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GB201516106D0 - Aircraft comprising a boundary layer ingesting propulsor - Google Patents

Aircraft comprising a boundary layer ingesting propulsor

Info

Publication number
GB201516106D0
GB201516106D0 GBGB1516106.0A GB201516106A GB201516106D0 GB 201516106 D0 GB201516106 D0 GB 201516106D0 GB 201516106 A GB201516106 A GB 201516106A GB 201516106 D0 GB201516106 D0 GB 201516106D0
Authority
GB
United Kingdom
Prior art keywords
propulsor
aircraft
boundary layer
ingesting
layer ingesting
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Withdrawn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
GBGB1516106.0A
Other versions
GB2542184A (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 GB1516106.0A priority Critical patent/GB2542184A/en
Publication of GB201516106D0 publication Critical patent/GB201516106D0/en
Publication of GB2542184A publication Critical patent/GB2542184A/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Withdrawn legal-status Critical Current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
    • B64C1/16—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like specially adapted for mounting power plant
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/01—Boundary layer ingestion [BLI] propulsion
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • B64D27/14—Aircraft characterised by the type or position of power plants of gas-turbine type  within, or attached to, fuselages
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D2027/005—Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR]
    • 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
    • Y02T50/10—Drag reduction
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Wind Motors (AREA)
GB1516106.0A 2015-09-11 2015-09-11 Aircraft comprising a boundary layer ingesting propulsor Withdrawn GB2542184A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1516106.0A GB2542184A (en) 2015-09-11 2015-09-11 Aircraft comprising a boundary layer ingesting propulsor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1516106.0A GB2542184A (en) 2015-09-11 2015-09-11 Aircraft comprising a boundary layer ingesting propulsor

Publications (2)

Publication Number Publication Date
GB201516106D0 true GB201516106D0 (en) 2015-10-28
GB2542184A GB2542184A (en) 2017-03-15

Family

ID=54363018

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1516106.0A Withdrawn GB2542184A (en) 2015-09-11 2015-09-11 Aircraft comprising a boundary layer ingesting propulsor

Country Status (1)

Country Link
GB (1) GB2542184A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108263620A (en) * 2018-03-14 2018-07-10 中国空气动力研究与发展中心高速空气动力研究所 A kind of aircraft electric drive is to rotary fan propeller
CN110395397A (en) * 2018-04-25 2019-11-01 波音公司 The pitching of compound aircraft and thrust control
CN115723945A (en) * 2016-09-26 2023-03-03 通用电气公司 Aircraft with rear engine and air injection assembly for the aircraft

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201702822D0 (en) * 2017-02-22 2017-04-05 Rolls Royce Plc A propulsor
GB201704268D0 (en) * 2017-03-17 2017-05-03 Rolls Royce Plc An electrical machine
US10723470B2 (en) 2017-06-12 2020-07-28 Raytheon Technologies Corporation Aft fan counter-rotating turbine engine
US12270301B2 (en) 2017-08-10 2025-04-08 Paul NEISER System and method for fluid manipulation
JP6974616B2 (en) 2017-08-10 2021-12-01 ネイサー、ポール Fluid control device assembly, fluid control device, and aircraft
WO2021113055A2 (en) * 2019-11-12 2021-06-10 Neiser Paul Apparatus and method for fluid manipulation
FR3074476B1 (en) * 2017-12-06 2020-12-25 Safran Aircraft Engines AIRCRAFT TURBOPROPELLER CONTAINING A NON-FAIRED PROPELLER
US11098678B2 (en) 2018-04-05 2021-08-24 Raytheon Technologies Corporation Aft counter-rotating boundary layer ingestion engine
US10906657B2 (en) 2018-06-19 2021-02-02 Raytheon Technologies Corporation Aircraft system with distributed propulsion
US10759545B2 (en) 2018-06-19 2020-09-01 Raytheon Technologies Corporation Hybrid electric aircraft system with distributed propulsion
FR3082828B1 (en) * 2018-06-21 2021-09-10 Safran REAR PROPULSION SYSTEM FOR AIRCRAFT
FR3082827B1 (en) 2018-06-21 2021-09-10 Safran REAR PROPULSION SYSTEM FOR AIRCRAFT
US10738694B1 (en) * 2018-08-23 2020-08-11 United Technologies Corporation Turbofan with motorized rotating inlet guide vane
CN112912308A (en) * 2018-10-22 2021-06-04 保罗·奈瑟 System and method for fluid manipulation
GB201818683D0 (en) 2018-11-16 2019-01-02 Rolls Royce Plc Boundary layer ingestion fan system
GB201818686D0 (en) 2018-11-16 2019-01-02 Rolls Royce Plc Boundary layer ingestion fan system
GB201818682D0 (en) 2018-11-16 2019-01-02 Rolls Royce Plc Boundary layer ingestion fan system
GB201818680D0 (en) 2018-11-16 2019-01-02 Rolls Royce Plc Boundary layer ingestion fan system
GB201818684D0 (en) 2018-11-16 2019-01-02 Rolls Royce Plc Boundary layer ingestion fan system
GB201818687D0 (en) 2018-11-16 2019-01-02 Rolls Royce Plc Boundary layer ingestion fan system
GB201818681D0 (en) 2018-11-16 2019-01-02 Rolls Royce Plc Boundary layer ingestion fan system
EP3798119B1 (en) * 2019-09-30 2023-02-22 Ratier-Figeac SAS Drive system for counter-rotating parts

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB873851A (en) * 1957-08-07 1961-07-26 Pierre Mercier Apparatus for improving the performance of stream-lined bodies propelled in a fluid
ES2035837T3 (en) * 1986-08-18 1993-05-01 Siemens Aktiengesellschaft FILLING LAYER COMPONENT.
DE102008062813A1 (en) * 2008-12-23 2010-07-15 Rolls-Royce Deutschland Ltd & Co Kg Airplane with a stern-propeller engine arrangement

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115723945A (en) * 2016-09-26 2023-03-03 通用电气公司 Aircraft with rear engine and air injection assembly for the aircraft
CN108263620A (en) * 2018-03-14 2018-07-10 中国空气动力研究与发展中心高速空气动力研究所 A kind of aircraft electric drive is to rotary fan propeller
CN110395397A (en) * 2018-04-25 2019-11-01 波音公司 The pitching of compound aircraft and thrust control

Also Published As

Publication number Publication date
GB2542184A (en) 2017-03-15

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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)