Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Józef Brzęczek"'
Publikováno v:
Advances in Sciences and Technology, Vol 10, Iss 31, Pp 109-118 (2016)
This article presents selected criteria for the quality assessment of single-lap adhesive joints formed on 0.66±0.04 thick hot dip zinc coated sheets with the hot dip zinc coating thickness equal to 18 µm. Three types of epoxy adhesives and three v
Externí odkaz:
https://doaj.org/article/227120f8d592477a8fd4d3e9ee5345cb
Autor:
Józef Brzęczek
Publikováno v:
Fatigue of Aircraft Structures. 2020:102-112
Cable control systems are widely used in aircraft and gliders. This paper deals with the problem of collecting real loads acting cable control systems and cable tests preparation (load spectrum) and performance. The author proposes a method for defin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d2f22abac57fc98f301a8407c4196cc5
https://doi.org/10.2478/fas-2020-0010
https://doi.org/10.2478/fas-2020-0010
Autor:
Józef Brzęczek
Publikováno v:
Advances in Science and Technology Research Journal, Vol 13, Iss 2, Pp 65-71 (2019)
Cable control systems are widely used in GA aircrafts and gliders. The paper deals with the accuracy of measurement the tension of cables on the production stage and maintenance of aeronautical products. Producers of measuring instruments used to mea
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::837a6b75020f7f0b222cc5286bf41116
http://www.journalssystem.com/astrj/Examination-of-aircraft-s-cable-control-systems-tension-,106238,0,2.html
http://www.journalssystem.com/astrj/Examination-of-aircraft-s-cable-control-systems-tension-,106238,0,2.html
Autor:
Janusz Pietruszka, Henryk Gruszecki, Jerzy Chodur, Józef Brzęczek, Leszek Pieróg, Mariusz Kubryn
Publikováno v:
Fatigue of Aircraft Structures. 2018:53-62
The cable flight control systems are commonly used for the control of small airplanes. In these systems, the cables are the only elements transmitting loads from the pilot to the control surfaces. During a flight the cables are moving through pulleys
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::759f2de0c63c8b8eb85854ca9f69065f
https://doi.org/10.2478/fas-2018-0005
https://doi.org/10.2478/fas-2018-0005
Autor:
Józef Brzęczek
Publikováno v:
Eksploatacja i Niezawodnosc - Maintenance and Reliability. 19:597-603
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b93804d6e892ffb834d44203a417fef8
https://doi.org/10.17531/ein.2017.4.14
https://doi.org/10.17531/ein.2017.4.14
Publikováno v:
Advances in Science and Technology Research Journal, Vol 10, Iss 31, Pp 109-118 (2016)
This article presents selected criteria for the quality assessment of single-lap adhesive joints formed on 0.66±0.04 thick hot dip zinc coated sheets with the hot dip zinc coating thickness equal to 18 µm. Three types of epoxy adhesives and three v
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::63a82611b7f3ef073fbf580a6899e413
http://www.journalssystem.com/astrj/THE-VISUAL-METHOD-IN-QUALITY-ASSESSMENT-OF-SINGLE-LAP-ADHESIVE-JOINTS,64066,0,2.html
http://www.journalssystem.com/astrj/THE-VISUAL-METHOD-IN-QUALITY-ASSESSMENT-OF-SINGLE-LAP-ADHESIVE-JOINTS,64066,0,2.html
Publikováno v:
Fatigue of Aircraft Structures. 2014:102-106
Service life of the PZL M28 is computed based on the results of the full-scale fatigue tests of the structure [1]. As the PZL M28 is a commuter category airplane according to the 14 CFR Part 23 and CS-23 regulations, the test objects are: (1) wing an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fbd8b3750b3f285de88211da61a68daf
https://doi.org/10.1515/fas-2014-0010
https://doi.org/10.1515/fas-2014-0010
Publikováno v:
Fatigue of Aircraft Structures. 2014:107-112
The PZL M28’s service life is determined based on the fatigue tests of the wing and wing loads-carry-through structure. During the fatigue test, the first occurrence of significance was the appearance of a in the area of the wing where loads are ap
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a0bb4e2cd54d43a532248f2e271a363b
https://doi.org/10.1515/fas-2014-0011
https://doi.org/10.1515/fas-2014-0011
Publikováno v:
Fatigue of Aircraft Structures. 2014:88-94
Service life of the PZL M28 is computed based on the results of the full-scale fatigue tests of the structure [1]. As the PZL M28 is a commuter category airplane according to the 14 CFR Part 23 and CS-23 regulations, the test objects were: (1) wing a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5c07a6b9f503cfea179c0d04b5399241
https://doi.org/10.1515/fas-2014-0008
https://doi.org/10.1515/fas-2014-0008
Publikováno v:
Fatigue of Aircraft Structures. 2014:95-101
The basis for the computation of the service life of the PZL M28 was the results of the full-scale fatigue tests of the structure [1]. As the PZL M28 is a commuter category airplane according to the 14 CFR Part 23 and CS-23 regulations, the test obje
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ee19442c9333e18ac2a98de6c71c2696
https://doi.org/10.1515/fas-2014-0009
https://doi.org/10.1515/fas-2014-0009