A wheel assembly in accordance with various embodiments for use with an aircraft can include an inner surface (226), a first lug (214) extending into an area defined by the inner surface (226) and a heat shield (202) configured to be coupled to the first lug (214). The wheel assembly can also include a gasket (204) configured to be positioned between the inner surface and the heat shield (202) and to remain in place relative to the first lug (214) in response to rotation of the wheel assembly relative to the aircraft.
SHORT TRAPEZOIDAL WHEEL GASKET
KURZE TRAPEZFÖRMIGE RADDICHTUNG
JOINT DE ROUE TRAPÉZOÏDAL COURT
19.04.2017
Patent
Elektronische Ressource
Englisch