Patent · US Active

Aircraft propulsion unit

US12392305B2 · kind B2 · utility

0Cited by
8References
13Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 29, 2021
Grant dateAug 19, 2025
Priority date
Expiry dateNov 29, 2041

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/60
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

An aircraft propulsion unit including a nacelle and a turbojet engine. The aircraft propulsion unit includes an external envelope, at least one fan casing, at least one actuator, and at least one support structure. The external envelope includes fan cowls. The fan casing cooperates with the fan cowls to define an interior space configured to house a thrust reverser configured to be displaced between a first position and a second position. The actuator configured to move the thrust reverser between the first position and the second position The support structure connects the fan cowls and the fan. The support structure includes at least one aperture configured to allow passage of part of the actuator.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.