- Patent Title: Compound helicopter with braced wings in joined-wing configuration
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Application No.: US17350609Application Date: 2021-06-17
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Publication No.: US11999469B2Publication Date: 2024-06-04
- Inventor: Axel Fink , Pierre Pardoux , Dominique Mailliu
- Applicant: AIRBUS HELICOPTERS DEUTSCHLAND GMBH , AIRBUS HELICOPTERS
- Applicant Address: DE Donauworth
- Assignee: AIRBUS HELICOPTERS DEUTSCHLAND GmbH,AIRBUS HELICOPTERS
- Current Assignee: AIRBUS HELICOPTERS DEUTSCHLAND GmbH,AIRBUS HELICOPTERS
- Current Assignee Address: DE Donauworth; FR Marignane
- Agency: Brooks Kushman P.C.
- Priority: EP 400023 2020.12.02
- Main IPC: B64C27/26
- IPC: B64C27/26 ; B64C39/06 ; B64D25/18

Abstract:
A compound helicopter with braced wings in joined-wing configuration, a fuselage that extends from a front fuselage section to a rear fuselage section, and an emergency floatation system with main floatation balloons and lateral floatation wherein balloons, the main floatation balloons comprise at least one front floatation balloon that is arranged in the front fuselage section and at least one rear floatation balloon that is arranged in the rear fuselage section, and wherein the lateral floatation balloons comprise at least one first lateral floatation balloon that is arranged close to an interconnection region of the first braced wing and at least one second lateral floatation balloon that is arranged close to an interconnection region of the second braced wing.
Public/Granted literature
- US20220169372A1 COMPOUND HELICOPTER WITH BRACED WINGS IN JOINED-WING CONFIGURATION Public/Granted day:2022-06-02
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