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Three Channel Fuel Flow Rate Digital Simulator.

Abstract: Three Channel Fuel Flow Rate Digital Simulator is designed for verification of correctness of fuel flow rate and quantity of fuel metering system of an aircraft using three channels Fuel Flow Rate Digital simulator. This method is required for carrying out following parameters/system: Testing of Fuel Metering System during Pre-installation Check Testing of Flow meter block and Electronic PCB Snag identification & analysis of fuel metering system on aircraft during ground check. ~~"'->""...,17~~-=-= 1/lYhjl(' . '.2\'i . ..(,..Jt# r71 f'"--;c•.''""#~ = , The apparatus is designecF·to~ geriel':ate -the same pulses which simulate the pulses as generated by flow rate in aircraft transducers in the fuelling line and engine feed lines of the aircraft wheri the aircraft fuel is flowing inside the pipelines of the aircraft. The apparatus incorporates three different channels together acts as single setup and same can also be used in different combination of channels selection.

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Patent Information

Application #
Filing Date
30 September 2022
Publication Number
14/2024
Publication Type
INA
Invention Field
MECHANICAL ENGINEERING
Status
Email
Parent Application

Applicants

HINDUSTAN AERONAUTICS LIMITED
INDUSTAN AERONAUTICS LIMITED INDIRA NAGAR LUCKNOW UTTAR PRADESH-226016, INDIA

Inventors

1. MR. HEERA LAL MAURYA
INDUSTAN AERONAUTICS LIMITED INDIRA NAGAR LUCKNOW UTTAR PRADESH-226016, INDIA

Specification

Documents

Application Documents

# Name Date
1 202211056111-Form-5-300922.pdf 2022-10-25
2 202211056111-Form-3-300922.pdf 2022-10-25
3 202211056111-Form-2-300922.pdf 2022-10-25
4 202211056111-Form-1-300922.pdf 2022-10-25