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Development of portioned providing equable output and support of the mass of fuel center in a specific range

Hossein Nadjari   (Postgrad. (PhD) Student, assistant, Samara University)

Hossein SafaaMuhammad RidhaHossein  (Postgrad. (PhD) Student, Samara University; Teacher, University of Karbala, Karbala, Iraq)

Hanfar Adam   (Postgrad. (PhD) Student, Samara University)

Ossiala Venceslas BelAmour  (Postgrad. (PhD) Student, Samara University)

Matveichuk Irina Alekseevna  (Postgrad. (PhD) Student, Samara University)

At present time, there is a work package for creation and equipping civil aviation with new aircrafts and helicopters, which, according to their flight-technical and operational characteristics should provide a higher level of safety, regularity and intensity of flights compared to the existing level, aircraft fuel savings, reduction the cost of maintenance and repair, and cost of air transportation. But at the same time, the equipment currently being used is also being improved, which must also meet the increased requirements, both technical and economical

Keywords:Portioner; Fuel system; ESP; density; reliability; bearing
 

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Citation link:
Hossein N. , Hossein S. R., Hanfar A. , Ossiala V. B., Matveichuk I. A. Development of portioned providing equable output and support of the mass of fuel center in a specific range // Современная наука: актуальные проблемы теории и практики. Серия: Естественные и Технические Науки. -2019. -№06-2. -С. 102-108
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