BE529656A - - Google Patents

Info

Publication number
BE529656A
BE529656A BE529656DA BE529656A BE 529656 A BE529656 A BE 529656A BE 529656D A BE529656D A BE 529656DA BE 529656 A BE529656 A BE 529656A
Authority
BE
Belgium
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 of BE529656A publication Critical patent/BE529656A/xx

Links

Classifications

    • A—HUMAN NECESSITIES
    • A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61K—PREPARATIONS FOR MEDICAL, DENTAL OR TOILETRY PURPOSES
    • A61K31/00—Medicinal preparations containing organic active ingredients
    • C—CHEMISTRY; METALLURGY
    • C07—ORGANIC CHEMISTRY
    • C07D—HETEROCYCLIC COMPOUNDS
    • C07D263/00—Heterocyclic compounds containing 1,3-oxazole or hydrogenated 1,3-oxazole rings
    • C07D263/02—Heterocyclic compounds containing 1,3-oxazole or hydrogenated 1,3-oxazole rings not condensed with other rings
    • C07D263/08—Heterocyclic compounds containing 1,3-oxazole or hydrogenated 1,3-oxazole rings not condensed with other rings having one double bond between ring members or between a ring member and a non-ring member
    • C07D263/10—Heterocyclic compounds containing 1,3-oxazole or hydrogenated 1,3-oxazole rings not condensed with other rings having one double bond between ring members or between a ring member and a non-ring member with only hydrogen atoms, hydrocarbon or substituted hydrocarbon radicals, directly attached to ring carbon atoms
    • C07D263/14—Heterocyclic compounds containing 1,3-oxazole or hydrogenated 1,3-oxazole rings not condensed with other rings having one double bond between ring members or between a ring member and a non-ring member with only hydrogen atoms, hydrocarbon or substituted hydrocarbon radicals, directly attached to ring carbon atoms with radicals substituted by oxygen atoms
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3053—Fixing blades to rotors; Blade roots ; Blade spacers by means of pins
    • 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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1207—Varying effective area of jet pipe or nozzle by means of pivoted flaps of one series of flaps hinged at their upstream ends on a fixed structure
    • 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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1223—Varying effective area of jet pipe or nozzle by means of pivoted flaps of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the downstream series having its flaps hinged at their upstream ends on the downstream ends of the flaps of the upstream series

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Organic Chemistry (AREA)
  • Health & Medical Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Health & Medical Sciences (AREA)
  • Pharmacology & Pharmacy (AREA)
  • Epidemiology (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Animal Behavior & Ethology (AREA)
  • Medicinal Chemistry (AREA)
  • Public Health (AREA)
  • Veterinary Medicine (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Nozzles (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Plural Heterocyclic Compounds (AREA)
  • Nitrogen- Or Sulfur-Containing Heterocyclic Ring Compounds With Rings Of Six Or More Members (AREA)
  • Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Supercharger (AREA)
  • Toys (AREA)
BE529656D 1953-04-10 BE529656A (sv)

Applications Claiming Priority (6)

Application Number Priority Date Filing Date Title
GB325950X 1953-04-10
GB318642X 1953-04-23
GB326650X 1953-05-18
GB327869X 1953-06-18
GB260354X 1954-03-26
GB20654X 1954-06-02

Publications (1)

Publication Number Publication Date
BE529656A true BE529656A (sv)

Family

ID=27546467

Family Applications (2)

Application Number Title Priority Date Filing Date
BE528164D BE528164A (sv) 1953-04-10
BE529656D BE529656A (sv) 1953-04-10

Family Applications Before (1)

Application Number Title Priority Date Filing Date
BE528164D BE528164A (sv) 1953-04-10

Country Status (7)

Country Link
US (2) US2980395A (sv)
BE (2) BE529656A (sv)
CH (4) CH325950A (sv)
DE (1) DE928345C (sv)
FR (4) FR1097487A (sv)
GB (4) GB742194A (sv)
NL (1) NL87657C (sv)

Families Citing this family (61)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1034637B (de) * 1954-11-04 1958-07-24 Rhone Poulenc Sa Verfahren zur Herstellung von Phenthiazinderivaten
DE1040032B (de) * 1954-11-04 1958-10-02 Rhone Poulenc Sa Verfahren zur Herstellung von Phenthiazinderivaten
DE1034639B (de) * 1954-11-29 1958-07-24 Rhone Poulenc Sa Verfahren zur Herstellung von racemischen und optisch aktiven Phenthiazinderivaten
US2928652A (en) * 1955-10-12 1960-03-15 Gen Electric Roll-pin support for turbomachine blades
DE1056611B (de) * 1955-11-15 1959-05-06 Rhone Poulenc Sa Verfahren zur Herstellung von Phenthiazinderivaten
BE552836A (sv) * 1955-11-25
NL96990C (sv) * 1956-01-10
NL97976C (sv) * 1956-04-07 Krupp Ag
US2931169A (en) * 1956-05-15 1960-04-05 Westinghouse Electric Corp Variable convergent-divergent exhaust nozzle
NL98004C (sv) * 1956-07-19
GB820059A (en) * 1956-07-30 1959-09-16 Bristol Aero Engines Ltd Improvements in or relating to jet propulsion nozzles
DE1088964B (de) * 1956-08-01 1960-09-15 Rhone Poulenc Sa Verfahren zur Herstellung von Phenthiazinderivaten
US3032974A (en) * 1956-08-24 1962-05-08 United Aircraft Corp Exhaust nozzle
BE562299A (sv) * 1956-11-15
FR1186182A (fr) * 1957-01-15 1959-08-17 Rhone Poulenc Sa Nouveaux dérivés nu-pipéraziniques substitués de la substituée-3 phénothiazine et leurs procédés de préparation
GB858579A (en) * 1957-01-17 1961-01-11 Havilland Engine Co Ltd Adjustable propulsion nozzles
DK97182C (da) * 1957-02-15 1963-10-28 Egyt Gyogyszervegyeszeti Gyar Fremgangsmåde til fremstilling af krystallinsk 3-chlor-10-(3'-dimethylaminopropyl)-phenthiazin.
DE1108225B (de) * 1957-02-22 1961-06-08 Egyt Gyogyszervegyeszeti Gyar Verfahren zur Herstellung von kristallinem 3-Chlor-10-(3'-dimethyl-aminopropyl)-phenthiazin
US3043563A (en) * 1957-04-16 1962-07-10 Aerpat Ag Turbine rotor mounting
GB872195A (en) * 1957-05-21 1961-07-05 English Electric Co Ltd Improvements in and relating to jet propulsion nozzles
US2906496A (en) * 1957-05-28 1959-09-29 Ransom S Thompson Retaining means for pin used for rotor blade attachment
US3003311A (en) * 1957-07-17 1961-10-10 Havilland Engine Co Ltd Adjustable propulsion nozzles
FR1212031A (fr) * 1957-10-21 1960-03-21 Rhone Poulenc Sa Dérivés de la phénothiazine substitués à l'azote par une chaîne basique comportant un hétérocycle et leur préparation
DE1101055B (de) * 1958-04-04 1961-03-02 Her Majesty The Queen In The R Querschnittsveraenderliche Vortriebsduese
DE1100635B (de) * 1958-04-22 1961-03-02 Rhone Poulenc Sa Verfahren zur Herstellung von Phenthiazinderivaten
DE1092476B (de) * 1958-04-24 1960-11-10 Rhone Poulenc Sa Verfahren zur Herstellung von Phenthiazinderivaten
US2932163A (en) * 1958-05-12 1960-04-12 Orenda Engines Ltd Means for actuating a variable nozzle
US2982518A (en) * 1959-01-28 1961-05-02 Gen Motors Corp Blade lock pin retainer
GB940979A (en) * 1959-02-03 1963-11-06 Rolls Royce Improvements relating to jet propulsion nozzles for gas turbine engines
US3042369A (en) * 1959-02-11 1962-07-03 Gen Motors Corp Pinned blade sealing means
US3039737A (en) * 1959-04-13 1962-06-19 Int Harvester Co Device for controlling clearance between rotor and shroud of a turbine
GB875517A (en) * 1959-06-12 1961-08-23 Rolls Royce Propelling nozzles for jet propulsion gas turbine engines
US3081021A (en) * 1959-10-14 1963-03-12 Gen Motors Corp Fabricated wheel and blade attachments
US3041822A (en) * 1960-04-21 1962-07-03 Chandler Evans Corp Nozzle control for turbojet engine
GB936044A (en) * 1960-11-28 1963-09-04 Rolls Royce Improvements in or relating to jet propulsion nozzle arrangements
BE635976A (sv) * 1962-08-10
US3694104A (en) * 1970-10-07 1972-09-26 Garrett Corp Turbomachinery blade
GB1605260A (en) * 1974-09-07 1986-11-12 Rolls Royce Gas turbine engines
US3979065A (en) * 1974-10-31 1976-09-07 United Technologies Corporation Cooling liner for an exhaust nozzle
US3972475A (en) * 1975-07-31 1976-08-03 United Technologies Corporation Nozzle construction providing for thermal growth
DE2711217A1 (de) * 1976-03-17 1977-09-22 Rolls Royce 1971 Ltd Verstellduese fuer gasturbinentriebwerke
US4081137A (en) * 1977-01-05 1978-03-28 The United States Of America As Represented By The Secretary Of The Air Force Finned surface cooled nozzle
US4181260A (en) * 1977-03-17 1980-01-01 General Electric Company Hydraulic actuation ring
US4176792A (en) * 1977-07-11 1979-12-04 General Electric Company Variable area exhaust nozzle
FR2724977B1 (fr) * 1980-12-30 1996-12-13 Snecma Tuyere convergente-divergente en particulier pour turboreacteur
FR2557211A1 (fr) * 1983-12-21 1985-06-28 Camboulives Andre Ensemble d'ejection, en particulier pour turboreacteur
US4659289A (en) * 1984-07-23 1987-04-21 United Technologies Corporation Turbine side plate assembly
US5102300A (en) * 1988-10-07 1992-04-07 United Technologies Corporation Pinned airfoil propeller assembly
JPH0711259B2 (ja) * 1989-09-07 1995-02-08 ゼネラル・エレクトリック・カンパニイ 排気ノズルヒンジ
US5101624A (en) * 1989-09-07 1992-04-07 General Electric Company Exhaust nozzle hinge
US5074753A (en) * 1989-10-16 1991-12-24 Bell Helicopter Textron Inc. Rotor blade
US5176323A (en) * 1991-04-15 1993-01-05 General Electric Company Reduced weight nozzle actuation mechanism
US5580219A (en) * 1995-03-06 1996-12-03 Solar Turbines Incorporated Ceramic blade attachment system
DE19516694C2 (de) * 1995-05-06 2001-06-28 Mtu Aero Engines Gmbh Einrichtung zur Fixierung von Laufschaufeln am Laufrad, insbesondere einer Turbine eines Gasturbinentriebwerks
DE19603388C1 (de) * 1996-01-31 1997-07-24 Mtu Muenchen Gmbh Einrichtung zur Fixierung der Laufschaufeln am Laufrad, insbesondere einer Turbine eines Gasturbinentriebwerks, durch Nietung
US5868351A (en) * 1996-05-23 1999-02-09 Bell Helicopter Textron Inc. Rotor blade stowing system
US6213719B1 (en) * 1999-07-28 2001-04-10 United Technologies Corporation Bar wedge preload apparatus for a propeller blade
EP1735531A4 (en) * 2003-12-01 2015-01-21 Univ Mississippi METHOD AND DEVICE FOR REDUCING MOTOR NOISE
DE102009013348A1 (de) * 2009-03-16 2010-09-23 Man Turbo Ag Vorrichtung und Verfahren zum Verbinden einer Schaufel mit einer Rotorwelle einer Strömungsmaschine
US20120051924A1 (en) * 2010-08-31 2012-03-01 General Electric Company Turbine Blade Assembly
RU2456468C1 (ru) * 2011-02-04 2012-07-20 Открытое акционерное общество "Научно-производственное объединение "Сатурн" (ОАО "НПО "Сатурн") Система переброса рабочего тела для поворотного сопла турбореактивного двигателя

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US612815A (en) * 1898-10-25 Rotary engine
GB302953A (en) * 1927-09-21 1928-12-21 Neil Shaw Muir Improvements in or relating to centrifugal blowers, compressors and the like
US2326145A (en) * 1941-03-18 1943-08-10 Westinghouse Electric & Mfg Co Turbine blade fastening
US2411895A (en) * 1944-04-15 1946-12-03 United Aircraft Corp Nozzle control
US2404076A (en) * 1944-05-04 1946-07-16 John W Leighton Adjustable threaded connection
US2406940A (en) * 1944-06-19 1946-09-03 Gen Motors Corp Pivot pin
US2462953A (en) * 1946-02-05 1949-03-01 United Aircraft Corp Adjustable cone orifice
US2435427A (en) * 1946-09-16 1948-02-03 United Specialties Co Turbine wheel
GB621315A (en) * 1947-02-17 1949-04-07 Frederick William Walton Morle Improvements relating to compressors and turbines
US2635848A (en) * 1948-10-28 1953-04-21 Packard Motor Car Co Rotor for gas turbines
US2697907A (en) * 1948-11-12 1954-12-28 Gen Motors Corp Multiplate variable area jet nozzle
US2625366A (en) * 1948-11-18 1953-01-13 Packard Motor Car Co Turbine rotor construction
US2634578A (en) * 1949-02-19 1953-04-14 Mcdonnell Aircraft Corp Device for varying the effective area of discharge orifices of jet engines or afterburners therefor
GB679714A (en) * 1949-04-21 1952-09-24 Rolls Royce Improvements in or relating to axial-flow compressors and turbines
US2711631A (en) * 1949-06-21 1955-06-28 Hartford Nat Bank & Trust Co Gas turbine power plant
FR989556A (fr) * 1949-06-25 1951-09-11 Cem Comp Electro Mec Perfectionnement aux aubes de turbo-machines
US2603062A (en) * 1949-09-30 1952-07-15 Westinghouse Electric Corp Variable area jet nozzle
US2819869A (en) * 1950-05-02 1958-01-14 Jr Andre J Meyer Mounting arrangement for turbine or compressor blading
US2682147A (en) * 1951-06-16 1954-06-29 Rohr Aircraft Corp Adjustable nozzle for exhaust gas

Also Published As

Publication number Publication date
FR1097487A (fr) 1955-07-06
FR1159179A (fr) 1958-06-24
GB742194A (en) 1955-12-21
GB820134A (en) 1959-09-16
DE928345C (de) 1955-05-31
CH318642A (fr) 1957-01-15
CH326650A (de) 1957-12-31
GB745069A (en) 1956-02-22
BE528164A (sv)
FR1099272A (fr) 1955-09-01
CH327869A (de) 1958-02-15
US2801516A (en) 1957-08-06
CH325950A (de) 1957-11-30
GB782493A (en) 1957-09-11
FR1107564A (fr) 1956-01-03
US2980395A (en) 1961-04-18
NL87657C (sv)

Similar Documents

Publication Publication Date Title
AT193854B (sv)
AT191364A (sv)
AT190646B (sv)
BE517130A (sv)
AT193331B (sv)
JPS316220B1 (sv)
AT189958B (sv)
AT191026B (sv)
AT191140B (sv)
AT192380B (sv)
AT191238B (sv)
BE517732A (sv)
BE517254A (sv)
BE561561A (sv)
BE531370A (sv)
NL87657C (sv)
BE530705A (sv)
BE529216A (sv)
BE528877A (sv)
BE526902A (sv)
BE523115A (sv)
BE521785A (sv)
BE517828A (sv)
BE488396A (sv)
BE506054A (sv)