GB201405895D0 - Aircraft vapour trail control system - Google Patents

Aircraft vapour trail control system

Info

Publication number
GB201405895D0
GB201405895D0 GBGB1405895.2A GB201405895A GB201405895D0 GB 201405895 D0 GB201405895 D0 GB 201405895D0 GB 201405895 A GB201405895 A GB 201405895A GB 201405895 D0 GB201405895 D0 GB 201405895D0
Authority
GB
United Kingdom
Prior art keywords
control system
trail control
vapour trail
aircraft
aircraft vapour
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Withdrawn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
GBGB1405895.2A
Other versions
GB2524774A (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 GB1405895.2A priority Critical patent/GB2524774A/en
Publication of GB201405895D0 publication Critical patent/GB201405895D0/en
Publication of GB2524774A publication Critical patent/GB2524774A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/46—Nozzles having means for adding air to the jet or for augmenting the mixing region between the jet and the ambient air, e.g. for silencing
    • F02K1/50—Deflecting outwardly a portion of the jet by retractable scoop-like baffles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C15/00—Attitude, flight direction, or altitude control by jet reaction
    • B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
    • B64C15/12—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets the power plant being tiltable
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • F02K1/008—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector in any rearward direction
    • 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)
  • Exhaust Silencers (AREA)
GB1405895.2A 2014-04-02 2014-04-02 Aircraft vapour trail control system Withdrawn GB2524774A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1405895.2A GB2524774A (en) 2014-04-02 2014-04-02 Aircraft vapour trail control system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1405895.2A GB2524774A (en) 2014-04-02 2014-04-02 Aircraft vapour trail control system

Publications (2)

Publication Number Publication Date
GB201405895D0 true GB201405895D0 (en) 2014-05-14
GB2524774A GB2524774A (en) 2015-10-07

Family

ID=50737851

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1405895.2A Withdrawn GB2524774A (en) 2014-04-02 2014-04-02 Aircraft vapour trail control system

Country Status (1)

Country Link
GB (1) GB2524774A (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201506473D0 (en) 2015-04-16 2015-06-03 Rolls Royce Plc Aircraft propulsion system
US11970279B2 (en) * 2020-02-21 2024-04-30 General Electric Company Control system and methods of controlling an engine-mounting link system
DE102021109848A1 (en) 2021-04-19 2022-10-20 MTU Aero Engines AG METHOD OF OPERATING AN AIRCRAFT PROPULSION SYSTEM

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0820174D0 (en) * 2008-11-05 2008-12-10 Rolls Royce Plc A gas turbine engine variable area exhaust nozzle
US8869508B2 (en) * 2012-01-31 2014-10-28 United Technologies Corporation Gas turbine engine variable area fan nozzle control
EP3546734B1 (en) * 2012-01-31 2022-09-14 Raytheon Technologies Corporation Gasturbine with a variable area fan nozzle fan flutter management system

Also Published As

Publication number Publication date
GB2524774A (en) 2015-10-07

Similar Documents

Publication Publication Date Title
IL279836B (en) Aircraft system
GB201505490D0 (en) Aircraft vapour trail control system
GB201510906D0 (en) Aircraft vapour trail control system
GB2524772B (en) Aircraft vapour trail control system
GB201614339D0 (en) Icing control system
GB201612684D0 (en) Vapour provision system
GB2524776B (en) Aircraft vapour trail control system
GB2524775B (en) Aircraft vapour trail control system
GB201615294D0 (en) Airplane status system
GB2533027B (en) Control system
GB201411975D0 (en) Aircraft control method
GB201507222D0 (en) Aircraft steering system
GB201410330D0 (en) Control system
EP3133283A4 (en) Vapor jet system
GB201506508D0 (en) Path control system
GB201412311D0 (en) Aircraft fuel system
GB201412325D0 (en) Aircraft fuel system
GB2549885B (en) Landing system
GB201405895D0 (en) Aircraft vapour trail control system
IL243033A0 (en) Rudder system
GB201405893D0 (en) Engine vapour trail mitigation system
GB2545965B (en) Aircraft environmental control system
GB201813121D0 (en) Icing control system
GB201521363D0 (en) Remote piloted aircraft system
GB201519380D0 (en) Remote piloted aircraft system

Legal Events

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