- •Computing and schematic paper
- •Variant 1
- •1. Introduction
- •2. Short description of the design and operation of fuel system Tу-154 and its elements
- •3. Block diagram of the system
- •1 Tanks; 2 booster pumps; 3 - check valves; 4 - fire valve; 5 - coarse filtering device; 6 - low-pressure pump; 7 - a fine filter; 8 - fuel-regulating equipment; 9 -nozzles
- •4. Systematization and classification of specific functional failures and damage to the system and its components
- •5. Analysis of the efficiency of the fuel system of Tu-154 failures of its individual elements
- •5.1 Calculating the probability of failure-free operation of other elements, blocks and system
- •6. Structural improvement
- •7. Algorithm development for detection of problem with functional system of the aircraft
6. Structural improvement
Analysis of calculation of reliability indicators evaluation indicates that the lowest probability of non-failure work of system among the blocks has a block IV. Among the block units IV the lowest probability of non-failure work has a booster pump. The overall damage of this equipment are: overheating, failures in work, cavitation and other.
The activities, which are aimed at improving operating efficiency and reliability of the system may be:
additional cleaning the fuel;
changes in equipment design;
diagnostic tools development
O
ne
way to improve the reliability of the system is the installation of
additional pump ЭЦН-323
(Figure 5).
1IV , 2IV - booster pump; 3IV - fine filter; 3IV - relief valve fine filter;
Figure 5. Improvement of Block IV
Calculate the probability of Block IV improvements following formula:
PIVim= 1 – {[1- (P1IVP3IV)][1- (P2IVP4IV)]}=
=1-{[1-(0,99704438*0,99852109)][1-(0,99704438*0,99808184)]}=0,9999784
P (system)im = PI PII PIII PIVim PV= =0,9999967*0,99997955*0,999642*0,9999784*0,99744328=0,9970409
P(system)im> Psystem - probability of non-failure operation of system increased here follows that improvement takes place.
7. Algorithm development for detection of problem with functional system of the aircraft
For the cases in flight and during the ground engine testing of fuel supply the following algorithm is proposed, which is shown in Figure 6. The scheme includes all possible situations connected with the mentioned problem, and sequence of measures for solution taking into account priority of operating aggregates. Beginning of the algorithm is denoted by “S” – “Start”, its ending with “F” – “Finish”. Graph is to be read upside-down following the denotations which correspond to the occurred situation.
Figure 6 Algorithm for determining the damage
Conclusion
During the work of a course project was the analysis of failure of the fuel system of the Ty-154. Turned a least reliable unit IV, namely block element - pump. The main failures of this element are: overheating, refusal to work, work in cavitation conditions. To improve the reliability of the system was suggested to install an additional pump. Calculations show that after the installation of additional pump the probability of non-failure system operation increased.
Reference
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Новіков І.М., Тугарiнов О.С., Докучаев В.Г. Експлуатація авіаційної техніки. Методичні вказівки по виконанню курсової роботи. – К.: НАУ, 2003.-44с.
СМИРНОВ Н.Н., ИЦКОВИЧ А.А. Обслуживание и ремонт авиационной техники по состоянию. – М.: Транспорт, 1987. – 272 с.
ДМИТРІЄВ С.О., ТУГАРІНОВ О.С., ДОКУЧАЄВ В.Г., ЧОХА Ю.М. Технічне обслуговування планера і функціональних систем ПС та АД: Навч. посібник. – К.: НАУ, 2003, 250 с.
