Compound helicopter
First Claim
1. A compound helicopter comprising:
- a fuselage with an upper side, a lower side opposed to the upper side, a left hand side, a right hand side, and a transverse axis extending from the left hand side to the right hand side;
at least one engine disposed on the upper side of the fuselage;
a main rotor mounted to the upper side of the fuselage at the transverse axis, the main rotor being driven by the at least one engine;
a first fixed wing mounted on the left hand side and a second fixed wing mounted on the right hand side of the fuselage; and
a respective longitudinally oriented propulsion device mounted to each of the fixed wings at a respective tip of each of the fixed wings, the fixed wings encompassing encompassing each a respective drive shaft from the at least one engine, wherein;
each fixed wing comprises a lower main wing and an upper secondary;
wing, and the upper secondary wing is anhedral;
the upper secondary wing and the lower main wing of each fixed wing are connected to each other within an interconnection region;
each respective propulsion device is arranged at the respective interconnection region of the respective fixed wing aft of the transverse axis, the propulsion devices including propellers in pusher configuration, the propellers being arranged aft of respective trailing edges of the respective fixed wings; and
and the upper secondary wings house the respective drive shafts from the at least one engine.
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Accused Products
Abstract
The invention relates to a compound helicopter comprising a fuselage, at least one engine and a main rotor driven by said at least one engine. At least one pair of fixed wings are mounted in an essentially horizontal plane on a left hand and a right hand side of the fuselage and horizontally oriented propulsion devices are mounted to each of the fixed wings, the fixed wings encompassing each a drive shaft from the at least one engine. Each fixed wing comprises a lower main wing and an upper secondary wing being connected to each other within an interconnection region. The propulsion devices include pusher propellers arranged at the interconnection region and the upper secondary wing houses the drive shaft from the at least one engine.
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Citations
18 Claims
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1. A compound helicopter comprising:
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a fuselage with an upper side, a lower side opposed to the upper side, a left hand side, a right hand side, and a transverse axis extending from the left hand side to the right hand side; at least one engine disposed on the upper side of the fuselage; a main rotor mounted to the upper side of the fuselage at the transverse axis, the main rotor being driven by the at least one engine; a first fixed wing mounted on the left hand side and a second fixed wing mounted on the right hand side of the fuselage; and a respective longitudinally oriented propulsion device mounted to each of the fixed wings at a respective tip of each of the fixed wings, the fixed wings encompassing encompassing each a respective drive shaft from the at least one engine, wherein; each fixed wing comprises a lower main wing and an upper secondary; wing, and the upper secondary wing is anhedral; the upper secondary wing and the lower main wing of each fixed wing are connected to each other within an interconnection region; each respective propulsion device is arranged at the respective interconnection region of the respective fixed wing aft of the transverse axis, the propulsion devices including propellers in pusher configuration, the propellers being arranged aft of respective trailing edges of the respective fixed wings; and and the upper secondary wings house the respective drive shafts from the at least one engine. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15)
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16. A rotorcraft comprising:
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a fuselage with a port side, a starboard side, and a transverse axis extending from the port side to the starboard side; at least one engine; a main rotor mounted to the fuselage at the transverse axis, the main rotor being driven by the at least one engine; a first fixed wing coupled to the port side, the first fixed wing including a first lower wing and a first upper wing joining at a first junction, the first junction being spaced from the fuselage; a second fixed wing coupled to the starboard side, the second fixed wing including a second lower wing and a second upper wing joining at a second junction, the second junction being spaced from the fuselage; a first propulsion device coupled to the first junction at a tip of the first fixed wing and driven by the at least one engine, the first propulsion device including a first pusher propeller arranged aft of the first fixed wing and aft of the transverse axis; and a second propulsion device coupled to the second junction at a tip of the second fixed wing and driven by the at least one engine, the second propulsion device including a second pusher propeller arranged aft of the second fixed wing and aft of the transverse axis. - View Dependent Claims (17, 18)
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Specification