Fuel efficient fixed wing aircraft

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 7549604
APP PUB NO 20080099599A1
SERIAL NO

11553016

Stats

ATTORNEY / AGENT: (SPONSORED)

Importance

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Abstract

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A fixed wing aircraft having a fuselage having a forward end and a rearward end, the fuselage's forward end forming a nose section; the aircraft further having a primary thrust turbo-prop engine fixedly mounted upon the fuselage's rearward end; the aircraft further having an auxiliary thrust turbo-fan jet engine; the aircraft further having a pivot axle and support strut combination interconnecting the auxiliary thrust turbo-fan engine and the fuselage, the pivot axle and support strut combination positioning the auxiliary thrust turbo-fan jet engine within the fuselage's nose section; the aircraft further having an auxiliary thrust port extending through an outer wall of the nose section, the pivot axle and support strut combination being adapted for alternately moving the turbo-fan engine between first and second positions, the turbo-fan engine residing within the nose section upon movement to the first position, the turbo-fan engine outwardly overlying the auxiliary thrust port upon alternate movement to the second position.

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First Claim

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Patent Owner(s)

  • HUTTERER, GLADYS IRENE;HUTTERER, JOSEPH O'CONNOR;HUTTERER, MICHAEL JOSEPH;VAN HORNE, CONSTANCE LOUISE;ZECHMANN, ANGELA JOAN

International Classification(s)

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  • [Patents Count]

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Hutterer, Joseph A 443 Elpyco 1 10

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