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FR1050166A - Système d'embiellage - Google Patents
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FR1050166A - Système d'embiellage - Google Patents

Système d'embiellage

Info

Publication number
FR1050166A
FR1050166A FR1050166DA FR1050166A FR 1050166 A FR1050166 A FR 1050166A FR 1050166D A FR1050166D A FR 1050166DA FR 1050166 A FR1050166 A FR 1050166A
Authority
FR
France
Prior art keywords
linkage system
linkage
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
Application number
Other languages
English (en)
Inventor
Amand-Rene Gorvel
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
Application filed filed Critical
Application granted granted Critical
Publication of FR1050166A publication Critical patent/FR1050166A/fr
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00Regulating or controlling by varying flow
    • F01D17/10Final actuators
    • F01D17/12Final actuators arranged in stator parts
    • F01D17/14Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162Final 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H21/00Gearings comprising primarily only links or levers, with or without slides
    • F16H21/10Gearings comprising primarily only links or levers, with or without slides all movement being in, or parallel to, a single plane
    • F16H21/16Gearings comprising primarily only links or levers, with or without slides all movement being in, or parallel to, a single plane for interconverting rotary motion and reciprocating motion
    • F16H21/18Crank gearings; Eccentric gearings
    • F16H21/36Crank gearings; Eccentric gearings without swinging connecting-rod, e.g. with epicyclic parallel motion, slot-and-crank motion
    • F16H21/365Crank gearings; Eccentric gearings without swinging connecting-rod, e.g. with epicyclic parallel motion, slot-and-crank motion with orbital gearing having a ratio of 2:1 between central gear and orbital gear

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1050166D 1952-06-04 1952-02-04 Système d'embiellage Expired FR1050166A (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB317621X 1952-06-04
GB130553X 1953-05-13

Publications (1)

Publication Number Publication Date
FR1050166A true FR1050166A (fr) 1954-01-05

Family

ID=26249483

Family Applications (2)

Application Number Title Priority Date Filing Date
FR1050166D Expired FR1050166A (fr) 1952-06-04 1952-02-04 Système d'embiellage
FR1080166D Expired FR1080166A (fr) 1952-06-04 1953-06-01 Perfectionnements aux machines à fluide à écoulement axial

Family Applications After (1)

Application Number Title Priority Date Filing Date
FR1080166D Expired FR1080166A (fr) 1952-06-04 1953-06-01 Perfectionnements aux machines à fluide à écoulement axial

Country Status (4)

Country Link
US (1) US2838274A (fr)
CH (1) CH317621A (fr)
FR (2) FR1050166A (fr)
GB (1) GB736796A (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2842305A (en) * 1955-11-01 1958-07-08 Gen Electric Compressor stator assembly
DE1136350B (de) * 1959-08-11 1962-09-13 Entwicklungsbau Pirna Veb Verstellvorrichtung fuer Leitschaufelkraenze einer Axial-Stroemungsmaschine
US3887297A (en) * 1974-06-25 1975-06-03 United Aircraft Corp Variable leading edge stator vane assembly
US4013377A (en) * 1975-10-08 1977-03-22 Westinghouse Electric Corporation Intermediate transition annulus for a two shaft gas turbine engine
US3990810A (en) * 1975-12-23 1976-11-09 Westinghouse Electric Corporation Vane assembly for close coupling the compressor turbine and a single stage power turbine of a two-shaped gas turbine
US4428714A (en) 1981-08-18 1984-01-31 A/S Kongsberg Vapenfabrikk Pre-swirl inlet guide vanes for compressor
USRE32756E (en) * 1981-08-18 1988-09-27 A/S Kongsberg Vapenfabrikk Pre-swirl inlet guide vane for compressor
GB9203168D0 (en) * 1992-02-13 1992-04-01 Rolls Royce Plc Guide vanes for gas turbine engines
RU2199670C1 (ru) * 2001-07-16 2003-02-27 Открытое Акционерное Общество "А. Люлька-Сатурн" Регулируемый входной направляющий аппарат компрессора газотурбинного двигателя
WO2021138538A1 (fr) * 2020-01-03 2021-07-08 University Of Kansas Procédés et systèmes d'atténuation du bruit de jet à grande vitesse

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2316813A (en) * 1939-07-22 1943-04-20 Holzwarth Gas Turbine Co Bearer for the stationary vanes of rotary motors
GB540707A (en) * 1940-09-18 1941-10-27 Davidson & Co Ltd Improvements relating to multi-stage axial flow fans, pumps and the like
US2382913A (en) * 1943-04-12 1945-08-14 Gen Electric Centrifugal compressor
US2412365A (en) * 1943-10-26 1946-12-10 Wright Aeronautical Corp Variable turbine nozzle
US2648195A (en) * 1945-12-28 1953-08-11 Rolls Royce Centrifugal compressor for supercharging internal-combustion engines
US2613029A (en) * 1947-06-04 1952-10-07 Rolls Royce Axial flow compressor regulation
BE501031A (fr) * 1950-02-03

Also Published As

Publication number Publication date
US2838274A (en) 1958-06-10
CH317621A (de) 1956-11-30
FR1080166A (fr) 1954-12-07
GB736796A (en) 1955-09-14

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