GB2522080B - Reduced weight aircraft engine intake pre-cooler - Google Patents

Reduced weight aircraft engine intake pre-cooler

Info

Publication number
GB2522080B
GB2522080B GB1402417.8A GB201402417A GB2522080B GB 2522080 B GB2522080 B GB 2522080B GB 201402417 A GB201402417 A GB 201402417A GB 2522080 B GB2522080 B GB 2522080B
Authority
GB
United Kingdom
Prior art keywords
cooler
aircraft engine
engine intake
reduced weight
intake pre
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.)
Active
Application number
GB1402417.8A
Other versions
GB201402417D0 (en
GB2522080A (en
Inventor
Desmond Lewis Stephen
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB201402417D0 publication Critical patent/GB201402417D0/en
Publication of GB2522080A publication Critical patent/GB2522080A/en
Application granted granted Critical
Publication of GB2522080B publication Critical patent/GB2522080B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00Arrangements in connection with fuel supply for power plant
    • B64D37/02Tanks
    • B64D37/04Arrangement thereof in or on aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/024Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising cooling means
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T90/00Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02T90/40Application of hydrogen technology to transportation, e.g. using fuel cells

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
GB1402417.8A 2014-01-11 2014-02-12 Reduced weight aircraft engine intake pre-cooler Active GB2522080B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB1400497.2A GB201400497D0 (en) 2014-01-11 2014-01-11 Low weight aircraft engine intake pre-cooler

Publications (3)

Publication Number Publication Date
GB201402417D0 GB201402417D0 (en) 2014-03-26
GB2522080A GB2522080A (en) 2015-07-15
GB2522080B true GB2522080B (en) 2017-06-28

Family

ID=50191214

Family Applications (2)

Application Number Title Priority Date Filing Date
GBGB1400497.2A Ceased GB201400497D0 (en) 2014-01-11 2014-01-11 Low weight aircraft engine intake pre-cooler
GB1402417.8A Active GB2522080B (en) 2014-01-11 2014-02-12 Reduced weight aircraft engine intake pre-cooler

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GBGB1400497.2A Ceased GB201400497D0 (en) 2014-01-11 2014-01-11 Low weight aircraft engine intake pre-cooler

Country Status (1)

Country Link
GB (2) GB201400497D0 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10793285B2 (en) 2018-02-13 2020-10-06 Bell Helicopter Textron Inc. Fuselage embedded fuel tank

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP4112478A1 (en) * 2021-06-28 2023-01-04 Airbus Operations GmbH Fuselage section of an aircraft, aircraft fuselage, and aircraft

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB849212A (en) * 1956-03-01 1960-09-21 Power Jets Res & Dev Ltd Supersonic aircraft
GB2238080A (en) * 1987-05-26 1991-05-22 Rolls Royce Plc Propulsion system for an aerospace vehicle
GB2274881A (en) * 1993-02-05 1994-08-10 Europ Propulsion Jet propulsion engine

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB849212A (en) * 1956-03-01 1960-09-21 Power Jets Res & Dev Ltd Supersonic aircraft
GB2238080A (en) * 1987-05-26 1991-05-22 Rolls Royce Plc Propulsion system for an aerospace vehicle
GB2274881A (en) * 1993-02-05 1994-08-10 Europ Propulsion Jet propulsion engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10793285B2 (en) 2018-02-13 2020-10-06 Bell Helicopter Textron Inc. Fuselage embedded fuel tank

Also Published As

Publication number Publication date
GB201402417D0 (en) 2014-03-26
GB201400497D0 (en) 2014-02-26
GB2522080A (en) 2015-07-15

Similar Documents

Publication Publication Date Title
EP3239499A4 (en) Aircraft engine device
GB201415078D0 (en) Gas turbine engine anti-icing system
EP3246546A4 (en) Aircraft engine device
GB201420989D0 (en) Aircraft engine fuel system
GB201511454D0 (en) Aircraft engine nacelle
PL3572638T3 (en) Turboprop engine
GB201315968D0 (en) Aircraft engine mount
PL3257753T3 (en) Reduction gearbox for aircraft engine
GB201307376D0 (en) An Aircraft Powerplant
EP3024729A4 (en) Aircraft engine pylon
EP3216994A4 (en) Uniflow-scavenged two-cycle engine
GB2528562B (en) Aircraft turboprop engine comprising two coaxial propellers
GB201413591D0 (en) Internal combustion engine
IL231653A0 (en) Aircraft pylon
PL3201437T3 (en) Internal combustion engine
PL3149309T3 (en) Combustion engine
GB201506838D0 (en) Aircraft fuel pump
ZA201705344B (en) Powered turboprop engine
GB201413345D0 (en) Internal combustion engine
PL3180506T3 (en) Exhaust arrangement for aircraft having sensor
GB201507729D0 (en) Aircraft fuel tank
GB201409075D0 (en) Efficient two-stroke engine
GB2522080B (en) Reduced weight aircraft engine intake pre-cooler
GB2529636B (en) Aero engine fuel system
TWM489676U (en) Quantity-changeable multi-rotor aircraft structure

Legal Events

Date Code Title Description
746 Register noted 'licences of right' (sect. 46/1977)

Effective date: 20170705