IL69906A - Laminar flow engine nacelle for an aircraft - Google Patents

Laminar flow engine nacelle for an aircraft

Info

Publication number
IL69906A
IL69906A IL69906A IL6990683A IL69906A IL 69906 A IL69906 A IL 69906A IL 69906 A IL69906 A IL 69906A IL 6990683 A IL6990683 A IL 6990683A IL 69906 A IL69906 A IL 69906A
Authority
IL
Israel
Prior art keywords
aircraft
laminar flow
engine nacelle
flow engine
nacelle
Prior art date
Application number
IL69906A
Other versions
IL69906A0 (en
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IL69906A0 publication Critical patent/IL69906A0/en
Publication of IL69906A publication Critical patent/IL69906A/en

Links

Classifications

    • 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
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • 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
    • B64D2033/0226—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising boundary layer control means

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)
  • Structure Of Belt Conveyors (AREA)
IL69906A 1982-10-29 1983-10-04 Laminar flow engine nacelle for an aircraft IL69906A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US43758182A 1982-10-29 1982-10-29

Publications (2)

Publication Number Publication Date
IL69906A0 IL69906A0 (en) 1984-01-31
IL69906A true IL69906A (en) 1990-04-29

Family

ID=23737028

Family Applications (1)

Application Number Title Priority Date Filing Date
IL69906A IL69906A (en) 1982-10-29 1983-10-04 Laminar flow engine nacelle for an aircraft

Country Status (11)

Country Link
JP (1) JPS5996462A (en)
AU (1) AU555526B2 (en)
CA (1) CA1209354A (en)
CH (1) CH667434A5 (en)
DE (1) DE3338286A1 (en)
GB (1) GB2128945B (en)
IL (1) IL69906A (en)
IT (1) IT1171783B (en)
NL (1) NL8303716A (en)
SE (1) SE456077B (en)
SU (1) SU1391490A3 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2920143B1 (en) * 2007-08-20 2010-01-22 Aircelle Sa DEVICE FOR CONTROLLING HOUSING MAINTENANCE ACTUATORS OF A TURBOREACTOR NACELLE
DE102009003084B4 (en) 2009-05-13 2013-03-14 Airbus Operations Gmbh Cladding for a buoyancy aid
GB2595724B (en) * 2020-06-05 2022-10-05 Rolls Royce Plc Nacelle for gas turbine engine and aircraft comprising the same
FR3116043B1 (en) * 2020-11-09 2023-04-28 Safran Aircraft Engines Aircraft propulsion unit nacelle air inlet to promote a thrust reversal phase

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1211192A (en) * 1964-07-01 1970-11-04 Gen Electric Improvements in low drag exhaust nozzle and nacelle arrangement for turbofan engines
US3765623A (en) * 1971-10-04 1973-10-16 Mc Donnell Douglas Corp Air inlet
US3952971A (en) * 1971-11-09 1976-04-27 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Airfoil shape for flight at subsonic speeds
IL42041A (en) * 1972-05-04 1977-05-31 Mc Donnell Douglas Corp Low drag airfoils and method of designing same
GB1554713A (en) * 1975-03-04 1979-10-24 Secr Defence Wings
GB1553816A (en) * 1975-06-12 1979-10-10 Secr Defence Wings
DE2712717A1 (en) * 1977-03-23 1978-09-28 Ver Flugtechnische Werke ABOVE CRITICAL WING PROFILE
US4209149A (en) * 1977-12-27 1980-06-24 Boeing Commercial Airplane Company Contracted inlet for jet engine being transported as cargo
FR2427249A1 (en) * 1978-05-29 1979-12-28 Aerospatiale SAIL PROFILE FOR AIRCRAFT
CA1185101A (en) * 1980-03-03 1985-04-09 Daniel J. Lahti Drag-reducing nacelle
DE3033101C2 (en) * 1980-09-03 1984-11-22 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Arrangement for increasing the resulting propulsive force in aircraft

Also Published As

Publication number Publication date
SE456077B (en) 1988-09-05
GB8328400D0 (en) 1983-11-23
GB2128945A (en) 1984-05-10
GB2128945B (en) 1986-03-26
SU1391490A3 (en) 1988-04-23
SE8305904L (en) 1984-04-30
NL8303716A (en) 1984-05-16
IT8323478A0 (en) 1983-10-27
IL69906A0 (en) 1984-01-31
DE3338286A1 (en) 1984-05-03
IT1171783B (en) 1987-06-10
CH667434A5 (en) 1988-10-14
AU1902683A (en) 1984-05-03
JPH0344221B2 (en) 1991-07-05
CA1209354A (en) 1986-08-12
JPS5996462A (en) 1984-06-02
SE8305904D0 (en) 1983-10-27
AU555526B2 (en) 1986-09-25

Similar Documents

Publication Publication Date Title
GB2114263B (en) Turbomachine flow duct
GB2168303B (en) Altitude verification system for aircraft
DE3376063D1 (en) Aircraft seat
JPS56149294A (en) Fixed airfoil aircraft
GB2126313B (en) Shroud for aircraft duct
JPS5760999A (en) Propelling device for aircraft
GB2126382B (en) Gas turbine engine control system
IL63566A0 (en) Management system for an aircraft engine
GB2112582B (en) Ion-generator for producing an air flow
JPS57330A (en) Aircraft gasturbine engine
DE3374794D1 (en) Ram air turbine with variable flow passage
GB8312111D0 (en) Prediffuser for gas turbine engine
GB2070139B (en) Inlet cowl for supersonic aircraft engine
DE3378138D1 (en) Air flow meter for internal-combustion engine
GB2138499B (en) I c engine propulsion arrangement for an aircraft
JPS56135721A (en) Turbine engine system
GB2123486B (en) Turbofan mixed flow exhaust system
DE3371893D1 (en) Duct means for aircraft
GB2129382B (en) Aircraft refuelling
GB2083420B (en) Disposition of engine on aircraft
IL69906A (en) Laminar flow engine nacelle for an aircraft
GB8329988D0 (en) Engine systems
IL72619A0 (en) Multiflow turbo jet engine secondary flow adjusting device
GB2238278B (en) Gas turbine engine for aircraft propulsion
GB2105800B (en) Transmission-responsive engine governor