Torque balancing for hybrid electric propulsion systems and aircraft utilizing hybrid electric propulsion systems
Number of patents in Portfolio can not be more than 2000
United States of America
Stats
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Mar 4, 2025
Grant Date -
Sep 3, 2020
app pub date -
Dec 6, 2019
filing date -
Dec 6, 2019
priority date (Note) -
In Force
status (Latency Note)
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Abstract
A hybrid electric engine control module (ECU) configured to be operatively connected to a hybrid electric aircraft powerplant having a heat engine system and an electric motor system to control a torque output from each of the heat engine system and the electric motor system. The ECU can be configured to receive a torque command and split output power between the electric motor system and the heat engine system. Additionally and/or alternatively, the ECU can be configured to balance a total torque against a second total torque of a second aircraft powerplant.
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International Classification(s)
- 2019 Application Filing Year
- B60W Class
- 4319 Applications Filed
- 3019 Patents Issued To-Date
- 69.91 % Issued To-Date
Cited Art Landscape
Patent Citation Ranking
- 0 Citation Count
- B60W Class
- 0 % this patent is cited more than
- < 1 Age
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