CA1314486C - Methode d'amelioration de la reserve de pompage d'un compresseur a flux axial - Google Patents

Methode d'amelioration de la reserve de pompage d'un compresseur a flux axial

Info

Publication number
CA1314486C
CA1314486C CA000483273A CA483273A CA1314486C CA 1314486 C CA1314486 C CA 1314486C CA 000483273 A CA000483273 A CA 000483273A CA 483273 A CA483273 A CA 483273A CA 1314486 C CA1314486 C CA 1314486C
Authority
CA
Canada
Prior art keywords
slot
axial flow
flow compressor
blades
compressor
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 - Lifetime
Application number
CA000483273A
Other languages
English (en)
Inventor
Michael John Charles Waterman
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=26287887&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=CA1314486(C) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Priority claimed from GB8511464A external-priority patent/GB2245312B/en
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of CA1314486C publication Critical patent/CA1314486C/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

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
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/522—Casings; Connections of working fluid for axial pumps especially adapted for elastic fluid pumps
    • F04D29/526—Details of the casing section radially opposing blade tips
    • 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
    • F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/68—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers
    • F04D29/681—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps
    • F04D29/685—Inducing localised fluid recirculation in the stator-rotor interface

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CA000483273A 1984-06-19 1985-06-06 Methode d'amelioration de la reserve de pompage d'un compresseur a flux axial Expired - Lifetime CA1314486C (fr)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
GB8415605 1984-06-19
GB8415605 1984-06-19
GB8511464A GB2245312B (en) 1984-06-19 1985-05-07 Axial flow compressor surge margin improvement
GB8511464 1985-05-07

Publications (1)

Publication Number Publication Date
CA1314486C true CA1314486C (fr) 1993-03-16

Family

ID=26287887

Family Applications (1)

Application Number Title Priority Date Filing Date
CA000483273A Expired - Lifetime CA1314486C (fr) 1984-06-19 1985-06-06 Methode d'amelioration de la reserve de pompage d'un compresseur a flux axial

Country Status (4)

Country Link
CA (1) CA1314486C (fr)
DE (1) DE3521798C2 (fr)
FR (1) FR2669687B1 (fr)
IT (1) IT1235237B (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114576205A (zh) * 2022-03-14 2022-06-03 中国航发湖南动力机械研究所 一种带模式转换的高效自循环处理机匣

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6231301B1 (en) * 1998-12-10 2001-05-15 United Technologies Corporation Casing treatment for a fluid compressor
DE10135003C1 (de) 2001-07-18 2002-10-02 Mtu Aero Engines Gmbh Verdichtergehäusestruktur
DE10205363A1 (de) * 2002-02-08 2003-08-21 Rolls Royce Deutschland Gasturbine
RU2208177C1 (ru) * 2002-07-15 2003-07-10 Открытое акционерное общество Авиамоторный научно-технический комплекс "Союз" Двухконтурный турбореактивный двигатель
FR2882112B1 (fr) 2005-02-16 2007-05-11 Snecma Moteurs Sa Prelevement en tete des roues mobiles de compresseur haute pression de turboreacteur
DE102007037924A1 (de) * 2007-08-10 2009-02-12 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit Ringkanalwandausnehmung
DE102008006739A1 (de) * 2008-01-30 2009-08-13 Daimler Ag Verdichtersystem für eine Brennstoffzellenanordnung, Brennstoffzellenanordnung und Verfahren zur Kontrolle
DE102008011644A1 (de) * 2008-02-28 2009-09-03 Rolls-Royce Deutschland Ltd & Co Kg Gehäusestrukturierung für Axialverdichter im Nabenbereich
DE102011006275A1 (de) 2011-03-28 2012-10-04 Rolls-Royce Deutschland Ltd & Co Kg Stator einer Axialverdichterstufe einer Turbomaschine
DE102011006273A1 (de) 2011-03-28 2012-10-04 Rolls-Royce Deutschland Ltd & Co Kg Rotor einer Axialverdichterstufe einer Turbomaschine
DE102011007767A1 (de) 2011-04-20 2012-10-25 Rolls-Royce Deutschland Ltd & Co Kg Strömungsmaschine
FR2989742B1 (fr) * 2012-04-19 2014-05-09 Snecma Carter de compresseur a cavites a forme amont optimisee
FR3109959B1 (fr) * 2020-05-06 2022-04-22 Safran Helicopter Engines Compresseur de turbomachine comportant une paroi fixe pourvue d’un traitement de forme
FR3147835B1 (fr) * 2023-04-11 2025-04-18 Safran Stator à calage variable amélioré et procédé utilisant un tel stator

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3893787A (en) * 1974-03-14 1975-07-08 United Aircraft Corp Centrifugal compressor boundary layer control
GB1518293A (en) * 1975-09-25 1978-07-19 Rolls Royce Axial flow compressors particularly for gas turbine engines
GB2017228B (en) * 1977-07-14 1982-05-06 Pratt & Witney Aircraft Of Can Shroud for a turbine rotor
JPS6318799Y2 (fr) * 1980-12-02 1988-05-26
US4479755A (en) * 1982-04-22 1984-10-30 A/S Kongsberg Vapenfabrikk Compressor boundary layer bleeding system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114576205A (zh) * 2022-03-14 2022-06-03 中国航发湖南动力机械研究所 一种带模式转换的高效自循环处理机匣
CN114576205B (zh) * 2022-03-14 2023-11-28 中国航发湖南动力机械研究所 一种带模式转换的高效自循环处理机匣

Also Published As

Publication number Publication date
FR2669687A1 (fr) 1992-05-29
IT1235237B (it) 1992-06-26
IT8521142A0 (it) 1985-06-13
FR2669687B1 (fr) 1994-07-01
DE3521798C2 (de) 1993-12-09
DE3521798A1 (de) 1992-08-27

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