Method for correcting cruise fuel consumption characteristics based on hovering test flight data

A technology of test flight data and characteristics, applied in the aviation field, can solve problems such as inability to accurately measure fuel consumption, inability to obtain multiple sets of test flight data, and unique aircraft weight.

Active Publication Date: 2020-09-25
CHENGDU AIRCRAFT INDUSTRY GROUP
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Problems solved by technology

However, the previous methods have the following deficiencies: 1. The flight action is instantaneous, considering the error of the fuel sensor, it is impossible to accurately measure the fuel consumption during the execution of the action; 2. When performing the flight action, the weight of the aircraft is unique and cannot Efficiently acquire multiple sets of flight test data in the same flight

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  • Method for correcting cruise fuel consumption characteristics based on hovering test flight data
  • Method for correcting cruise fuel consumption characteristics based on hovering test flight data
  • Method for correcting cruise fuel consumption characteristics based on hovering test flight data

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Embodiment 1

[0051] A method for correcting cruise fuel consumption characteristics based on circling flight test data, characterized in that: comprising the following steps:

[0052] a. Select the altitude point, select the speed point and select the flight state. Under the same altitude, speed and weight, calculate the hourly fuel consumption when hovering stably at different roll angles. Take n different roll angles (n is a variable) , the stable hovering time is 3 to 5 minutes), and the stable hovering is established to obtain different roll angles. The calculation formula for the hourly fuel consumption in this state under the same weight is as follows;

[0053]

[0054] Among them, W px is the hourly fuel consumption, △W px is the fuel consumption of circling, △ one is the time of circling;

[0055] b. Correction of fuel consumption characteristics, including stable hovering mechanics model and engine mechanics model;

[0056] The equations of the stable hovering mechanics mode...

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Abstract

The invention discloses a method for correcting cruise fuel consumption characteristics based on circling test flight data. The method comprises the following steps of: a, selecting a height point, aspeed point and a flight state, and calculating the hourly fuel consumption during stable circling at different roll angles; b, carrying out oil consumption characteristic correction; c, calculating the hourly oil consumption of the engine through the function relationship; e, correcting to the target weight, which comprises circling oil consumption calculation and level flight oil consumption calculation; correcting the oil consumption per hour to a target weight level flight state through the performance data; the method comprises the following steps: calculating the hourly oil consumption of an engine, the hourly oil consumption of the engine and the oil consumption in a level flight state during different rolling stable circling; the flight test data can be analyzed and calculated at different speeds, cost-reduced oil consumption data can be reliably and accurately measured, Meanwhile, multiple groups of effective flight test data can be obtained by selecting multiple groups of stable circling with different roll angles and changing the angle of the stable circling.

Description

technical field [0001] The invention belongs to the field of aviation technology, and in particular relates to a correction method for cruising fuel consumption characteristics based on circling flight test data. Background technique [0002] The fuel consumption characteristics of the aircraft cruising section have a very important impact on the aircraft's range and endurance performance, which is directly related to the accessibility of the aircraft's range and endurance performance indicators in the flight test. However, in the flight test stage, due to the constraints of the aircraft's production time , flight test cost constraints, and the number of flight sorties, the flight test data in the cruising segment is not enough to cover all the sample points of fuel consumption characteristics of the aircraft, resulting in a shortage of data in the analysis of fuel consumption characteristics, which affects the follow-up test flight plan and test flight progress. , in the fl...

Claims

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Application Information

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IPC IPC(8): G06F30/28G06F30/15
CPCG06F30/15G06F30/28G06F2119/14
Inventor 冯宇鹏程家林黄祥胡沛韩锐
Owner CHENGDU AIRCRAFT INDUSTRY GROUP
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