TURBINE SHAFT POWER TAKE-OFF

• Main Author: LEFEBVRE, Guy
• Format: Patent
• Language: English; French; German
• Published: 24.01.2018
• 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

A multi-spool gas turbine engine (10) comprises a low pressure (LP) spool (20) and a high pressure (HP) spool (40) independently rotatable of one another about an engine axis (17). The LP spool (20) comprises an LP turbine (21), an LP compressor (22) and an LP shaft (23). The HP pressure spool (40)...