (en) | Gas turbine engine with geared architecture | |
| US20090064659A1 (en) | Gas turbine engine with fan variable area nozzle having a rotational valve system | |
| CN107849928A (zh) | 包括具有可变供给部的被整合至后部机身中的涡轮发动机的航空器 | |
| US8256225B2 (en) | Gas turbine engine with a variable exit area fan nozzle, nacelle assembly of such a engine, and corresponding operating method | |
| US20150192298A1 (en) | Gas turbine engine with improved fuel efficiency | |
| US20100050595A1 (en) | Gas turbine engine with axial movable fan variable area nozzle | |
| CA2199875C (fr) | Purgeur et diffuseur annulaire combines pour conduite intercompresseur de turbine a gaz | |
| EP2115289B1 (fr) | Moteur à turbine à gaz à tuyère de soufflante à section variable à segments rotatifs superposés |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request | ||
| MKLA | Lapsed |