GB8605896D0 - Ducted fan & gas turbine engines - Google Patents

Ducted fan & gas turbine engines

Info

Publication number
GB8605896D0
GB8605896D0 GB868605896A GB8605896A GB8605896D0 GB 8605896 D0 GB8605896 D0 GB 8605896D0 GB 868605896 A GB868605896 A GB 868605896A GB 8605896 A GB8605896 A GB 8605896A GB 8605896 D0 GB8605896 D0 GB 8605896D0
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engines
ducted fan
ducted
fan
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Withdrawn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
GB868605896A
Other versions
GB2187796A (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 GB08605896A priority Critical patent/GB2187796A/en
Publication of GB8605896D0 publication Critical patent/GB8605896D0/en
Publication of GB2187796A publication Critical patent/GB2187796A/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Withdrawn legal-status Critical Current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
    • 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
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB08605896A 1986-03-11 1986-03-11 Ducted fan and ducted propeller gas turbine engines Withdrawn GB2187796A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08605896A GB2187796A (en) 1986-03-11 1986-03-11 Ducted fan and ducted propeller gas turbine engines

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US83846086A 1986-03-11 1986-03-11
GB08605896A GB2187796A (en) 1986-03-11 1986-03-11 Ducted fan and ducted propeller gas turbine engines

Publications (2)

Publication Number Publication Date
GB8605896D0 true GB8605896D0 (en) 1986-04-16
GB2187796A GB2187796A (en) 1987-09-16

Family

ID=68771311

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08605896A Withdrawn GB2187796A (en) 1986-03-11 1986-03-11 Ducted fan and ducted propeller gas turbine engines

Country Status (1)

Country Link
GB (1) GB2187796A (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2329555A1 (en) * 2000-12-22 2002-06-22 Jose Albero Main propulsion engine system integrated with secondary power unit
US8127529B2 (en) * 2007-03-29 2012-03-06 United Technologies Corporation Variable area fan nozzle and thrust reverser
US9091214B2 (en) * 2007-06-28 2015-07-28 United Technologies Corporation Reduced gearbox size by separate electrically powered engine oil system
DE102009033755A1 (en) * 2009-07-17 2011-01-20 Rolls-Royce Deutschland Ltd & Co Kg Turbofan
GB201811219D0 (en) 2018-07-09 2018-08-29 Rolls Royce Plc Apparatus for gas turbine engines

Also Published As

Publication number Publication date
GB2187796A (en) 1987-09-16

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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)