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A Method for Determining Control Law of Afterburner Total Fuel Flow

A technology of fuel flow and control law, which is applied in the direction of fuel control of turbine/propulsion device, turbine/propulsion fuel delivery system, charging system, etc., and can solve the problems of poor applicability in non-standard days

Active Publication Date: 2021-10-01
AECC SHENYANG ENGINE RES INST
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0009] In order to solve at least one of the above technical problems, this application provides a method for determining the total fuel flow control law of afterburner, which solves the problem of poor applicability in non-standard days existing in the existing control laws, improves the performance of the engine on non-standard days, and improves engine operating safety, the method comprising:

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  • A Method for Determining Control Law of Afterburner Total Fuel Flow
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  • A Method for Determining Control Law of Afterburner Total Fuel Flow

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[0034] In order to make the objectives, technical solutions and advantages of the implementation of the application clearer, the technical solutions in the implementation modes of the application will be described in more detail below with reference to the drawings in the implementation modes of the application. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the present application. The embodiments described below by referring to the figures are exemplary and are intended to explain the present application, and should not be construed as limiting the present application. Based on the implementation manners in this application, all other implementation manners obtained by persons of ordinary skill in the art without creative efforts fall within the scope of protection of this application. Embodiments of the pr...

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Abstract

The application belongs to the technical field of aero-engine state detection, and in particular relates to a method for determining the law of total afterburner fuel flow control. The method includes calculating the performance of the full afterburner state, obtaining different engine inlet total temperature deviations and afterburner oil-gas ratios under different engine inlet total temperatures; obtaining the aircraft altitude and calculating the corresponding ambient temperature under standard atmospheric conditions; obtaining Calculate the Mach number of the aircraft and calculate the corresponding total temperature of the inlet inlet; determine the total temperature deviation of the engine inlet; interpolate and calculate the fuel-air ratio of the afterburner, so as to obtain the total fuel flow control law of the afterburner. This application considers the non-standard weather conditions The afterburner total fuel flow control law can effectively solve the problem of poor applicability in non-standard weather conditions existing in the existing rules, and can effectively improve the performance and work safety of the engine in non-standard days.

Description

technical field [0001] The application belongs to the technical field of aero-engine fuel control, and in particular relates to a method for determining the law of total afterburner fuel flow control. Background technique [0002] Afterburner total fuel flow control law generally refers to, according to the engine inlet total temperature T t2 , formulate the corresponding oil-gas ratio W fab / P t3 . [0003] With the development of aviation science and technology, military aircraft are required to have the ability to fly at a sudden increase in flight speed when taking off, climbing or performing interception tasks, and gas turbine engines with afterburners have emerged as the times require. Fuel is supplied to the afterburner by the afterburner fuel control system, and the fuel is mixed with the oxygen contained in the turbine and the outlet airflow of the outer culvert again to achieve the purpose of further increasing the engine thrust. At present, the general design ...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F02C9/28
CPCF02C9/28
Inventor 袁继来姜繁生张志成陈泽华张志舒
Owner AECC SHENYANG ENGINE RES INST