Aircraft Designing and Manufacturing

Zinchenko A., Kumchenko I., Tarabanova V.

ANDREYI A. ZINCHENKO, Head, Structural Analysis Bureau, e-mail: ediablo@mail.ru 
IVAN I. KUMCHENKO, Process Engineer, e-mail: ediablo@mail.ru 
VERA V. TARABANOVA, Maintenance Engineer, e-mail: ouriv@list.ru 
Arsenyev Airscraft Company Progress
5 Lenin Square, Arsenyev, Primorski Region, Russia 692335

The article deals with the authors’ automated system of automatic control over the weight of the aircraft assemblies which substantially simplifies the technological processes of their manufacturing. The advantages of the innovation and the algorithm of its exploitation in a serial production enterprise are presented in it.
Key words: automation, centre of mass, construction of minimum weight, control of mass, software, aircraft.

REFERENCES

1. Industry Standard OST 1 02562-85. Planes and helicopters. General requirements for the measurement of mass and center of gravity determination. (in Russ.). [Otraslevoy standart OST 1 02562-85. Samoletu I vertoletu. Obshie trebovaniy k izmereniu massi i opredeleniy pologeniy zentra massu].
2. Industry Standard OST 1 02606-86. Planes and helicopters. Control weight parts, assemblies and finished products in the mass production. (in Russ.). [Otraslevoy standart OST 1 02606-86. Samoletu I vertoletu. Kontrol massu detaley, sborochnuh edeniz i pokupnuh izdeliy v seriynom proizvodstve]. 
3. Guiding technical materials TsAGI. Automated system for weight control. 1976 (in Russ.). [Rukovodyshie tehnicheskie materiali ZAGI. Avtomanizirovannay sistema vesovogo kontroly, 1976 g.].
4. Standard Control Organization STO 690-2013. Weight parts, subassemblies and purchased products. (in Russ.). [Standart organizazii STO 690-2013. Kontrol massi detaley, sborochnih ediniz I pokupnih izdeliy].