Aircraft wing pylon extensions for minimized aerodynamic penalti

Details Aircraft wing pylon extensions for minimized aerodynamic penalti Aircraft wing pylon extensions for minimized aerodynamic penalti

1990-12-12

1992-04-07

Peters, Jr., Joseph F.

Aeronautics and astronautics

Aircraft power plants

Mounting

244130, B64D 2726

Patent

active

051020696

ABSTRACT:
A wing mounted pylon for an aircraft in which the pylon can be maintained in a desired maximum thickness consistent with structural and accessory and equipment space requirement but with substantially zero aerodynamic penalties. The maximum parallel thickness extends over at least a portion of the pylon length and is then maintained beyond the wing local trailing edge by means of a trailing edge extension fairing.

REFERENCES:
patent: 4067518 (1978-01-01), Paterson et al.
patent: 4314681 (1982-02-01), Kutney
patent: 4637573 (1987-01-01), Perin et al.
patent: 4712750 (1987-12-01), Ridgwell
patent: 4867394 (1989-09-01), Patterson, Jr.

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