GB201120637D0 - Motor assisted fine pitch startup ram air turbine - Google Patents

Motor assisted fine pitch startup ram air turbine

Info

Publication number
GB201120637D0
GB201120637D0 GBGB1120637.2A GB201120637A GB201120637D0 GB 201120637 D0 GB201120637 D0 GB 201120637D0 GB 201120637 A GB201120637 A GB 201120637A GB 201120637 D0 GB201120637 D0 GB 201120637D0
Authority
GB
United Kingdom
Prior art keywords
generator
rat
fine pitch
air turbine
ram air
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.)
Granted
Application number
GBGB1120637.2A
Other versions
GB2497102A (en
GB2497102B (en
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.)
Hamilton Sundstrand Corp
Original Assignee
Hamilton Sundstrand Corp
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 Hamilton Sundstrand Corp filed Critical Hamilton Sundstrand Corp
Priority to GB1120637.2A priority Critical patent/GB2497102B/en
Publication of GB201120637D0 publication Critical patent/GB201120637D0/en
Publication of GB2497102A publication Critical patent/GB2497102A/en
Application granted granted Critical
Publication of GB2497102B publication Critical patent/GB2497102B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J4/00Circuit arrangements for mains or distribution networks not specified as AC or DC
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/32Arrangement, mounting, or driving, of auxiliaries
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D2221/00Electric power distribution systems onboard aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D41/00Power installations for auxiliary purposes
    • B64D41/007Ram air turbines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/34Application in turbines in ram-air turbines ("RATS")
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J2310/00The network for supplying or distributing electric power characterised by its spatial reach or by the load
    • H02J2310/40The network being an on-board power network, i.e. within a vehicle
    • H02J2310/44The network being an on-board power network, i.e. within a vehicle for aircrafts

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Power Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Eletrric Generators (AREA)

Abstract

A startup assistance apparatus for a fine pitch Ram Air Turbine (RAT) is provided and includes a generator 20 to provide motive power to the RAT when operating in a first mode and to generate electricity from RAT operation when operating in a second mode and a control unit 30, including a sensing unit configured to sense an operating condition of the generator 20 and a controller 50 operably coupled to the generator 20 and configured to control the generator 20 to operate in the first or the second mode based on the sensed operating condition. The sensed operating condition may be a generator frequency. The RAT may be a fine pitch RAT of an aircraft wherein the generator 20 provides electricity to aircraft loads in the second mode.
GB1120637.2A 2011-11-30 2011-11-30 Motor assisted fine pitch startup ram air turbine Active GB2497102B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1120637.2A GB2497102B (en) 2011-11-30 2011-11-30 Motor assisted fine pitch startup ram air turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1120637.2A GB2497102B (en) 2011-11-30 2011-11-30 Motor assisted fine pitch startup ram air turbine

Publications (3)

Publication Number Publication Date
GB201120637D0 true GB201120637D0 (en) 2012-01-11
GB2497102A GB2497102A (en) 2013-06-05
GB2497102B GB2497102B (en) 2014-04-16

Family

ID=45508971

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1120637.2A Active GB2497102B (en) 2011-11-30 2011-11-30 Motor assisted fine pitch startup ram air turbine

Country Status (1)

Country Link
GB (1) GB2497102B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112478184A (en) * 2020-12-01 2021-03-12 陕西航空电气有限责任公司 RAT release control architecture of turboprop branch aircraft

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10322815B1 (en) * 2018-03-22 2019-06-18 Hamilton Sundstrand Corporation Stored electrical energy assisted ram air turbine (RAT) system
US12104843B2 (en) * 2020-11-05 2024-10-01 Carrier Corporation Transport refrigeration system energy management system and method

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8424800B2 (en) * 2010-06-23 2013-04-23 Hamilton Sundstrand Corporation Multi-source emergency power optimization

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112478184A (en) * 2020-12-01 2021-03-12 陕西航空电气有限责任公司 RAT release control architecture of turboprop branch aircraft
CN112478184B (en) * 2020-12-01 2024-03-19 陕西航空电气有限责任公司 Vortex oar branch line aircraft RAT release control architecture

Also Published As

Publication number Publication date
GB2497102A (en) 2013-06-05
GB2497102B (en) 2014-04-16

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