Patents by Inventor Arnaud Chambreuil
Arnaud Chambreuil has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).
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Patent number: 7451947Abstract: This invention relates to a mounting structure (1) for mounting an engine (2) under an aircraft wing (4), the structure comprising a rigid structure (8) and means (10) of fastening this rigid structure under the wing, the mounting means comprising a forward fastener (14), an intermediate fastener (15) and an aft fastener (16). According to the invention, the forward fastener has at least one triangular shackle on each side of a vertical plane passing through a longitudinal axis (5) of the engine (2), placed in a vertical plane oriented along a longitudinal direction (X) of the aircraft. Furthermore, the intermediate fastener comprises a connecting rod capable of transferring forces applied in a direction (Y) transverse to the aircraft, and the aft fastener comprises at least one shackle oriented along a vertical direction (Z) of the aircraft.Type: GrantFiled: November 15, 2004Date of Patent: November 18, 2008Assignee: Airbus FranceInventors: Stephane Machado, Jerome Cassagne, Anthony Del Blanco, Yvon Martin, Arnaud Chambreuil
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Patent number: 7350747Abstract: This invention relates to a structure (1) for mounting an engine (2) under an aircraft wing (4), comprising a rigid structure (8) and means (10) of mounting this rigid structure under the wing, the mounting means (10) comprising a forward fastener (14) and an aft fastener (16). According to the invention, the forward fastener has at least one triangular shackle on each side of a vertical plane passing through a longitudinal axis (5) of the engine, placed in a vertical plane oriented along a direction inclined with respect to a longitudinal direction (X) and a transverse direction (Y) of the aircraft, and located in a horizontal plane defined by these directions (X) and (Y). Furthermore, the aft fastener comprises at least one shackle oriented along a vertical direction (Z) of the aircraft.Type: GrantFiled: November 24, 2004Date of Patent: April 1, 2008Assignee: Airbus FranceInventors: Stéphane Machado, Jérôme Cassagne, Anthony Del Blanco, Yvon Martin, Arnaud Chambreuil
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Patent number: 7296768Abstract: A structure for mounting a turboprop under an aircraft wing includes a rigid structure and a device for fastening the turboprop on the rigid structure. The rigid structure is composed of a box, and the device for fastening includes at least two lateral connecting rods resisting the engine torque generated by the turboprop, the connecting rods being arranged on each side of the box and each having a forward end connected to a gear box of the turboprop, and an aft end connected to the box.Type: GrantFiled: November 15, 2004Date of Patent: November 20, 2007Assignee: Airbus FranceInventors: Stephane Machado, Jerome Cassagne, Anthony Del Blanco, Yvon Martin, Arnaud Chambreuil
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Patent number: 7159819Abstract: A mounting structure for mounting a turboprop under an aircraft wing includes a rigid structure provided with an aft underwing box, and at least one forward rigid section. Each forward rigid section has two transverse frames at a spacing from each other. At least one forward rigid section of the rigid structure also includes at least one forward upper box connecting a top part of the two transverse frames of the forward rigid section.Type: GrantFiled: November 15, 2004Date of Patent: January 9, 2007Assignee: Airbus FranceInventors: Stephane Machado, Jerome Cassagne, Anthony Del Blanco, Yvon Martin, Arnaud Chambreuil
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Patent number: 7121504Abstract: The invention relates to a hanging device (1) connecting an engine (2) to a wing (4) of an aircraft, with the device being made up of a rigid structure (8) and hanging equipment (10) interposed between the rigid structure (8) and the wing (4), with the hanging equipment (10) being made up of a forward attachment (14) and a rear attachment (16) made up of at leas one triangular shackle placed in a vertical plane aligned in a transverse direction (Y) of the aircraft. According to the invention, the forward attachment (14) has, on one side and the other of a vertical plane passing through a longitudinal axis (5) of the engine (2), at least one triangular shackle aligned in the longitudinal direction (X) of the aircraft. Furthermore, the hanging equipment is made up exclusively of forward and rear attachments.Type: GrantFiled: November 23, 2004Date of Patent: October 17, 2006Assignee: Airbus FranceInventors: Stephane Machado, Jerome Cassagne, Anthony Del Blanco, Yvon Martin, Arnaud Chambreuil
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Publication number: 20060027705Abstract: This invention relates to a structure (1) for mounting an engine (2) under an aircraft wing (4), comprising a rigid structure (8) and means (10) of mounting this rigid structure under the wing, the mounting means (10) comprising a forward fastener (14) and an aft fastener (16). According to the invention, the forward fastener has at least one triangular shackle on each side of a vertical plane passing through a longitudinal axis (5) of the engine, placed in a vertical plane oriented along a direction inclined with respect to a longitudinal direction (X) and a transverse direction (Y) of the aircraft, and located in a horizontal plane defined by these directions (X) and (Y). Furthermore, the aft fastener comprises at least one shackle oriented along a vertical direction (Z) of the aircraft.Type: ApplicationFiled: November 24, 2004Publication date: February 9, 2006Applicant: Airbus FranceInventors: Stephane Machado, Jerome Cassagne, Anthony Del Blanco, Yvon Martin, Arnaud Chambreuil
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Publication number: 20050178889Abstract: This invention relates to a structure (1) for mounting a turboprop (2) under an aircraft wing (4), comprising a rigid structure and means (10) of fastening the turboprop on the rigid structure. According to the invention, the rigid structure is composed of a box (8), and the mounting means comprise at least two lateral connecting rods (26) resisting the engine torque generated by the turboprop, the connecting rods (26) being arranged on each side of the box and each having a forward end (26a) connected to a gear box (24) of the turboprop (2), and an aft end (26b) connected to said box.Type: ApplicationFiled: November 15, 2004Publication date: August 18, 2005Applicant: Airbus FranceInventors: Stephane Machado, Jerome Cassagne, Anthony Del Blanco, Yvon Martin, Arnaud Chambreuil
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Publication number: 20050178888Abstract: This invention relates to a mounting structure (1) for mounting an engine (2) under an aircraft wing (4), the structure comprising a rigid structure (8) and means (10) of fastening this rigid structure under the wing, the mounting means comprising a forward fastener (14), an intermediate fastener (15) and an aft fastener (16). According to the invention, the forward fastener has at least one triangular shackle on each side of a vertical plane passing through a longitudinal axis (5) of the engine (2), placed in a vertical plane oriented along a longitudinal direction (X) of the aircraft. Furthermore, the intermediate fastener comprises a connecting rod capable of transferring forces applied in a direction (Y) transverse to the aircraft, and the aft fastener comprises at least one shackle oriented along a vertical direction (Z) of the aircraft.Type: ApplicationFiled: November 15, 2004Publication date: August 18, 2005Applicant: Airbus FranceInventors: Stephane Machado, Jerome Cassagne, Anthony Del Blanco, Yvon Martin, Arnaud Chambreuil
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Publication number: 20050151008Abstract: The invention relates to a hanging device (1) connecting an engine (2) to a wing (4) of an aircraft, with the device being made up of a rigid structure (8) and hanging equipment (10) interposed between the rigid structure (8) and the wing (4), with the hanging equipment (10) being made up of a forward attachment (14) and a rear attachment (16) made up of at leas one triangular shackle placed in a vertical plane aligned in a transverse direction (Y) of the aircraft. According to the invention, the forward attachment (14) has, on one side and the other of a vertical plane passing through a longitudinal axis (5) of the engine (2), at least one triangular shackle aligned in the longitudinal direction (X) of the aircraft. Furthermore, the hanging equipment is made up exclusively of forward and rear attachments.Type: ApplicationFiled: November 23, 2004Publication date: July 14, 2005Applicant: Airbus FranceInventors: Stephane Machado, Jerome Cassagne, Anthony Del Blanco, Yvon Martin, Arnaud Chambreuil
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Publication number: 20050116093Abstract: This invention relates to a mounting structure (1) for mounting a turboprop (2) under an aircraft wing (4), the structure comprising a rigid structure (8) provided with an aft underwing box (10), and at least one forward rigid segment (12, 14), each forward rigid segment having two transverse frames (30, 32, 54) at a spacing from each other. According to the invention, at least one forward rigid segment (12, 14) of the rigid structure also comprises at least one forward upper box (34, 56) connecting a top part (30a, 32a, 54a) of the two transverse frames (30, 32, 54) of the forward rigid segment.Type: ApplicationFiled: November 15, 2004Publication date: June 2, 2005Applicant: Airbus FranceInventors: Stephane Machado, Jerome Cassagne, Anthony Del Blanco, Yvon Martin, Arnaud Chambreuil