FR1588007A - - Google Patents
Info
- Publication number
- FR1588007A FR1588007A FR1588007DA FR1588007A FR 1588007 A FR1588007 A FR 1588007A FR 1588007D A FR1588007D A FR 1588007DA FR 1588007 A FR1588007 A FR 1588007A
- Authority
- FR
- France
- Legal status (The legal status 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 status listed.)
- Expired
Links
Classifications
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
- H02K7/18—Structural association of electric generators with mechanical driving motors, e.g. with turbines
- H02K7/1807—Rotary generators
- H02K7/1823—Rotary generators structurally associated with turbines or similar engines
-
- 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
- F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
- F01D15/10—Adaptations for driving, or combinations with, electric generators
-
- 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
-
- 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
- F02C7/32—Arrangement, mounting, or driving, of auxiliaries
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4790567A GB1174969A (en) | 1967-10-20 | 1967-10-20 | Gas Turbine Engine Provided with an Alternator |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1588007A true FR1588007A (en) | 1970-04-03 |
Family
ID=10446675
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1588007D Expired FR1588007A (en) | 1967-10-20 | 1968-10-18 |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE1803419A1 (en) |
FR (1) | FR1588007A (en) |
GB (1) | GB1174969A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2922265A1 (en) * | 2007-10-12 | 2009-04-17 | Snecma Sa | Ducted-fan and twin-spool turbine engine for aircraft, has current generator including permanent magnet rotor and stator that are centered on axis of motor, where rotor is driven by rotor shaft and stator is integrated to intermediate case |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2250726B (en) * | 1990-11-24 | 1995-01-11 | Dominic Wickman | Hydro electric vehicle drive system |
GB2409936B (en) | 2001-02-09 | 2005-09-14 | Rolls Royce Plc | Gas turbine with electrical machine |
FR2842565B1 (en) * | 2002-07-17 | 2005-01-28 | Snecma Moteurs | INTEGRATED GENERATOR STARTER FOR TURBOMACHINE |
DE102004004945A1 (en) * | 2004-01-31 | 2005-08-18 | Mtu Aero Engines Gmbh | Gas turbine, in particular aircraft engine |
FR2919896B1 (en) | 2007-08-07 | 2009-10-30 | Snecma Sa | TURBOREACTOR COMPRISING A CURRENT GENERATOR MOUNTED IN THE BLOWER AND A METHOD FOR MOUNTING THE SAME GENERATOR IN THE SOUFFLANTE |
FR2921978B1 (en) * | 2007-10-08 | 2014-04-11 | Snecma | TURBOREACTOR WITH ELECTRIC GENERATOR AGENCY IN THE SOUFFLANTE |
CA2744474C (en) * | 2008-11-24 | 2018-05-01 | Ole Bjorn Kleven | Gas turbine with external combustion, applying a rotating regenerating heat exchanger |
US20110018273A1 (en) * | 2009-07-27 | 2011-01-27 | Rolls-Royce Corporation | Starter/generator integrated into compressor of turbine engine |
US8745990B2 (en) | 2009-07-27 | 2014-06-10 | Rolls-Royce Corporation | Gas turbine engine with integrated electric starter/generator |
US8294316B2 (en) | 2009-07-28 | 2012-10-23 | Rolls-Royce North American Technologies, Inc. | Electrical power generation apparatus for contra-rotating open-rotor aircraft propulsion system |
EP2388890A1 (en) * | 2010-05-19 | 2011-11-23 | Siemens Aktiengesellschaft | Generator with aluminium winding and wind turbine |
US8522522B2 (en) | 2010-07-30 | 2013-09-03 | Hamilton Sundstrand Corporation | Fan embedded power generator |
US8519555B2 (en) * | 2010-11-29 | 2013-08-27 | Pratt & Whitney Canada Corp. | Combination low spool generator and ram air turbine generator |
EP2949876B1 (en) * | 2014-05-29 | 2020-07-08 | Rolls-Royce Corporation | System and method to manage engine transients for rapid power demand changes |
CN111484761B (en) * | 2020-06-12 | 2021-06-25 | 西南交通大学 | Preparation method of anti-icing ultraviolet-proof coating |
GB202103747D0 (en) * | 2021-03-18 | 2021-05-05 | Rolls Royce Plc | Turbine generator |
-
1967
- 1967-10-20 GB GB4790567A patent/GB1174969A/en not_active Expired
-
1968
- 1968-10-16 DE DE19681803419 patent/DE1803419A1/en active Pending
- 1968-10-18 FR FR1588007D patent/FR1588007A/fr not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2922265A1 (en) * | 2007-10-12 | 2009-04-17 | Snecma Sa | Ducted-fan and twin-spool turbine engine for aircraft, has current generator including permanent magnet rotor and stator that are centered on axis of motor, where rotor is driven by rotor shaft and stator is integrated to intermediate case |
Also Published As
Publication number | Publication date |
---|---|
DE1803419A1 (en) | 1969-06-19 |
GB1174969A (en) | 1969-12-17 |
Similar Documents
Legal Events
Date | Code | Title | Description |
---|---|---|---|
TP | Transmission of property | ||
TP | Transmission of property | ||
ST | Notification of lapse |