JPH05240063

PURPOSE: To realize heat expansion without stress, reduction of space and weight, and replacement of component elements respectively simultaneously by providing means for supporting a heat exchanger on an engine casing via intermediate plates at one end of each of pipes. CONSTITUTION: A gas turbine...

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Bibliographische Detailangaben
Hauptverfasser:	HERUMUUTO GURESU, KAARU MAIAA, KURISUTEIAN GUROINE
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OFGENERAL APPLICATION GAS-TURBINE PLANTS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HEAT EXCHANGE IN GENERAL HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE WEAPONS
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Beschreibung
Zusammenfassung:	PURPOSE: To realize heat expansion without stress, reduction of space and weight, and replacement of component elements respectively simultaneously by providing means for supporting a heat exchanger on an engine casing via intermediate plates at one end of each of pipes. CONSTITUTION: A gas turbine 1 comprises a recuperative exhaust gas heat exchanger 2 and a transmission 3. The gas turbine 1 also comprises a compressor 4 driven by a turbine 6 via a turbine shaft 5 and a combustion chamber 7. The transmission 3 is driven by an effective output turbine 8. In this case, the heat exchanger 2 is supported in an engine casing 28 at one end of each of pipes 10a, 10b via intermediate plates 11, 12. The pipes 10a, 10b are supported in a suitable through hole 17 of one of the intermediate plates 11. The other end of each of the pipes 10a, 10b is connected to the engine casing 28 via the other intermediate plate 12, being movable axially with respect to the radial supporter.