Braid construction to match coefficients of thermal expansion for composite transmission housings
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[0017]FIG. 1 schematically illustrates a rotary-wing aircraft 10 having a main rotor assembly 12. The aircraft 10 includes an airframe 14 having an extending tail 16 which mounts an anti-torque rotor 18. The main rotor assembly 12 is driven through a transmission (illustrated schematically at 20) by one or more engines 22. Although a particular helicopter configuration is illustrated in the disclosed embodiment, other machines such as turbo-props, tilt-rotor and tilt-wing aircraft will also benefit from the present invention.
[0018] Referring to FIG. 2, the transmission 20 includes a transmission housing 30. The transmission housing 30 includes a composite outer structure 32 which is preferably fabricated from a graphite fiber reinforced composite. The composite outer structure 32 structurally supports an adjacent first composite support 34 and tail rotor take off drive 36.
[0019] The first composite support 34 is annular in shape and defines an axis 38. A bull gear 40 with a steel ...
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