GB0113967D0 - A gas turbine engine breather outlet - Google Patents

A gas turbine engine breather outlet

Info

Publication number
GB0113967D0
GB0113967D0 GB0113967A GB0113967A GB0113967D0 GB 0113967 D0 GB0113967 D0 GB 0113967D0 GB 0113967 A GB0113967 A GB 0113967A GB 0113967 A GB0113967 A GB 0113967A GB 0113967 D0 GB0113967 D0 GB 0113967D0
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engine
breather outlet
engine breather
outlet
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.)
Withdrawn
Application number
GB0113967A
Other versions
GB2376269A (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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB0113967A priority Critical patent/GB2376269A/en
Publication of GB0113967D0 publication Critical patent/GB0113967D0/en
Publication of GB2376269A publication Critical patent/GB2376269A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • B64C1/1407—Doors; surrounding frames
    • B64C1/1453—Drain masts
    • 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
    • F02C7/06—Arrangements of bearings; Lubricating

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
GB0113967A 2001-06-08 2001-06-08 A gas turbine engine breather outlet Withdrawn GB2376269A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB0113967A GB2376269A (en) 2001-06-08 2001-06-08 A gas turbine engine breather outlet

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0113967A GB2376269A (en) 2001-06-08 2001-06-08 A gas turbine engine breather outlet

Publications (2)

Publication Number Publication Date
GB0113967D0 true GB0113967D0 (en) 2001-08-01
GB2376269A GB2376269A (en) 2002-12-11

Family

ID=9916178

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0113967A Withdrawn GB2376269A (en) 2001-06-08 2001-06-08 A gas turbine engine breather outlet

Country Status (1)

Country Link
GB (1) GB2376269A (en)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007026060A1 (en) * 2007-06-01 2008-12-04 Rolls-Royce Deutschland Ltd & Co Kg Ventilation for the lubricating oil system of a jet engine
US8621839B2 (en) * 2009-09-28 2014-01-07 Pratt & Whitney Canada Corp. Gas turbine engine breather exhaust oil collector
DE102009053002A1 (en) * 2009-11-16 2011-05-19 Rolls-Royce Deutschland Ltd & Co Kg Exhaust outlet for lubricating oil system of aircraft engine, is arranged at exterior surface of engine- or engine mount lining, where region of exterior surface is limited to edge of outlet
DE102009060051A1 (en) * 2009-12-21 2011-06-22 Rolls-Royce Deutschland Ltd & Co KG, 15827 Arrangement for blowing off from the lubricating oil ventilation system of a gas turbine engine from separate exhaust air
RU2456461C1 (en) * 2010-12-09 2012-07-20 Открытое акционерное общество "Научно-производственное объединение "Сатурн" (ОАО "НПО "Сатурн") Breathing system of turbine pedestal of double-flow jet turbine engine
DE102012208673A1 (en) * 2012-05-23 2013-11-28 Rolls-Royce Deutschland Ltd & Co Kg Device for discharging oil ventilation air from lubrication oil venting system of dual flow jet engine, has air outlet formed at suction side and at pressure side such that oil ventilation air is exhausted over air outlet into flow channel
RU2532393C1 (en) * 2013-09-10 2014-11-10 Открытое акционерное общество "Авиадвигатель" Breathing system of turbojet engine
DE102016108068A1 (en) * 2016-05-02 2017-11-02 Rolls-Royce Deutschland Ltd & Co Kg Turbofan engine and method for discharging bleed air of an oil separator in a turbofan engine
DE102016114394A1 (en) * 2016-08-03 2018-02-08 Rolls-Royce Deutschland Ltd & Co Kg Device of a turbomachine for separating oil from an air-oil volume flow
ES2732174T3 (en) * 2016-08-22 2019-11-21 Airbus Operations Sl Drainage mast of an aircraft
ES2832462T3 (en) * 2016-10-20 2021-06-10 Airbus Operations Sl Drainage mast of an aircraft
FR3073820B1 (en) * 2017-11-21 2020-09-11 Airbus Operations Sas AIRCRAFT CONTAINING A LIQUID ACCUMULATION ZONE AND A SYSTEM FOR EXHAUSTING THE LIQUID TO THE EXTERIOR
US11168585B2 (en) 2018-01-08 2021-11-09 Raytheon Technologies Corporation Geared gas turbine engine with improved breather air venting
FR3077850B1 (en) * 2018-02-13 2020-03-13 Safran Aircraft Engines OUTPUT DIRECTIVE VANE FOR TURBOMACHINE, MADE FROM SEVERAL PARTS ASSEMBLED BETWEEN THEM BY MEANS OF ATTACHMENT OF THE VEIN
US10717514B2 (en) * 2018-03-09 2020-07-21 Senior Ip Gmbh Integrated drain mast structure
GB201808855D0 (en) * 2018-05-31 2018-07-18 Rolls Royce Plc Oil recovery system

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3935704A (en) * 1974-09-12 1976-02-03 United Technologies Corporation Fan propulsor oil escapement means
GB9002028D0 (en) * 1990-01-30 1990-03-28 Rolls Royce Plc Gearbox breather outlet
GB9804807D0 (en) * 1998-03-06 1998-04-29 Rolls Royce Plc A breather outlet

Also Published As

Publication number Publication date
GB2376269A (en) 2002-12-11

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)