FR3048675B1 - Alimentation en air d'un circuit de conditionnement d'air d'une cabine d'un aeronef - Google Patents

Alimentation en air d'un circuit de conditionnement d'air d'une cabine d'un aeronef Download PDF

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Publication number
FR3048675B1
FR3048675B1 FR1652122A FR1652122A FR3048675B1 FR 3048675 B1 FR3048675 B1 FR 3048675B1 FR 1652122 A FR1652122 A FR 1652122A FR 1652122 A FR1652122 A FR 1652122A FR 3048675 B1 FR3048675 B1 FR 3048675B1
Authority
FR
France
Prior art keywords
rotor
conditioning circuit
gearbox
rotation
low pressure
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.)
Active
Application number
FR1652122A
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English (en)
Other versions
FR3048675A1 (fr
Inventor
Julien Alexis Louis Ricordeau
Marc Missout
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR1652122A priority Critical patent/FR3048675B1/fr
Priority to GB1703906.6A priority patent/GB2549597B/en
Priority to US15/457,773 priority patent/US10662960B2/en
Publication of FR3048675A1 publication Critical patent/FR3048675A1/fr
Application granted granted Critical
Publication of FR3048675B1 publication Critical patent/FR3048675B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • 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
    • F04D27/004—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids by varying driving speed
    • 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
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D13/02—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being pressurised
    • 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
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
    • 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
    • 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
    • F02C6/206—Adaptations of gas-turbine plants for driving vehicles the vehicles being airscrew driven
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00—Pumping installations or systems
    • F04D25/02—Units comprising pumps and their driving means
    • F04D25/028—Units comprising pumps and their driving means the driving means being a planetary gear
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00—Pumping installations or systems
    • F04D25/02—Units comprising pumps and their driving means
    • F04D25/06—Units comprising pumps and their driving means the pump being electrically driven
    • 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
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
    • B64D2013/0603—Environmental Control Systems
    • B64D2013/0644—Environmental Control Systems including electric motors or generators
    • 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
    • F05D2260/40—Transmission of power
    • F05D2260/403—Transmission of power through the shape of the drive components
    • F05D2260/4031—Transmission of power through the shape of the drive components as in toothed gearing
    • F05D2260/40311—Transmission of power through the shape of the drive components as in toothed gearing of the epicyclical, planetary or differential type
    • 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
    • Y02T50/50—On board measures aiming to increase energy efficiency
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Pulmonology (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
  • Supercharger (AREA)

Abstract

Turbopropulseur (110) d'aéronef, comportant au moins un corps basse pression (12) et un corps haute pression (14), le corps basse pression entraînant une hélice de propulsion par l'intermédiaire d'une boîte d'engrenages (16), le turbopropulseur comportant en outre des moyens d'alimentation en air d'un circuit (36) de conditionnement d'air d'une cabine de l'aéronef, lesdits moyens d'alimentation comportant un compresseur de charge (60) dont un rotor (61) est accouplé audit corps basse pression par l'intermédiaire de ladite boîte d'engrenages, caractérisé en ce que lesdits moyens d'alimentation comprennent en outre des moyens de régulation de la vitesse de rotation du rotor (61) dudit compresseur (60), qui comprennent un moteur électrique (70), et un différentiel mécanique (72) d'accouplement d'un premier arbre de sortie (74) dudit moteur électrique, avec un second arbre de sortie (76) de ladite boîte d'engrenages, et avec ledit rotor (61) du compresseur, de façon à ce que la vitesse de rotation (V3) dudit rotor soit fonction des vitesses de rotation (V1, V2) respectives desdits premier et second arbres de sortie.
FR1652122A 2016-03-14 2016-03-14 Alimentation en air d'un circuit de conditionnement d'air d'une cabine d'un aeronef Active FR3048675B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1652122A FR3048675B1 (fr) 2016-03-14 2016-03-14 Alimentation en air d'un circuit de conditionnement d'air d'une cabine d'un aeronef
GB1703906.6A GB2549597B (en) 2016-03-14 2017-03-10 Supply of air to an air-conditioning circuit of an aircraft cabin
US15/457,773 US10662960B2 (en) 2016-03-14 2017-03-13 Supply of air to an air-conditioning circuit of an aircraft cabin

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1652122A FR3048675B1 (fr) 2016-03-14 2016-03-14 Alimentation en air d'un circuit de conditionnement d'air d'une cabine d'un aeronef

Publications (2)

Publication Number Publication Date
FR3048675A1 FR3048675A1 (fr) 2017-09-15
FR3048675B1 true FR3048675B1 (fr) 2022-02-18

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
FR1652122A Active FR3048675B1 (fr) 2016-03-14 2016-03-14 Alimentation en air d'un circuit de conditionnement d'air d'une cabine d'un aeronef

Country Status (3)

Country Link
US (1) US10662960B2 (fr)
FR (1) FR3048675B1 (fr)
GB (1) GB2549597B (fr)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10731501B2 (en) * 2016-04-22 2020-08-04 Hamilton Sundstrand Corporation Environmental control system utilizing a motor assist and an enhanced compressor
GB2570478A (en) 2018-01-26 2019-07-31 Rolls Royce Plc Cabin blower system
GB2570475B (en) * 2018-01-26 2020-04-08 Rolls Royce Plc Cabin blower system
US11629646B2 (en) 2018-09-28 2023-04-18 Raytheon Technologies Corporation Differential geared amplification of auxiliary power unit
CA3115964C (fr) * 2018-11-06 2023-09-26 Ihi Corporation Dispositif de climatisation d'aeronef
US11697505B2 (en) 2019-03-01 2023-07-11 Pratt & Whitney Canada Corp. Distributed propulsion configurations for aircraft having mixed drive systems
US11732639B2 (en) 2019-03-01 2023-08-22 Pratt & Whitney Canada Corp. Mechanical disconnects for parallel power lanes in hybrid electric propulsion systems
US11628942B2 (en) 2019-03-01 2023-04-18 Pratt & Whitney Canada Corp. Torque ripple control for an aircraft power train
WO2020190344A2 (fr) 2019-03-18 2020-09-24 United Technologies Advanced Projects Inc. Architectures pour propulsion hybride électrique
US20210122487A1 (en) * 2019-10-24 2021-04-29 Pratt & Whitney Canada Corp. Aircraft power supply arrangements
US11486472B2 (en) 2020-04-16 2022-11-01 United Technologies Advanced Projects Inc. Gear sytems with variable speed drive
GB202203103D0 (en) * 2022-03-07 2022-04-20 Rolls Royce Plc Blower system
US20240026827A1 (en) * 2022-07-22 2024-01-25 Raytheon Technologies Corporation Aircraft system with gas turbine engine powered compressor

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB602411A (en) * 1944-07-18 1948-05-26 Bendix Aviat Corp Improvements in or relating to supercharger control systems
US4523517A (en) * 1980-09-02 1985-06-18 Lockhead Corporation All electric environmental control system for advanced transport aircraft
US5125806A (en) * 1990-06-18 1992-06-30 Sundstrand Corporation Integrated variable speed compressor drive system
DE10306418A1 (de) * 2003-02-15 2004-08-26 Deere & Company, Moline Antriebsanordnung für ein Förderaggregat
FR2863312B1 (fr) * 2003-12-09 2008-07-04 Snecma Moteurs Turboreacteur a double corps avec moyen d'entrainement des machines accessoires
FR2934321B1 (fr) * 2008-07-25 2013-09-27 Hispano Suiza Sa Regulation du debit de carburant preleve dans un circuit carburant d'un aeronef propulse par un moteur.
US20130040545A1 (en) * 2011-08-11 2013-02-14 Hamilton Sundstrand Corporation Low pressure compressor bleed exit for an aircraft pressurization system
US9163562B2 (en) * 2012-03-14 2015-10-20 United Technologies Corporation Constant speed pump system for engine ECS loss elimination
FR3017159B1 (fr) 2014-01-31 2016-03-04 Snecma Alimentation en air d'un circuit de conditionnement d'air d'une cabine d'un aeronef a partir de son turbopropulseur
US9810158B2 (en) * 2014-04-01 2017-11-07 The Boeing Company Bleed air systems for use with aircraft and related methods
GB201508545D0 (en) * 2015-05-19 2015-07-01 Rolls Royce Plc Compressor tip injector

Also Published As

Publication number Publication date
GB2549597B (en) 2021-03-24
US20170284408A1 (en) 2017-10-05
GB2549597A (en) 2017-10-25
FR3048675A1 (fr) 2017-09-15
US10662960B2 (en) 2020-05-26
GB201703906D0 (en) 2017-04-26

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