Wing mounted unducted fan engine

Aeronautics and astronautics – Aircraft power plants – Arrangement

Patent

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Details

244 65, B64D 2700

Patent

active

051351854

ABSTRACT:
An aircraft engine is mounted on an aircraft wing such that the wing wake sheds along a zone at a predetermined position on the engine disk thereby minimizing dynamic loads or resonance. For a prechosen or design set of engine conditions the strength of the dynamic load is a function of the radial location of the zone on the disk having at least one relative minima between the centerline and the perimeter of the disk. The zone is positioned on the disk such that the value of the function is essentially a relative minima.

REFERENCES:
patent: 1980233 (1934-11-01), Stout
patent: 2242198 (1941-05-01), Woods
patent: 2395513 (1946-02-01), Stalker
patent: 2397526 (1946-04-01), Bonbright
patent: 2402311 (1946-06-01), Bissett
patent: 2604276 (1952-07-01), Huben
patent: 4311289 (1982-01-01), Finch
patent: 4318516 (1982-03-01), Cole
patent: 4533101 (1985-08-01), Patterson
patent: 4629147 (1986-12-01), Johnson et al.
Batchelor, "An Introduction to Fluid Mechanics", 1967 (plate 7).

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