IT201900003999A1 - Valvola di comando combinato per sovra-velocita', messa in bandiera ed abilitazione di inversione per un gruppo elica - Google Patents

Valvola di comando combinato per sovra-velocita', messa in bandiera ed abilitazione di inversione per un gruppo elica

Info

Publication number
IT201900003999A1
IT201900003999A1 IT102019000003999A IT201900003999A IT201900003999A1 IT 201900003999 A1 IT201900003999 A1 IT 201900003999A1 IT 102019000003999 A IT102019000003999 A IT 102019000003999A IT 201900003999 A IT201900003999 A IT 201900003999A IT 201900003999 A1 IT201900003999 A1 IT 201900003999A1
Authority
IT
Italy
Prior art keywords
flag
speed
over
control valve
combined control
Prior art date
Application number
IT102019000003999A
Other languages
English (en)
Inventor
Simone Castellani
Giuseppe Cervelli
Original Assignee
Ge Avio Srl
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 Ge Avio Srl filed Critical Ge Avio Srl
Priority to IT102019000003999A priority Critical patent/IT201900003999A1/it
Priority to EP20161704.0A priority patent/EP3712058B1/en
Priority to US16/815,942 priority patent/US12037100B2/en
Priority to CN202010189953.2A priority patent/CN111720177B/zh
Publication of IT201900003999A1 publication Critical patent/IT201900003999A1/it

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
    • 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
    • B64C11/385—Blade pitch-changing mechanisms fluid, e.g. hydraulic comprising feathering, braking or stopping systems
    • 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
    • F01D17/141—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path
    • F01D17/145—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path by means of valves, e.g. for steam turbines
    • 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
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/021—Blade-carrying members, e.g. rotors for flow machines or engines with only one axial stage
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/148—Blades with variable camber, e.g. by ejection of fluid
    • 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
    • F05D2260/00—Function
    • F05D2260/70—Adjusting of angle of incidence or attack of rotating blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Architecture (AREA)
  • Control Of Turbines (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
IT102019000003999A 2019-03-19 2019-03-19 Valvola di comando combinato per sovra-velocita', messa in bandiera ed abilitazione di inversione per un gruppo elica IT201900003999A1 (it)

Priority Applications (4)

Application Number Priority Date Filing Date Title
IT102019000003999A IT201900003999A1 (it) 2019-03-19 2019-03-19 Valvola di comando combinato per sovra-velocita', messa in bandiera ed abilitazione di inversione per un gruppo elica
EP20161704.0A EP3712058B1 (en) 2019-03-19 2020-03-09 Combined overspeed, feathering, and reverse enabler control valve for a propeller assembly
US16/815,942 US12037100B2 (en) 2019-03-19 2020-03-11 Combined overspeed, feathering, and reverse enabler control valve for a propeller assembly
CN202010189953.2A CN111720177B (zh) 2019-03-19 2020-03-18 用于推进器组件的组合超速、顺桨和反向使能器控制阀

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT102019000003999A IT201900003999A1 (it) 2019-03-19 2019-03-19 Valvola di comando combinato per sovra-velocita', messa in bandiera ed abilitazione di inversione per un gruppo elica

Publications (1)

Publication Number Publication Date
IT201900003999A1 true IT201900003999A1 (it) 2020-09-19

Family

ID=66776802

Family Applications (1)

Application Number Title Priority Date Filing Date
IT102019000003999A IT201900003999A1 (it) 2019-03-19 2019-03-19 Valvola di comando combinato per sovra-velocita', messa in bandiera ed abilitazione di inversione per un gruppo elica

Country Status (4)

Country Link
US (1) US12037100B2 (it)
EP (1) EP3712058B1 (it)
CN (1) CN111720177B (it)
IT (1) IT201900003999A1 (it)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20200324877A1 (en) * 2019-04-09 2020-10-15 Pratt & Whitney Canada Corp. Method and system for feathering a propeller
IT201900010929A1 (it) 2019-07-04 2021-01-04 Ge Avio Srl Gruppo elica ed unita' di controllo di passo
US11668253B2 (en) * 2020-10-16 2023-06-06 Pratt & Whitney Canada Corp. System and method for providing in-flight reverse thrust for an aircraft
CN112627992B (zh) * 2020-12-17 2023-03-14 中国航空工业集团公司成都飞机设计研究所 一种发动机控制系统
US11905840B2 (en) * 2021-02-01 2024-02-20 Pratt & Whitney Canada Corp. System and method for detecting failure of a propeller feedback device
EP4046907B1 (en) * 2021-02-23 2024-10-09 Ratier-Figeac SAS Blade pitch control
US12077279B2 (en) 2021-04-27 2024-09-03 Pratt & Whitney Canada Corp. System and method for detecting and mitigating a propeller failure condition
WO2023034027A1 (en) * 2021-09-05 2023-03-09 Muller Peter Jacques Rim driven thruster with adjustable rotor blade pitch
US12006883B2 (en) * 2022-02-04 2024-06-11 Pratt & Whitney Canada Corp. Method and system of operating an airplane engine
CN115593639B (zh) * 2022-09-30 2024-09-17 陕西飞机工业有限责任公司 一种顺桨控制装置
US20240124125A1 (en) * 2022-10-12 2024-04-18 Pratt & Whitney Canada Corp. Back-up protection for uncontrolled fluid pressure increase in propeller control units
US20240150010A1 (en) * 2022-11-08 2024-05-09 Pratt & Whitney Canada Corp. Systems and methods for controlling propeller control unit fluid pressure
US11958589B1 (en) 2022-12-30 2024-04-16 Pratt & Whitney Canada Corp. Controlling rate of rotor feather by primary blade angle control system

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0311277A2 (en) * 1987-10-03 1989-04-12 Dowty Rotol Limited Propeller blade systems
US5174718A (en) * 1991-08-12 1992-12-29 United Technologies Corporation Blade pitch change control system
US20130323050A1 (en) * 2012-05-30 2013-12-05 Woodward, Inc. Electrohydraulic Propeller Governor
EP3434585A1 (en) * 2017-07-28 2019-01-30 General Electric Company Propeller control system for an aircraft

Family Cites Families (15)

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Publication number Priority date Publication date Assignee Title
US2980188A (en) 1958-11-14 1961-04-18 United Aircraft Corp Combined feathering and pitch lock system
US3090445A (en) 1960-12-19 1963-05-21 United Aircraft Corp Simultaneous feather and pitch lock actuator
US3160213A (en) 1961-08-02 1964-12-08 United Aircraft Corp Feather control for aeronautical propellers
US8545178B2 (en) 2006-03-08 2013-10-01 Hamilton Sundstrand Corporation Controlled propeller pitch lock actuation system
FR2928977B1 (fr) 2008-03-21 2010-04-09 Snecma Systeme d'helices contrarotatives disposant d'un dispositif de mise en drapeau des pales d'helices
GB0821239D0 (en) 2008-11-21 2008-12-31 Rolls Royce Plc A machine such as a gas turbine
GB0821783D0 (en) 2008-12-01 2009-01-07 Rolls Royce Plc Blade pitch control system
WO2015052459A1 (en) * 2013-10-07 2015-04-16 Ge Aviation Systems Limited Pitch control assembly
US9561860B2 (en) 2014-08-29 2017-02-07 Tzunum, Inc. System and methods for implementing regional air transit network using hybrid-electric aircraft
US10472050B2 (en) 2016-08-31 2019-11-12 Honeywell International Inc. Propeller pitch control actuation system
US10793256B2 (en) * 2016-09-12 2020-10-06 Pratt & Whitney Canada Corp. Propeller blade angle control system
US10119495B1 (en) 2017-06-28 2018-11-06 General Electric Company System and method of operating a ducted fan propulsion system inflight
US11312476B2 (en) * 2017-09-25 2022-04-26 Woodward, Inc. Propeller control unit
US11554851B2 (en) * 2019-02-15 2023-01-17 Pratt & Whitney Canada Corp. System and method for aircraft propeller governing
IT201900010929A1 (it) * 2019-07-04 2021-01-04 Ge Avio Srl Gruppo elica ed unita' di controllo di passo

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0311277A2 (en) * 1987-10-03 1989-04-12 Dowty Rotol Limited Propeller blade systems
US5174718A (en) * 1991-08-12 1992-12-29 United Technologies Corporation Blade pitch change control system
US20130323050A1 (en) * 2012-05-30 2013-12-05 Woodward, Inc. Electrohydraulic Propeller Governor
EP3434585A1 (en) * 2017-07-28 2019-01-30 General Electric Company Propeller control system for an aircraft

Also Published As

Publication number Publication date
EP3712058A1 (en) 2020-09-23
US12037100B2 (en) 2024-07-16
CN111720177A (zh) 2020-09-29
EP3712058B1 (en) 2024-05-22
US20200298959A1 (en) 2020-09-24
CN111720177B (zh) 2023-03-07

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