Aircraft
The aircraft has a main body 1 and a pair of sub bodies 4 and 5 positioned substantially in parallel with the main body 1 and respectively in both of the left and right sides of the main body 1 . A canard 3 and main wings 8 and 9 each have a central portion fixed to the main body 1 and portions fixe...
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| Main Author | |
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| Format | Patent |
| Language | English |
| Published |
07.10.2004
|
| Online Access | Get full text |
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| Summary: | The aircraft has a main body
1
and a pair of sub bodies
4
and
5
positioned substantially in parallel with the main body
1
and respectively in both of the left and right sides of the main body
1
. A canard
3
and main wings
8
and
9
each have a central portion fixed to the main body
1
and portions fixed respectively to the sub bodies
4
and
5
, near left and right ends of the wings. Engines
6
and
7
are respectively mounted on outer surfaces of the sub bodies
4
and
5
. The sub bodies
4
and
5
are thinner than the main body
1
. The canard
3
, which is positioned closest to the fore end of the aircraft, has a shorter wing span than the other wings. The sub bodies
4
and
5
contain fuel. The fuel is supplied to the engines
6
and
7
assuring high safety. The main wings
8
and
9
are positioned, shifted respectively forth and back relative to the main body
1
. Therefore, stability is not impaired even if cargos are loaded into the main body over a wide range from the bow to the tail. |
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