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BE682895A - - Google Patents

Info

Publication number
BE682895A
BE682895A BE682895DA BE682895A BE 682895 A BE682895 A BE 682895A BE 682895D A BE682895D A BE 682895DA BE 682895 A BE682895 A BE 682895A
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.)
Filing date
Publication date
Application filed filed Critical
Publication of BE682895A publication Critical patent/BE682895A/xx

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00Regulating or controlling by varying flow
    • F01D17/10Final actuators
    • F01D17/12Final actuators arranged in stator parts
    • F01D17/14Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047Heating to prevent icing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L27/00Adjustable joints; Joints allowing movement
    • F16L27/10Adjustable joints; Joints allowing movement comprising a flexible connection only
    • F16L27/1004Adjustable joints; Joints allowing movement comprising a flexible connection only introduced in exhaust pipes for hot gases
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L27/00Adjustable joints; Joints allowing movement
    • F16L27/12Adjustable joints; Joints allowing movement allowing substantial longitudinal adjustment or movement
    • F16L27/127Adjustable joints; Joints allowing movement allowing substantial longitudinal adjustment or movement with means for locking the longitudinal adjustment or movement in the final mounted position
    • F16L27/1274Adjustable joints; Joints allowing movement allowing substantial longitudinal adjustment or movement with means for locking the longitudinal adjustment or movement in the final mounted position by means of a swivel nut
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L37/00Couplings of the quick-acting type
    • F16L37/08Couplings of the quick-acting type in which the connection between abutting or axially overlapping ends is maintained by locking members
    • F16L37/12Couplings of the quick-acting type in which the connection between abutting or axially overlapping ends is maintained by locking members using hooks, pawls, or other movable or insertable locking members
    • F16L37/14Joints secured by inserting between mating surfaces an element, e.g. a piece of wire, a pin, a chain
    • F16L37/142Joints secured by inserting between mating surfaces an element, e.g. a piece of wire, a pin, a chain where the securing element is inserted tangentially
    • F16L37/148Joints secured by inserting between mating surfaces an element, e.g. a piece of wire, a pin, a chain where the securing element is inserted tangentially the securing element being flexible

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BE682895D 1965-08-19 1966-06-21 BE682895A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US481130A US3339832A (en) 1965-08-19 1965-08-19 Pipe connections for aircraft gas turbine engines

Publications (1)

Publication Number Publication Date
BE682895A true BE682895A (fr) 1966-12-01

Family

ID=23910733

Family Applications (1)

Application Number Title Priority Date Filing Date
BE682895D BE682895A (fr) 1965-08-19 1966-06-21

Country Status (4)

Country Link
US (1) US3339832A (fr)
BE (1) BE682895A (fr)
DE (1) DE1476791A1 (fr)
GB (1) GB1121222A (fr)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3434743A (en) * 1966-07-07 1969-03-25 Fmc Corp Well apparatus
IT217543Z2 (it) * 1988-12-02 1991-12-19 Metal Work Spa Raccordo per dispositivo destinato ad essere connesso ad un condotto di impianto di fluido in pressione
US5152499A (en) * 1990-05-18 1992-10-06 Sequoia Controls Limited Flow device body and slide-wire connector nut
US5219190A (en) * 1991-05-13 1993-06-15 General Electric Company Shear wire flange joint for a gas turbine engine
US6086118A (en) * 1991-09-10 2000-07-11 Bundy Corporation Quick connect tubing connector
US5232337A (en) * 1991-10-30 1993-08-03 General Electric Company Slip joint for maintaining concentricity
FR2707365B1 (fr) * 1993-07-09 1995-09-08 Assistance Proto Ind France Dispositif de montage d'un élément sur une pièce présentant un canal de fluide.
US5584512A (en) * 1993-10-07 1996-12-17 Carstensen; Kenneth J. Tubing interconnection system with different size snap ring grooves
FR2771452B1 (fr) * 1997-11-21 2000-04-14 Aerospatiale Dispositif de degivrage pour capot d'entree d'air de moteur a reaction
EP1079068A3 (fr) * 1999-08-27 2004-01-07 General Electric Company Tube connecteur pour le circuit de refroidissement d'un rotor de turbine
US8794916B2 (en) 2010-12-07 2014-08-05 Honda Motor Co., Ltd. Shroud supporting structure for gas turbine engine
EP2639411B1 (fr) * 2012-03-12 2014-12-10 MTU Aero Engines GmbH Boîtier de turbomachine avec un système de recirculation de fluide
US9441651B2 (en) * 2012-12-10 2016-09-13 Rolls-Royce Plc Joint assembly and method of using the same
US10443498B2 (en) 2014-08-15 2019-10-15 United Technologies Corporation Gas turbine engine cooling fluid metering system
EP3037629B1 (fr) * 2014-12-22 2018-08-29 Rolls-Royce plc Ensemble de raccord et son procédé d'utilisation
DE102016218239A1 (de) 2016-09-22 2018-03-22 MTU Aero Engines AG Dichtungsanordnung für ein Turbinenzwischengehäuse einer Gasturbine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US618194A (en) * 1899-01-24 Pipe connection for water-meters
GB540490A (en) * 1940-04-10 1941-10-20 Walter Arthur Melsom Improvements in and relating to pipe couplings
US2521127A (en) * 1948-05-08 1950-09-05 Wright Aeronautical Corp Fluid tight joint
US2672924A (en) * 1952-04-18 1954-03-23 Union Carbide & Carbon Corp Blowpipe with rotatable locking collar for quickly detachable head
DE1193451B (de) * 1962-03-24 1965-05-26 Minsup Mining Supplies Halterung fuer Schraemhauen an einer Schraemwalze
US3123283A (en) * 1962-12-07 1964-03-03 Anti-icing valve means

Also Published As

Publication number Publication date
US3339832A (en) 1967-09-05
GB1121222A (en) 1968-07-24
DE1476791A1 (de) 1969-10-23

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