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Patent Agency Ranking
公开(公告)号：US11981460B2
公开(公告)日：2024-05-14
申请号：US18510592
申请日：2023-11-15
Applicant: Firestorm Labs, Inc.
Inventor： Ian Muceus , Daniel Magy
CPC classification number: B64U10/70 , B64U20/75 , B64U20/87 , B64U2201/104
Abstract: Disclosed are devices, systems and methods for mission-adaptable aerial vehicle. In some aspects, a mission-adaptable aerial vehicle includes a configuration having swappable, manipulatable, and interchangeable sections and components connectable by a connection and fastening system able to be modified by an end-user in the field. In some embodiments, a mission-adaptable aerial vehicle can be configured to include a main center body extending along a longitudinal direction, a wing with a lateral cross-sectional airfoil shape, and/or stabilizer and control surface structures with corresponding cross-sectional airfoil shapes.
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公开(公告)号：US12139280B2
公开(公告)日：2024-11-12
申请号：US18655221
申请日：2024-05-03
Applicant: Firestorm Labs, Inc.
Inventor： Ian Muceus , Daniel Magy
Abstract: Disclosed are devices, systems and methods for mission-adaptable aerial vehicle. In some aspects, a mission-adaptable aerial vehicle includes a configuration having swappable, manipulatable, and interchangeable sections and components connectable by a connection and fastening system able to be modified by an end-user in the field. In some embodiments, a mission-adaptable aerial vehicle can be configured to include a main center body extending along a longitudinal direction, a wing with a lateral cross-sectional airfoil shape, and/or stabilizer and control surface structures with corresponding cross-sectional airfoil shapes.
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公开(公告)号：US20240294279A1
公开(公告)日：2024-09-05
申请号：US18655221
申请日：2024-05-03
Applicant: Firestorm Labs, Inc.
Inventor： Ian Muceus , Daniel Magy
CPC classification number: B64U10/70 , B64U20/75 , B64U20/87 , B64U2201/104
Abstract: Disclosed are devices, systems and methods for mission-adaptable aerial vehicle. In some aspects, a mission-adaptable aerial vehicle includes a configuration having swappable, manipulatable, and interchangeable sections and components connectable by a connection and fastening system able to be modified by an end-user in the field. In some embodiments, a mission-adaptable aerial vehicle can be configured to include a main center body extending along a longitudinal direction, a wing with a lateral cross-sectional airfoil shape, and/or stabilizer and control surface structures with corresponding cross-sectional airfoil shapes.
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公开(公告)号：US20240092510A1
公开(公告)日：2024-03-21
申请号：US18510592
申请日：2023-11-15
Applicant: Firestorm Labs, Inc.
Inventor： Ian Muceus , Daniel Magy
CPC classification number: B64U10/70 , B64U20/75 , B64U20/87 , B64U2201/104
Abstract: Disclosed are devices, systems and methods for mission-adaptable aerial vehicle. In some aspects, a mission-adaptable aerial vehicle includes a configuration having swappable, manipulatable, and interchangeable sections and components connectable by a connection and fastening system able to be modified by an end-user in the field. In some embodiments, a mission-adaptable aerial vehicle can be configured to include a main center body extending along a longitudinal direction, a wing with a lateral cross-sectional airfoil shape, and/or stabilizer and control surface structures with corresponding cross-sectional airfoil shapes.
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公开(公告)号：US20250058904A1
公开(公告)日：2025-02-20
申请号：US18936906
申请日：2024-11-04
Applicant: Firestorm Labs, Inc.
Inventor： Ian Muceus , Daniel Magy
Abstract: Disclosed are devices, systems and methods for mission-adaptable aerial vehicle. In some aspects, a mission-adaptable aerial vehicle includes a configuration having swappable, manipulatable, and interchangeable sections and components connectable by a connection and fastening system able to be modified by an end-user in the field. In some embodiments, a mission-adaptable aerial vehicle can be configured to include a main center body extending along a longitudinal direction, a wing with a lateral cross-sectional airfoil shape, and/or stabilizer and control surface structures with corresponding cross-sectional airfoil shapes.
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