Aircraft isolator devices, systems, and methods for isolating a structural component within an aircraft can include an engine interface, airframe, and one or more (e.g., a plurality of) isolator devices attached to the engine interface and the airframe. In some aspects, the isolator devices have a housing, which has a first surface and a second surface that together at least partially define a perimeter of the housing and is configured for attachment to the airframe; an engine attachment component configured for attachment to the engine interface and disposed at least partially inside of the housing; and a plurality of elastomeric elements disposed on or over each of the first and second surfaces of the housing The plurality of elastomeric elements are spaced apart from the engine attachment component via the housing for improved heat dissipation from the engine, reducing operational temperatures of the elastomeric elements to prolong their use.
ISOLATOR DEVICES, SYSTEMS AND METHODS FOR AIRCRAFT
ISOLATORVORRICHTUNGEN, -SYSTEME UND -VERFAHREN FÜR EIN FLUGZEUG
DISPOSITIFS, SYSTÈMES ET PROCÉDÉS D'ISOLATION POUR AÉRONEF
20.03.2019
Patent
Elektronische Ressource
Englisch