An assembly for an aircraft propulsion system includes an upstream cowl and a downstream cowl. The upstream cowl extends axially from a first upstream end to a first downstream end. The upstream cowl includes an inner barrel panel, an outer barrel panel, and a bulkhead. The bulkhead extends radially between and connects the inner barrel panel and the outer barrel panel at the first downstream end. The downstream cowl extends axially from a second upstream end to a second downstream end. The downstream cowl includes a cowl panel and a seal assembly. The seal assembly includes a seal frame and a seal member. The seal frame is mounted to the bulkhead. The seal member is mounted to the cowl panel. The seal member includes a first radial portion projecting away from the cowl panel. The first radial portion is located at the second upstream end.
COWL SEAL ASSEMBLY FOR AN AIRCRAFT PROPULSION SYSTEM
VERKLEIDUNGSDICHTUNGSANORDNUNG FÜR EIN FLUGZEUGANTRIEBSSYSTEM
ENSEMBLE D'ÉTANCHÉITÉ DE CAPOT POUR SYSTÈME DE PROPULSION D'AÉRONEF
2024-01-03
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
LATCH ASSEMBLY FOR AN AIRCRAFT PROPULSION SYSTEM COWL
Europäisches Patentamt | 2024
|LATCH ASSEMBLY FOR AN AIRCRAFT PROPULSION SYSTEM COWL
Europäisches Patentamt | 2024
|