CH326061A - Antriebseinrichtung an einem Flugzeug - Google Patents

Antriebseinrichtung an einem Flugzeug

Info

Publication number
CH326061A
CH326061A CH326061DA CH326061A CH 326061 A CH326061 A CH 326061A CH 326061D A CH326061D A CH 326061DA CH 326061 A CH326061 A CH 326061A
Authority
CH
Switzerland
Prior art keywords
aircraft
propulsion device
propulsion
Prior art date
Application number
Other languages
English (en)
Inventor
Macaulay Davidson Ivor
Stapleton Stratford Brian
Original Assignee
Power Jets Res & Dev Ltd
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 Power Jets Res & Dev Ltd filed Critical Power Jets Res & Dev Ltd
Publication of CH326061A publication Critical patent/CH326061A/de

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/52—Nozzles specially constructed for positioning adjacent to another nozzle or to a fixed member, e.g. fairing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/385—Variable incidence wings
    • 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
    • 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
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • F02K1/006—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector within one plane only
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/04—Boundary layer controls by actively generating fluid flow
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/16—Boundary layer controls by blowing other fluids over the surface than air, e.g. He, H, O2 or exhaust gases
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Tires In General (AREA)
  • Testing Of Engines (AREA)
CH326061D 1953-04-08 1954-04-08 Antriebseinrichtung an einem Flugzeug CH326061A (de)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
GB326061X 1953-04-08
GB140753X 1953-07-14
GB70953X 1953-09-07
GB190354X 1954-03-19

Publications (1)

Publication Number Publication Date
CH326061A true CH326061A (de) 1957-11-30

Family

ID=27447572

Family Applications (1)

Application Number Title Priority Date Filing Date
CH326061D CH326061A (de) 1953-04-08 1954-04-08 Antriebseinrichtung an einem Flugzeug

Country Status (5)

Country Link
US (1) US2756008A (de)
CH (1) CH326061A (de)
DE (1) DE1021249B (de)
FR (1) FR1099647A (de)
NL (1) NL91484C (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2402077A1 (fr) * 1975-06-30 1979-03-30 Gen Electric Dispositif d'ejection manoeuvrable en vol pour un moteur a turbine a gaz

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3055614A (en) * 1960-05-12 1962-09-25 Wendell J Thompson Air-ejector aircraft
US4913479A (en) * 1989-01-31 1990-04-03 Allison Lawrence P M A Door knob handle attachment
ATE312754T1 (de) * 2004-01-26 2005-12-15 Fiat Ricerche Flugzeug mit einem antriebssystem bestehend aus mehreren pulsierten detonationskraftmaschinen
US7726609B2 (en) * 2007-03-16 2010-06-01 The Boeing Company High-performance low-noise aircraft exhaust systems and methods
JP5406251B2 (ja) * 2011-08-10 2014-02-05 網矢 ハル子 分散噴射型エンジン
DE102015207445B4 (de) * 2015-04-23 2023-08-17 Lilium GmbH Tragfläche für ein Luftfahrzeug und Luftfahrzeug
RU2637235C1 (ru) * 2016-11-02 2017-12-01 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") Импульсный плазменный тепловой актуатор эжекторного типа

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR694497A (fr) * 1929-07-31 1930-12-04 Perfectionnement aux aéronefs
DE693898C (de) * 1938-07-09 1940-07-20 Messerschmitt Boelkow Blohm Kraftgetriebene Einrichtung zur Beeinflussung der eugen
FR55362E (fr) * 1940-09-05 1952-06-27 Système d'emballage pour fromages ou autres produits
FR971992A (fr) * 1940-12-07 1951-01-24 Perfectionnements aux véhicules aériens à propulsion par réaction
FR55382E (fr) * 1941-02-24 1952-06-27 Perfectionnements aux véhicules aériens à propulsion par réaction
GB578837A (en) * 1941-10-14 1946-07-15 Boulton Aircraft Ltd Improvements in and relating to aircraft
US2568813A (en) * 1945-09-28 1951-09-25 Svenska Turbinfab Ab Jet-propelled aircraft with boundary layer control
US2479487A (en) * 1946-01-28 1949-08-16 Goembel William Philip Jet propelled airplane with wing discharge slot
US2557522A (en) * 1946-05-28 1951-06-19 Sncase Aerodynes equipped with reaction jet propulsion means
US2589732A (en) * 1948-07-22 1952-03-18 Onera (Off Nat Aerospatiale) Jet-propelled aircraft
GB656390A (en) * 1948-09-07 1951-08-22 Rolls Royce Improvements in or relating to aircraft and wing structures thereof
US2580339A (en) * 1949-03-19 1951-12-25 Jr George A Woodward Boundary layer control and intake system for aircraft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2402077A1 (fr) * 1975-06-30 1979-03-30 Gen Electric Dispositif d'ejection manoeuvrable en vol pour un moteur a turbine a gaz

Also Published As

Publication number Publication date
DE1021249B (de) 1957-12-19
FR1099647A (fr) 1955-09-07
US2756008A (en) 1956-07-24
NL91484C (de)

Similar Documents

Publication Publication Date Title
CH318287A (de) Schubdüseneinrichtung
FR1204592A (fr) Moteur-fusée
FR1194723A (fr) Moteur-fusée
CH326061A (de) Antriebseinrichtung an einem Flugzeug
FR1109799A (fr) Perfectionnements relatifs aux hélicoptères
FR1082009A (fr) Appareil aéronautique
CH331332A (de) Nachbrenner an einem Flugzeug-Strahltriebwerk
FR1140352A (fr) Dispositif de fusée
FR1073268A (fr) Aéronef
FR1087786A (fr) Parachute
FR1095546A (fr) Propulseur
CH314183A (de) Haltevorrichtung an Korbflasche
FR1073608A (fr) Scaphandre amphibie autonome
FR1072615A (fr) Appareil volant
AT179997B (de) Schutzhülle an Kleinfahrzeugen
FR1095157A (fr) Perfectionnement aux hélicoptères
FR1063718A (fr) Véhicule aérien
FR64040E (fr) Parachute
FR1117806A (fr) Avion perfectionné
FR1088338A (fr) Perfectionnements aux avions
AT184826B (de) Fluggerät
FR1076863A (fr) Fuselage d'aéronef
FR1096663A (fr) Propulseur de navires
FR1087451A (fr) Engin pyrotechnique
FR1115450A (fr) Appareil de vol du type aérogire