Fuel efficient fixed wing aircraft
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United States of America Patent
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Jun 23, 2009
Grant Date -
May 1, 2008
app pub date -
Oct 26, 2006
filing date -
Oct 26, 2006
priority date (Note) -
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Abstract
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.
First Claim
Family
- 15 United States
- 10 France
- 8 Japan
- 7 China
- 5 Korea
- 2 Other
Patent Owner(s)
- HUTTERER, GLADYS IRENE;HUTTERER, JOSEPH O'CONNOR;HUTTERER, MICHAEL JOSEPH;VAN HORNE, CONSTANCE LOUISE;ZECHMANN, ANGELA JOAN
International Classification(s)
Inventor(s)
Inventor Name | Address | # of filed Patents | Total Citations |
---|---|---|---|
Hutterer, Joseph A | 443 Elpyco | 1 | 10 |
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Fee | Large entity fee | small entity fee | micro entity fee |
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Surcharge after expiration - Late payment is unavoidable | $700.00 | $350.00 | $175.00 |
Surcharge after expiration - Late payment is unintentional | $1,640.00 | $820.00 | $410.00 |
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