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公开(公告)号:WO2022245798A1
公开(公告)日:2022-11-24
申请号:PCT/US2022/029594
申请日:2022-05-17
Applicant: BETA AIR, LLC
Inventor: AUERBACH, Joshua E. , GIROUX, Andrew , TOWNSEND, Chris , RICHTER, Timothy Gerard , SHEPPARD, Matthew John
Abstract: An aircraft for fixed pitch lift includes a fuselage, a plurality of flight components attached to the fuselage, wherein the plurality of flight components further comprises at least a lift propulsor component, wherein the lift propulsor component comprises a plurality of blades configured at a fixed angle of attack, and a pusher component, wherein the pusher component is configured to produce a forward thrust.
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2.
公开(公告)号:WO2022212247A1
公开(公告)日:2022-10-06
申请号:PCT/US2022/022127
申请日:2022-03-28
Applicant: BETA AIR, LLC
Inventor: TOWNSEND, Chris , AUERBACH, Joshua E. , GIROUX, Andrew
IPC: B64C13/04 , B64C13/50 , G05D1/00 , B64C9/00 , G06N20/00 , B64C13/503 , B64C2009/005 , B64C29/0025 , G05D1/0077 , G05D1/0088 , G06N3/0454 , G06N5/003 , G06N7/005
Abstract: In an aspect a system for fly-by-wire flight control configured for use in electric aircraft includes at least a sensor, wherein the sensor is communicatively connected a pilot control and configured to detect a pilot input from the pilot control and generate, as a function of the pilot input, command datum. A system includes a flight controller, the flight controller including a computing device and configured to perform a voting algorithm, wherein performing the voting algorithm includes determining that the sensor is an allowed sensor, wherein determining that the sensor is an allowed sensor includes determining that the command datum is an active datum, determining the command datum is an admissible datum, generating, as a function of the command datum and the allowed sensor, a control surface datum wherein the control surface datum is correlated to the pilot input.
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