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 languages
English (en)
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/xx
Publication of IL69906A publication Critical patent/IL69906A/xx

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
    • B64D29/00Power-plant nacelles, fairings, or cowlings
    • 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
    • B64D2033/0226Arrangements 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 (xx)
AU (1) AU555526B2 (xx)
CA (1) CA1209354A (xx)
CH (1) CH667434A5 (xx)
DE (1) DE3338286A1 (xx)
GB (1) GB2128945B (xx)
IL (1) IL69906A (xx)
IT (1) IT1171783B (xx)
NL (1) NL8303716A (xx)
SE (1) SE456077B (xx)
SU (1) SU1391490A3 (xx)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2920143B1 (fr) * 2007-08-20 2010-01-22 Aircelle Sa Dispositif de commande des actionneurs de maintenance de capots d'une nacelle de turboreacteur
DE102009003084B4 (de) 2009-05-13 2013-03-14 Airbus Operations Gmbh Verkleidung für eine Auftriebshilfe
GB2595724B (en) 2020-06-05 2022-10-05 Rolls Royce Plc Nacelle for gas turbine engine and aircraft comprising the same
FR3116043B1 (fr) * 2020-11-09 2023-04-28 Safran Aircraft Engines Entrée d’air de nacelle d’ensemble propulsif d’aéronef pour favoriser une phase d’inversion de poussée

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 (de) * 1977-03-23 1978-09-28 Ver Flugtechnische Werke Ueberkritisches tragfluegelprofil
US4209149A (en) * 1977-12-27 1980-06-24 Boeing Commercial Airplane Company Contracted inlet for jet engine being transported as cargo
FR2427249A1 (fr) * 1978-05-29 1979-12-28 Aerospatiale Profil de voilure pour aeronef
CA1185101A (en) * 1980-03-03 1985-04-09 Daniel J. Lahti Drag-reducing nacelle
DE3033101C2 (de) * 1980-09-03 1984-11-22 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Anordnung zur Erhöhung der resultierenden Vortriebskraft bei Flugzeugen

Also Published As

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

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