Back-up control method and apparatus for turbo machine
AssigneePratt & Whitney Canada Corp.
InventorsAlexandre Jay, Jim Robert Jarvo, Daniel Claude Gratton
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Abstract
A method and apparatus for controlling a turbo-machine in case of failure of the main burn fuel flow calculator. The apparatus receives at least information from various sensors as well as from the main burn fuel flow calculator. The method and apparatus, herein disclosed, provides a smooth and secure transition between the last burn fuel flow value before the failure of the main burn fuel flow calculator and the future burn fuel flow values.
Claims3
A method for determining a burn fuel flow value, comprising the steps of:
- receiving a current fuel flaw value provided to a fuel metering unit of a turbo-machine from a main burn fuel flow calculator;
- storing said current fuel flow value in a memory upon detection of a malfunction of said main burn fuel flow calculator;
- calculating a transitional value using said stored fuel flow value and a back-up burn fuel flow value received from a back-up burn fuel flow calculator;
- and
- outputting said transitional value to said fuel metering unit.
A method for determining a burn fuel flow valve for an aircraft turbo-machine in case of a malfunction, said method comprising the steps of:
- receiving a current fuel flow value from a main burn fuel flow calculator;
- storing said current fuel flow value prior to said malfunction;
- calculating a back-up burn fuel flow value using sensor readings form said aircraft and initially said stored current fuel flow value, wherein said calculating using an algorithm which is different from an algorithm used for calculating said main burn fuel value, said back-up burn fuel flow value having a smooth transition between said current fuel flow value prior to said malfunction and future burn fuel flow values;
- and
- outputting said back-up burn fuel flow value to a fuel metering unit.
Dependencies are inferred from the claim text.