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
Links
Classifications
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- 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
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
- F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
- F02C6/08—Gas-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
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- 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
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
- F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
- F01D17/162—Final 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
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- 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
- F02C7/047—Heating to prevent icing
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L27/00—Adjustable joints; Joints allowing movement
- F16L27/10—Adjustable joints; Joints allowing movement comprising a flexible connection only
- F16L27/1004—Adjustable joints; Joints allowing movement comprising a flexible connection only introduced in exhaust pipes for hot gases
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L27/00—Adjustable joints; Joints allowing movement
- F16L27/12—Adjustable joints; Joints allowing movement allowing substantial longitudinal adjustment or movement
- F16L27/127—Adjustable joints; Joints allowing movement allowing substantial longitudinal adjustment or movement with means for locking the longitudinal adjustment or movement in the final mounted position
- F16L27/1274—Adjustable 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
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L37/00—Couplings of the quick-acting type
- F16L37/08—Couplings of the quick-acting type in which the connection between abutting or axially overlapping ends is maintained by locking members
- F16L37/12—Couplings 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
- F16L37/14—Joints secured by inserting between mating surfaces an element, e.g. a piece of wire, a pin, a chain
- F16L37/142—Joints 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
- F16L37/148—Joints 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)
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)
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)
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 |
-
1965
- 1965-08-19 US US481130A patent/US3339832A/en not_active Expired - Lifetime
-
1966
- 1966-06-20 GB GB27375/66A patent/GB1121222A/en not_active Expired
- 1966-06-21 BE BE682895D patent/BE682895A/xx unknown
- 1966-07-06 DE DE19661476791 patent/DE1476791A1/de active Pending
Also Published As
Publication number | Publication date |
---|---|
US3339832A (en) | 1967-09-05 |
GB1121222A (en) | 1968-07-24 |
DE1476791A1 (de) | 1969-10-23 |