Double corrector for asymmetrical mechanism compensation

A corrector, asymmetric technology, applied in the direction of controllers, instruments, machinery, etc. with specific characteristics, which can solve the requirements of meeting overflow, cannot allow slow behavior, rapidity, servo control solutions cannot allow meeting specifications, etc. question

Pending Publication Date: 2021-08-10
SAFRAN AIRCRAFT ENGINES SAS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0027] This obviously creates a regulation problem: homogeneous behavior with local loops and therefore homogeneous behavior with full regulation
[0028] A "slow" corrector synthesized by taking into account the "fast" transfer function will not allow to meet the requirements regarding the rapidity of the slow behavior of the system during negative control changes
[0029] Conversely, a "fast" corrector synthesized by taking into account the "slow" behavior will not allow satisfying the requirements regarding the spillover aspects of the fast behavior of the system during positive control changes
[0030] Therefore, in terms of both speed and overflow, conventional servo control solutions do not allow to meet the specifications

Method used

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  • Double corrector for asymmetrical mechanism compensation
  • Double corrector for asymmetrical mechanism compensation

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Embodiment Construction

[0050] Now, a specific implementation of this solution will be described. The solution is again explained in conjunction with the three-way valve described in the introduction. The "Situational Modeling" context described in section is considered.

[0051] will refer to figure 1 and figure 2 The control system 1 and the control method are described.

[0052] The control system includes a valve 10 such as a three-way valve (channel one, channel two and channel three) and a calculator 20 . Advantageously, a sensor 30 is provided to measure the position of the valve 10 . Define three positions P1, P2 and P3 for the three-way valve 10:

[0053] - In position P1 (called stop position), channel three (exit channel) is connected to channel one (oil from the exchanger),

[0054] - In position P2 (also called stop position), channel three is connected to channel two (uncooled oil),

[0055] - In position P3, channel three is connected to the other two channels (this position ac...

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PUM

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Abstract

The invention concerns a method for controlling a mechanism (10) displaying asymmetrical behaviour, the mechanism (10) comprising a first operating direction (F+) and a second operating direction (F-), the control method making it possible to generate, using a control module (24) of a computer (20), a control signal (x_com) from a setpoint signal (x_cons), in which - when the setpoint signal (x_cons) indicates that the mechanism (10) should be operated in the first direction (F+), the control module (24) applies a first corrector (100) to the setpoint signal (x_cons) in order to generate a control signal (x_com), - when the setpoint signal (x_cons) indicates that the mechanism (10) should be operated in the second direction (F-), the control module (24) applies a second corrector (100) to the setpoint signal (x_cons) in order to generate a control signal (x_com), and in which the first and second correctors (100, 200) have different parameters (Kp1, Kp2, Ti1, Ti2), in order to compensate for the asymmetrical behaviour of the mechanism (10).

Description

technical field [0001] The invention relates to electronic valve regulation, in particular to control checks of valves. [0002] The invention finds particular application in aircraft turbines, such as open rotors. [0003] The invention will be described in this context, but is applicable to any mechanism with undesired or unintended functional asymmetry. Background technique [0004] A statement of the prior art and the problem identified by the applicant [0005] An open rotor is an aircraft engine whose structure consists of a gas generator and a propulsion unit equipped with a power turbine, a propeller gearbox (PGB) and a pair of unducted counter-rotating variable pitch propellers. [0006] Delivering very high torque to the propeller results in high heat rejection which can damage PGBs and other equipment designed to operate within certain restricted temperature ranges. [0007] The PGB is both oil cooled and oil lubricated. To obtain the desired temperature, a th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F15B5/00G05B11/42G05B19/44
CPCG05B19/44G05B11/42G05B2219/41143G05B2219/41154F15B13/02F16H57/0413
Inventor 克里斯多夫·马克·亚历山大·勒布伦塞巴斯蒂安·吉恩·费尔南德·德诺芙
Owner SAFRAN AIRCRAFT ENGINES SAS
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