PL413811A1 - Układ i sposób regulacji skoku śmigła - Google Patents

Układ i sposób regulacji skoku śmigła

Info

Publication number
PL413811A1
PL413811A1 PL413811A PL41381115A PL413811A1 PL 413811 A1 PL413811 A1 PL 413811A1 PL 413811 A PL413811 A PL 413811A PL 41381115 A PL41381115 A PL 41381115A PL 413811 A1 PL413811 A1 PL 413811A1
Authority
PL
Poland
Prior art keywords
pitch
otb
flange
pitch adjustment
main channel
Prior art date
Application number
PL413811A
Other languages
English (en)
Other versions
PL226825B1 (pl
Inventor
Krzysztof Miszkiewicz
Aleksander Krzysztof Szymandera
Piotr Szymański
Adam Przadka
Original Assignee
General Electric Company
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 by General Electric Company filed Critical General Electric Company
Priority to PL413811A priority Critical patent/PL226825B1/pl
Priority to JP2016166483A priority patent/JP2017095082A/ja
Priority to US15/251,294 priority patent/US10543901B2/en
Priority to CA2940848A priority patent/CA2940848A1/en
Priority to BR102016020534A priority patent/BR102016020534A2/pt
Priority to EP16187701.4A priority patent/EP3144219A1/en
Priority to CN201610807190.7A priority patent/CN106499521B/zh
Publication of PL413811A1 publication Critical patent/PL413811A1/pl
Publication of PL226825B1 publication Critical patent/PL226825B1/pl

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/30—Blade pitch-changing mechanisms
    • B64C11/38—Blade pitch-changing mechanisms fluid, e.g. hydraulic
    • B64C11/40—Blade pitch-changing mechanisms fluid, e.g. hydraulic automatic
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/30—Blade pitch-changing mechanisms
    • B64C11/306—Blade pitch-changing mechanisms specially adapted for contrarotating propellers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/30—Blade pitch-changing mechanisms
    • B64C11/38—Blade pitch-changing mechanisms fluid, e.g. hydraulic
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/46—Arrangements of, or constructional features peculiar to, multiple propellers
    • B64C11/48—Units of two or more coaxial propellers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/107—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with two or more rotors connected by power transmission
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/20—Adaptations of gas-turbine plants for driving vehicles
    • 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
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/34—Blade mountings
    • F04D29/36—Blade mountings adjustable
    • F04D29/362—Blade mountings adjustable during rotation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/325—Application in turbines in gas turbines to drive unshrouded, high solidity propeller
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/60—Control system actuates means
    • F05D2270/64—Hydraulic actuators
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Hydraulic Motors (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
  • Wind Motors (AREA)

Abstract

Ujawniono układy i sposoby do regulacji kąta skoku śmigła i zespół wirnikowy, który selektywnie ogranicza kąt skoku w zależności od wybranego trybu pracy. Układ zawiera kołnierz (48) z precyzyjnym zatrzymaniem wyznaczający kanał główny, łożysko olejowe (OTB) biegnące w poprzek kołnierza z precyzyjnym zatrzymaniem, tłok siłownika połączony z wałem korbowym łopaty śmigła do zmiany skoku łopat śmigła, gdzie tłok pierścieniowy jest umieszczony wokół OTB w połączeniu płynu z kanałem głównym.
PL413811A 2015-09-07 2015-09-07 Układ isposób regulacji skoku smigła PL226825B1 (pl)

Priority Applications (7)

Application Number Priority Date Filing Date Title
PL413811A PL226825B1 (pl) 2015-09-07 2015-09-07 Układ isposób regulacji skoku smigła
JP2016166483A JP2017095082A (ja) 2015-09-07 2016-08-29 プロペラピッチを制御するためのシステム及び方法
US15/251,294 US10543901B2 (en) 2015-09-07 2016-08-30 System and method for controlling propeller pitch
CA2940848A CA2940848A1 (en) 2015-09-07 2016-09-01 System and method for controlling propeller pitch
BR102016020534A BR102016020534A2 (pt) 2015-09-07 2016-09-06 sistema de mudança de passo e método para controlar um ângulo de passo de uma linha de pás propulsoras
EP16187701.4A EP3144219A1 (en) 2015-09-07 2016-09-07 System and method for controlling propeller pitch
CN201610807190.7A CN106499521B (zh) 2015-09-07 2016-09-07 用于控制螺旋桨桨距的系统和方法

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL413811A PL226825B1 (pl) 2015-09-07 2015-09-07 Układ isposób regulacji skoku smigła

Publications (2)

Publication Number Publication Date
PL413811A1 true PL413811A1 (pl) 2017-03-13
PL226825B1 PL226825B1 (pl) 2017-09-29

Family

ID=56896390

Family Applications (1)

Application Number Title Priority Date Filing Date
PL413811A PL226825B1 (pl) 2015-09-07 2015-09-07 Układ isposób regulacji skoku smigła

Country Status (7)

Country Link
US (1) US10543901B2 (pl)
EP (1) EP3144219A1 (pl)
JP (1) JP2017095082A (pl)
CN (1) CN106499521B (pl)
BR (1) BR102016020534A2 (pl)
CA (1) CA2940848A1 (pl)
PL (1) PL226825B1 (pl)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
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FR2980770B1 (fr) * 2011-10-03 2014-06-27 Snecma Turbomachine a helice(s) pour aeronef avec systeme pour changer le pas de l'helice.
EP3434585B1 (en) * 2017-07-28 2021-04-14 General Electric Company Propeller control system for an aircraft
FR3072714B1 (fr) * 2017-10-24 2019-09-27 Safran Transmission Systems Tube de transfert d'huile pour un systeme de commande de regulation du pas d'une helice de turbomachine
FR3123313B1 (fr) * 2021-05-28 2023-05-26 Safran Aircraft Engines Mécanisme de changement de pas comprenant un actionneur électrohydraulique amélioré
FR3130894B1 (fr) 2021-12-20 2024-09-06 Safran Aircraft Engines Module de turbomachine equipe d’aubes a calage variable et d’une virole annulaire d’interface
FR3130878A1 (fr) 2021-12-20 2023-06-23 Safran Aircraft Engines Ensemble pour turbomachine comprenant un moyen de commande et un dispostif de transfert de fluide integre au moyen de commande
FR3130877B1 (fr) 2021-12-20 2024-10-25 Safran Aircraft Engines Dispostif de transfert de fluide avec moyens de connexion hydraulique et mecanique
IT202200022992A1 (it) 2022-11-08 2024-05-08 Ge Avio Srl Elica a passo variabile di un motore a turbina a gas
FR3154447A1 (fr) * 2023-10-20 2025-04-25 Safran Aircraft Engines Dispositif de transfert fluidique multivoies comprenant des bagues contribuant à définir une surface interne de partie périphérique
FR3154453B1 (fr) * 2023-10-20 2025-10-31 Safran Aircraft Engines Dispositif de transfert fluidique multivoies à partie périphérique pourvue d’une frette
US12504029B2 (en) 2024-02-20 2025-12-23 Pratt & Whitney Canada Corp. Aerospace actuator stroke limiting device
FR3163704A1 (fr) * 2024-06-20 2025-12-26 Safran Aircraft Engines Procédé de fabrication d’un dispositif pour transférer du fluide comprenant des mesures pour protéger un joint d’étanchéité vis-à-vis d’une arête formée par un orifice de sortie d’un canal tubulaire

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US3096043A (en) 1960-05-10 1963-07-02 Aviation Louis Breguet Sa Aerodynes having a slipstream-assisted wing system
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US4523891A (en) 1983-06-15 1985-06-18 United Technologies Corporation Propeller pitch change actuation system
GB8609554D0 (en) * 1986-04-18 1986-05-21 Dowty Rotol Ltd Bladed rotor assembly
US4936746A (en) 1988-10-18 1990-06-26 United Technologies Corporation Counter-rotation pitch change system
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US5186608A (en) 1991-10-25 1993-02-16 United Technologies Corporation Hydraulic low pitch switch for propeller pitch change system
US6811376B2 (en) 2002-03-19 2004-11-02 Hamilton Sundstrand Actuation system for a controllable pitch propeller
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Also Published As

Publication number Publication date
CN106499521A (zh) 2017-03-15
CA2940848A1 (en) 2017-03-07
US20170066524A1 (en) 2017-03-09
US10543901B2 (en) 2020-01-28
PL226825B1 (pl) 2017-09-29
JP2017095082A (ja) 2017-06-01
EP3144219A1 (en) 2017-03-22
BR102016020534A2 (pt) 2017-03-14
CN106499521B (zh) 2020-05-22

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