COOLING CONFIGURATION FOR ENGINE COMPONENT
This disclosure relates to a gas turbine engine. The engine includes a component having a first wall and a second wall spaced-apart from the first wall. The component further includes a cooling passageway provided in part by a helical wall between the first wall and the second wall.
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Main Authors | , |
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Format | Patent |
Language | English French German |
Published |
15.01.2020
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Subjects | |
Online Access | Get full text |
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Abstract | This disclosure relates to a gas turbine engine. The engine includes a component having a first wall and a second wall spaced-apart from the first wall. The component further includes a cooling passageway provided in part by a helical wall between the first wall and the second wall. |
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AbstractList | This disclosure relates to a gas turbine engine. The engine includes a component having a first wall and a second wall spaced-apart from the first wall. The component further includes a cooling passageway provided in part by a helical wall between the first wall and the second wall. |
Author | SLAVENS, Thomas N SNYDER, Brooks E |
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DocumentTitleAlternate | CONFIGURATION DE REFROIDISSEMENT POUR UN COMPOSANT DE MOTEUR KÜHLKONFIGURATION FÜR MOTORKOMPONENTEN |
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Notes | Application Number: EP20140864478 |
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PublicationDateYYYYMMDD | 2020-01-15 |
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PublicationDecade | 2020 |
PublicationYear | 2020 |
RelatedCompanies | United Technologies Corporation |
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Snippet | This disclosure relates to a gas turbine engine. The engine includes a component having a first wall and a second wall spaced-apart from the first wall. The... |
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SubjectTerms | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS |
Title | COOLING CONFIGURATION FOR ENGINE COMPONENT |
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