Hybrid aircraft wheel comprising metal and composite portions

Aeronautics and astronautics – Landing gear – Wheel

Reexamination Certificate

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C301S064702, C301S095102

Reexamination Certificate

active

08042766

ABSTRACT:
An aircraft wheel (14) comprises a metal support structure (30) having a first annular ring (31) and a second annular ring (32) connected via at least one connecting element (37); and a fiber-enforced, molded-composite body. The metal support structure (30) is at least partially embedded in the composite body to form a first aircraft wheel section (20, 22) having a rim flange (16a,16b) for forming a seal with a tire.

REFERENCES:
patent: 4244413 (1981-01-01), Takahashi et al.
patent: 5080444 (1992-01-01), Hopkins et al.
patent: 5985072 (1999-11-01), Finck et al.
patent: 7066228 (2006-06-01), Grimberg et al.
patent: 7377596 (2008-05-01), Steinke et al.

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