GB0812568D0 - Aircraft propulsion arrangement - Google Patents

Aircraft propulsion arrangement

Info

Publication number
GB0812568D0
GB0812568D0 GBGB0812568.4A GB0812568A GB0812568D0 GB 0812568 D0 GB0812568 D0 GB 0812568D0 GB 0812568 A GB0812568 A GB 0812568A GB 0812568 D0 GB0812568 D0 GB 0812568D0
Authority
GB
United Kingdom
Prior art keywords
aircraft propulsion
propulsion arrangement
arrangement
aircraft
propulsion
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Withdrawn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
GBGB0812568.4A
Other versions
GB2461718A (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 GB0812568A priority Critical patent/GB2461718A/en
Publication of GB0812568D0 publication Critical patent/GB0812568D0/en
Publication of GB2461718A publication Critical patent/GB2461718A/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Withdrawn legal-status Critical Current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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • 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
    • F05D2250/00—Geometry
    • F05D2250/10—Two-dimensional
    • F05D2250/12—Two-dimensional rectangular
    • 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
    • F05D2250/00—Geometry
    • F05D2250/70—Shape
    • F05D2250/71—Shape curved

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)
GB0812568A 2008-07-10 2008-07-10 An aircraft propulsion arrangement having a single fan located within a curved guide path Withdrawn GB2461718A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB0812568A GB2461718A (en) 2008-07-10 2008-07-10 An aircraft propulsion arrangement having a single fan located within a curved guide path

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0812568A GB2461718A (en) 2008-07-10 2008-07-10 An aircraft propulsion arrangement having a single fan located within a curved guide path

Publications (2)

Publication Number Publication Date
GB0812568D0 true GB0812568D0 (en) 2008-08-13
GB2461718A GB2461718A (en) 2010-01-13

Family

ID=39718222

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0812568A Withdrawn GB2461718A (en) 2008-07-10 2008-07-10 An aircraft propulsion arrangement having a single fan located within a curved guide path

Country Status (1)

Country Link
GB (1) GB2461718A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20210061248A1 (en) * 2019-08-19 2021-03-04 Mark T. Holtzapple Enhanced-Thrust Lift and Propulsion Systems

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3809178A (en) * 1973-04-30 1974-05-07 Boeing Co Clamshell exhaust nozzle and sound deflector
US6575406B2 (en) * 2001-01-19 2003-06-10 The Boeing Company Integrated and/or modular high-speed aircraft
GB2372019A (en) * 2001-02-10 2002-08-14 Rolls Royce Plc Turbofan engine negatively scarfed nacelle for uniform flow to the fan
US6527224B2 (en) * 2001-03-23 2003-03-04 The Boeing Company Separate boundary layer engine inlet
GB0401189D0 (en) * 2004-01-21 2004-02-25 Rolls Royce Plc Turbine engine arrangements

Also Published As

Publication number Publication date
GB2461718A (en) 2010-01-13

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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)