NL73561C - - Google Patents

Info

Publication number
NL73561C
NL73561C NL73561DA NL73561C NL 73561 C NL73561 C NL 73561C NL 73561D A NL73561D A NL 73561DA NL 73561 C NL73561 C NL 73561C
Authority
NL
Netherlands
Application number
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.)
Publication date
Application granted granted Critical
Publication of NL73561C publication Critical patent/NL73561C/xx

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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/08—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being continuous
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M9/00—Aerodynamic testing; Arrangements in or on wind tunnels
    • G01M9/02—Wind tunnels
    • G01M9/04—Details
NL73561D 1947-04-22 NL73561C (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB264811X 1947-04-22
GB220348X 1948-03-22

Publications (1)

Publication Number Publication Date
NL73561C true NL73561C (de) 1953-06-15

Family

ID=26255664

Family Applications (1)

Application Number Title Priority Date Filing Date
NL73561D NL73561C (de) 1947-04-22

Country Status (5)

Country Link
US (1) US2573834A (de)
CH (1) CH264811A (de)
FR (1) FR964216A (de)
GB (1) GB636605A (de)
NL (1) NL73561C (de)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2721715A (en) * 1951-09-28 1955-10-25 Chance Vought Aircraft Inc Flush inlet
US2877965A (en) * 1952-04-22 1959-03-17 George H Wakefield Jet inlet diffuser for supersonic flying wing
US2772620A (en) * 1952-07-03 1956-12-04 Ferri Antonio Air inlet for supersonic airplane or missile
FR1104644A (fr) * 1954-02-15 1955-11-22 Thomson Houston Comp Francaise Perfectionnements aux systèmes de commande de l'écoulement d'un fluide
US3062484A (en) * 1953-04-10 1962-11-06 Curtiss Wright Corp Supersonic air inlet construction
US2776806A (en) * 1954-02-05 1957-01-08 United Aircraft Corp Weathercocking supersonic wedge diffuser for air inlets in aircraft
US2990142A (en) * 1955-05-11 1961-06-27 Curtiss Wright Corp Scoop-type supersonic inlet with precompression surface
US2967678A (en) * 1956-08-13 1961-01-10 Chance Vought Aircraft Inc Duct airflow stabilizing and aircraft braking means
DE1061570B (de) * 1956-10-27 1959-07-16 Messerschmitt Boelkow Blohm Einlaufdiffusor fuer UEberschallstrahltriebwerke
US2918229A (en) * 1957-04-22 1959-12-22 Collins Radio Co Ducted aircraft with fore elevators
US3074668A (en) * 1958-12-10 1963-01-22 Snecma Burner for hot fuel
US4924228A (en) * 1963-07-17 1990-05-08 Boeing Company Aircraft construction
US4198357A (en) * 1978-12-08 1980-04-15 Dresser Industries, Inc. Flow device and method
US4418879A (en) * 1980-12-29 1983-12-06 The Boeing Company Scoop and inlet for auxiliary power units and method
US4569494A (en) * 1982-12-23 1986-02-11 The Boeing Company Pitch control of swept wing aircraft
US4706910A (en) * 1984-12-27 1987-11-17 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Combined riblet and lebu drag reduction system
US20070181743A1 (en) * 2006-02-08 2007-08-09 Lockheed Martin Corporation Method for streamline traced external compression inlet
US8944774B2 (en) 2012-01-03 2015-02-03 General Electric Company Gas turbine nozzle with a flow fence
US9062554B2 (en) 2012-01-03 2015-06-23 General Electric Company Gas turbine nozzle with a flow groove
CN113062803B (zh) * 2021-04-09 2022-04-26 北京航空航天大学 一种分离边界层的分层式进气道及其造型方法

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR868609A (fr) * 1939-10-13 1942-01-09 B M W Flugmotorenbau G M B H Dispositif pour influencer les conditions aérodynamiques sur le côté de courant d'impact de corps munis d'un revêtement, notamment de groupes propulseurs d'aéronefs
US2334070A (en) * 1942-04-25 1943-11-09 William J Conley Aircraft
BE462775A (de) * 1945-02-01

Also Published As

Publication number Publication date
GB636605A (en) 1950-05-03
FR964216A (de) 1950-08-08
US2573834A (en) 1951-11-06
CH264811A (de) 1949-10-31

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