CONVERTIPLANE
First Claim
1. A convertiplane (1) comprising:
- a pair of semi-wings (3);
at least one first rotor (4) comprising a shaft (6) which may rotate about relative first axis (B) and tilt about a second axis (C) together with said first axis (B) with respect to said semi-wings (3) between a helicopter mode and an aeroplane mode;
said first axis (B) being, in use, transversal to a longitudinal direction (A) of said convertiplane (1) in said helicopter mode and being, in use, substantially parallel to said longitudinal direction (A) in said aeroplane mode;
characterized by comprising;
an electrical power storage device (70;
81, 82);
andat least one electrical machine (71);
said electrical machine (71) comprising, in turn,;
a stator (72) which is electrically connected to said storage device (70;
81, 82); and
a second rotor (73) which is operatively connected to a shaft (6) of said first rotor (4);
said electrical machine (71) being operable as;
an electric motor for driving in rotation said first rotor (4) by using the electrical power stored in said storage device (70;
81, 82);
oras an electrical power generator for re-charging said storage device (70;
81, 82) by causing the rotation of said first rotor (4) under the action of a wind current;
said first rotor (4) being tiltable about said second axis (C) in a direction facing the wind current, when said convertiplane (1) is on ground and said storage device (70;
81, 82) needs to be re-charged.
5 Assignments
0 Petitions
Accused Products
Abstract
There is described a convertiplane comprising: a pair of semi-wings; a first rotor comprising a shaft which may rotate about first axis and tilt about a second axis together with first axis with respect to semi-wings between a helicopter mode and an aeroplane mode; first axis being transversal to a longitudinal direction of convertiplane in helicopter mode and being substantially parallel to longitudinal direction in aeroplane mode; convertiplane also comprises an electrical power storage device; and an electrical machine which comprises, in turn, a stator electrically connected to storage device; and a second rotor operatively connected to a shaft of first rotor; electrical machine acts as an electric motor for driving in rotation said first rotor by using the electrical power stored in storage device; or as an electrical power generator for re-charging storage device by causing the rotation second rotor under the action of a wind current.
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Citations
12 Claims
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1. A convertiplane (1) comprising:
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a pair of semi-wings (3); at least one first rotor (4) comprising a shaft (6) which may rotate about relative first axis (B) and tilt about a second axis (C) together with said first axis (B) with respect to said semi-wings (3) between a helicopter mode and an aeroplane mode; said first axis (B) being, in use, transversal to a longitudinal direction (A) of said convertiplane (1) in said helicopter mode and being, in use, substantially parallel to said longitudinal direction (A) in said aeroplane mode; characterized by comprising; an electrical power storage device (70;
81, 82);and at least one electrical machine (71); said electrical machine (71) comprising, in turn,; a stator (72) which is electrically connected to said storage device (70;
81, 82); anda second rotor (73) which is operatively connected to a shaft (6) of said first rotor (4); said electrical machine (71) being operable as; an electric motor for driving in rotation said first rotor (4) by using the electrical power stored in said storage device (70;
81, 82);
oras an electrical power generator for re-charging said storage device (70;
81, 82) by causing the rotation of said first rotor (4) under the action of a wind current;said first rotor (4) being tiltable about said second axis (C) in a direction facing the wind current, when said convertiplane (1) is on ground and said storage device (70;
81, 82) needs to be re-charged.- View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10)
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11. A method of operating a convertiplane (1);
- said convertiplane (1) comprising;
a pair of semi-wings (3); at least one first rotor (4) which may rotate about relative first axis (B) and tilt about a second axis (C) together with said first axis (B) with respect to said semi-wings (3) between a helicopter mode and an aeroplane mode; said first axis (B) being, in use, transversal to a longitudinal direction (A) of said convertiplane (1) in said helicopter mode and being, in use, substantially parallel to said longitudinal direction (A) in said aeroplane mode; said method being characterized by comprising the steps of; operating an electrical machine (71) as an electric motor for driving in rotation said first rotor (4) by using the electrical power stored in an electrical power storage device (70;
81, 82); andoperating said electrical machine (71) as an electric power generator for re-charging said storage device (70;
81, 82);said step of operating said electrical machine (71) as an electric power generator comprising the step of using wind energy for driving in rotation said first rotor (4); said convertiplane (1) comprising; said electrical power storage device (70;
81, 82); andsaid at least one electrical machine (71); said electrical machine (71) comprising, in turn, a stator (72) which is electrically connected to said storage device (70;
81, 82); anda second rotor (73) which is operatively connected to said first rotor (4); characterized by comprising the step of tilting said first rotor (4) of a given angle about said second axis (C) before said step of operating said electrical machine (71) as an electric motor, when said convertiplane (1) is on ground and said storage device (70;
81, 82) needs to be re-charged;said given angle being associated to a main direction of the wind-current. - View Dependent Claims (12)
- said convertiplane (1) comprising;
Specification