Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Turbojet having a large bypass ratio

Turbojet having a large bypass ratio

US Patent 7430852 · Granted Oct 7, 2008

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Structure for linking and supporting a turbine engine on an aircraft pylon2025
System for managing the deceleration of an aircraft on a runway on the ground an2025
Turbomachine lubrication system comprising a bypass for preferentially supplying2025
Assembly for supporting an accessory gearbox of an aircraft turbine engine2025
Aircraft turbomachine comprising means for priming the lubricating pump2024
System for controlling an aircraft thrust reversal means2024
Aircraft with an offset nacelle aligned with the wake of the wing2024
Power-over-ethernet (PoE) control system2023
Drive unit for an aircraft having lifting points, and carriages for supporting s2023
Switching converter controller with soft stop2022
Power stage controller for switching converter with clamp2022
Portion of a fluid drainage conduit for a turbomachine2022