TURBINE ENGINE WITH SINGLE WALL CANTILEVERED ARCHITECTURE

• Main Authors: GOULD KENNETH A, MARTIN MILES D'ANGELO, MARK GREGORY WOTZAK, BRIAN LEWIS DEVENDORF, DANIEL WASLO
• Format: Patent
• Language: English; Japanese
• Published: 22.03.2019
• Subjects: AIR INTAKES FOR JET-PROPULSION PLANTS; BLASTING; COMBUSTION ENGINES; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS; GAS-TURBINE PLANTS; HEATING; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS; LIGHTING; MECHANICAL ENGINEERING; WEAPONS

To provide a turbine engine with a single wall cantilevered architecture.SOLUTION: An apparatus and method for mounting a turbine engine (20) to an aircraft (10) can include an engine core (40) for the turbine engine (20) including a compressor section (42), a combustor section (48), and a turbine s...