Electric power generation controller for use in aircraft and electric power generating apparatus including same

US11465767B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11465767-B2
Application numberUS-201817294003-A
CountryUS
Kind codeB2
Filing dateNov 19, 2018
Priority dateNov 19, 2018
Publication dateOct 11, 2022
Grant dateOct 11, 2022

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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Abstract

Official abstract text for this publication.

An electric power generation controller for use in an aircraft is a controller of an electric power generating apparatus including a manual transmission configured to change speed of rotational power of an aircraft engine, transmit the rotational power to an electric power generator, and switch a gear stage by a friction clutch pressed by an actuator. The electric power generation controller includes a manual transmission control section configured to control the manual transmission. The manual transmission control section includes: a shift command section configured to output a shift signal which switches the gear stage of the manual transmission; and a clutch control section configured to, when switching the gear stage of the manual transmission, control clutch pressure of the actuator such that the friction clutch becomes a half-engaged state.

First claim

Opening claim text (preview).

The invention claimed is: 1. An electric power generation controller for use in an aircraft, the electric power generation controller being a controller of an electric power generating apparatus including a manual transmission configured to change speed of rotational power of an aircraft engine, transmit the rotational power to an electric power generator, and switch a gear stage by a friction clutch pressed by an actuator, the electric power generation controller comprising a manual transmission control section configured to control the manual transmission, wherein the manual transmission control section includes a shift command section configured to output a shift signal which switches the gear stage of the manual transmission and a clutch control section configured to, when switching the gear stage of the manual transmission, control clutch pressure of the actuator such that the friction clutch becomes a half-engaged state, wherein: the manual transmission control section further includes an electric power generation load receiving section configured to receive an electric power generation load of the electric power generator; and when the friction clutch is in the half-engaged state, the clutch control section controls the actuator such that clutch pressure of the friction clutch increases as the electric power generation load increases. 2. The electric power generation controller according to claim 1 , wherein: a continuously variable transmission is interposed on a power transmission path between the manual transmission and the electric power generator; and the electric power generation controller further comprises a continuously variable transmission control section configured to control the continuously variable transmission based on an input rotational frequency of the continuously variable transmission such that the rotational frequency input to the electric power generator becomes constant. 3. The electric power generation controller according to claim 1 , wherein: when the friction clutch is in a first state that is one of an engaged state or a disengaged state, the manual transmission is set to a first gear stage; when the friction clutch is in a second state that is the other of the engaged state and the disengaged state, the manual transmission is set to a second gear stage; the shift signal is a shift-down signal which decreases a change gear ratio or a shift-up signal which increases the change gear ratio; when switching the gear stage of the manual transmission such that the change gear ratio decreases, the clutch control section controls the clutch pressure of the actuator such that the friction clutch becomes the half-engaged state, and then, controls the clutch pressure of the actuator such that the friction clutch becomes the second state; and when switching the gear stage of the manual transmission such that the change gear ratio increases, the clutch control section controls the clutch pressure of the actuator such that the friction clutch becomes the half-engaged state, and then, controls the clutch pressure of the actuator such that the friction clutch becomes the first state. 4. An electric power generating apparatus for use in an aircraft, the electric power generating apparatus comprising: the electric power generation controller according to claim 1 ; a manual transmission configured to change speed of rotational power of an aircraft engine and including a plurality of gear stages; and an electric power generator configured to transmit power which has been changed in speed by the manual transmission. 5. An electric power generation controller for use in an aircraft, the electric power generation controller being a controller of an electric power generating apparatus including a manual transmission configured to change speed of rotational power of an aircraft engine, transmit the rotational power to an electric power generator, and switch a gear stage by a friction clutch pressed by an actuator, the electric power generation controller comprising a manual transmission control section configured to control the manual transmission; and a rotational frequency receiving section configured to receive an output-side rotational frequency of the manual transmission, wherein: the manual transmission control section includes a shift command section configured to output a shift signal which switches the gear stage of the manual transmission and a clutch control section configured to, when switching the gear stage of the manual transmission, control clutch pressure of the actuator such that the friction clutch becomes a half-engaged state, wherein: when the friction clutch is in the half-engaged state, the clutch control section controls the actuator such that clutch pressure of the friction clutch increases as the output-side rotational frequency of the manual transmission decreases.

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What does patent US11465767B2 cover?
An electric power generation controller for use in an aircraft is a controller of an electric power generating apparatus including a manual transmission configured to change speed of rotational power of an aircraft engine, transmit the rotational power to an electric power generator, and switch a gear stage by a friction clutch pressed by an actuator. The electric power generation controller in…
Who is the assignee on this patent?
Kawasaki Heavy Ind Ltd
What technology area does this patent fall under?
Primary CPC classification F02C7/32. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Oct 11 2022 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).