GB9218203D0 - Aircraft engine nacelle having circular arc profile - Google Patents

Aircraft engine nacelle having circular arc profile

Info

Publication number
GB9218203D0
GB9218203D0 GB929218203A GB9218203A GB9218203D0 GB 9218203 D0 GB9218203 D0 GB 9218203D0 GB 929218203 A GB929218203 A GB 929218203A GB 9218203 A GB9218203 A GB 9218203A GB 9218203 D0 GB9218203 D0 GB 9218203D0
Authority
GB
United Kingdom
Prior art keywords
circular arc
aircraft engine
engine nacelle
arc profile
profile
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Withdrawn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
GB929218203A
Other versions
GB2259114A (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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of GB9218203D0 publication Critical patent/GB9218203D0/en
Publication of GB2259114A publication Critical patent/GB2259114A/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Withdrawn legal-status Critical Current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
    • 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
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • 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
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0266—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
    • B64D2033/0286—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for turbofan engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Wind Motors (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB9218203A 1991-08-28 1992-08-27 Aircraft engine nacelle profile Withdrawn GB2259114A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US75101391A 1991-08-28 1991-08-28

Publications (2)

Publication Number Publication Date
GB9218203D0 true GB9218203D0 (en) 1992-10-14
GB2259114A GB2259114A (en) 1993-03-03

Family

ID=25020101

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9218203A Withdrawn GB2259114A (en) 1991-08-28 1992-08-27 Aircraft engine nacelle profile

Country Status (2)

Country Link
FR (1) FR2680831A1 (en)
GB (1) GB2259114A (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0401189D0 (en) 2004-01-21 2004-02-25 Rolls Royce Plc Turbine engine arrangements
DE602005005157T2 (en) * 2005-02-11 2009-03-19 Rolls-Royce Plc Engine assembly
RU2490169C2 (en) * 2011-11-10 2013-08-20 Николай Евгеньевич Староверов Staroverov's aircraft (versions)
US11480104B2 (en) 2013-03-04 2022-10-25 Raytheon Technologies Corporation Gas turbine engine inlet
GB201716284D0 (en) * 2017-10-05 2017-11-22 Rolls Royce Plc A gas turbine engine and air intake assembly
GB201809822D0 (en) 2018-06-15 2018-08-01 Rolls Royce Plc Gas turbine engine
GB201809823D0 (en) * 2018-06-15 2018-08-01 Rolls Royce Plc Gas turbine engine

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2611555A (en) * 1950-01-31 1952-09-23 Willard R Custer Jet-propelled aircraft with fuselage lifting channels
GB820366A (en) * 1956-01-06 1959-09-16 Rolls Royce Improvements in or relating to retractable guards for air intakes
GB877838A (en) * 1959-08-20 1961-09-20 Rolls Royce Improvements relating to gas turbine engine air intakes
GB950909A (en) * 1962-05-11 1964-02-26 Rolls Royce Improvements relating to the mounting of gas turbine engines
US4194519A (en) * 1964-11-18 1980-03-25 The United States Of America As Represented By The Secretary Of The Navy Hypersonic modular inlet
US3765623A (en) * 1971-10-04 1973-10-16 Mc Donnell Douglas Corp Air inlet
US3905566A (en) * 1972-08-29 1975-09-16 Edwin R Anderson Jet engine intake protection system
US3946830A (en) * 1974-09-06 1976-03-30 General Electric Company Inlet noise deflector
US4012013A (en) * 1976-02-05 1977-03-15 The Boeing Company Variable camber inlet for supersonic aircraft
GB2064005A (en) * 1979-11-22 1981-06-10 Rolls Royce Air Intake to Ducted Fan Engine
IL62132A0 (en) * 1980-02-26 1981-03-31 Gen Electric Inlet cowl for a two-dimensional inlet
GB2074654A (en) * 1980-04-16 1981-11-04 Rolls Royce Remote power system for aircraft
US5082206A (en) * 1988-07-25 1992-01-21 General Electric Company Hypersonic flight vehicle
US5058617A (en) * 1990-07-23 1991-10-22 General Electric Company Nacelle inlet for an aircraft gas turbine engine

Also Published As

Publication number Publication date
GB2259114A (en) 1993-03-03
FR2680831A1 (en) 1993-03-05

Similar Documents

Publication Publication Date Title
GB9218229D0 (en) Aircraft engine nacelle having circular arc profile
EP0516468A3 (en) Jet engine fan nacelle
GB2260371B (en) Turbine engines
GB9122965D0 (en) Turbine engine control system
AU1508692A (en) Turbine
GB2250060B (en) Engine nacelle
GB2266931B (en) Turbine blade assembly
GB2273318B (en) Aircraft engine arrangement
AU121271S (en) Aircraft
EP0510585A3 (en) Gas engine
GB9218203D0 (en) Aircraft engine nacelle having circular arc profile
GB9315389D0 (en) Operating aircraft
GB9115625D0 (en) Aircraft engines
GB9218544D0 (en) Turbines
GB9127198D0 (en) Engine components
GB9101719D0 (en) Gas turbines
GB2270543B (en) Turbines
PL289858A1 (en) Turbine engine
GB9103594D0 (en) Engine structure
GB9101937D0 (en) Aircraft
AU116067S (en) Aircraft
GB9121211D0 (en) Aircraft
GB9212083D0 (en) An aircraft
GB9016828D0 (en) Screw nosed turbine aircraft engine
AU2282092A (en) Wind engine

Legal Events

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