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公开(公告)号:US12012910B2
公开(公告)日:2024-06-18
申请号:US17873705
申请日:2022-07-26
Applicant: Textron Innovations, Inc.
Inventor: Patrick Henry Baer , Michael Glynn Glucksman
Abstract: An improved air-cooled aviation engine includes a compact combustion chamber having an intake valve opening, an exhaust valve opening, and a generally elliptical shape. The elliptical shape has a major axis and a minor axis, with the major axis intersecting both the intake valve opening and the exhaust valve opening. In some examples, the major axis is the same length or shorter than a diameter of a cylinder bore of the engine, and the minor axis is smaller than the major axis. Combustion is thus constrained to a smaller area than that of the cylinder bore.
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公开(公告)号:US20240337227A1
公开(公告)日:2024-10-10
申请号:US18745150
申请日:2024-06-17
Applicant: Textron Innovations Inc.
Inventor: Patrick Henry Baer , Michael Glynn Glucksman
Abstract: An improved air-cooled aviation engine includes a compact combustion chamber having an intake valve opening, an exhaust valve opening, and a generally elliptical shape. The elliptical shape has a major axis and a minor axis, with the major axis intersecting both the intake valve opening and the exhaust valve opening. In some examples, the major axis is the same length or shorter than a diameter of a cylinder bore of the engine, and the minor axis is smaller than the major axis. Combustion is thus constrained to a smaller area than that of the cylinder bore.
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