Detail publikace

EXPERIMENTAL TIGHTENING MOMENT DETERMINATION OF FRICTION JOINT

JURAČKA, J.

Originální název

EXPERIMENTAL TIGHTENING MOMENT DETERMINATION OF FRICTION JOINT

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

angličtina

Originální abstrakt

The Institute of Aerospace Engineering in its own aircraft test laboratory, authorised by the Czech Civil Aviation Authorities, ran the static and fatigue tests of the Ae 270 Ibis aircraft engine mount. In the frame of these tests, we determined the tightening moment for pre-stressed bolt connection. This connection is usually not used in Czech aircraft industry. The share forces are more frequently trans loaded through the shear pin. The tightening moment measurement was done for calculation confirmations. During the measurement the influence of lubrications appeared.

Klíčová slova

TIGHTENING MOMEN

Autoři

JURAČKA, J.

Rok RIV

2003

Vydáno

10. 5. 2003

Nakladatel

University of Bologna

Místo

Milano Marittima

ISBN

88-901080-0-2

Kniha

Extended Summaries

Edice

NEUVEDENO

Číslo edice

NEUVEDENO

Strany od

85

Strany do

86

Strany počet

2

BibTex

@inproceedings{BUT7279,
  author="Jaroslav {Juračka}",
  title="EXPERIMENTAL TIGHTENING MOMENT DETERMINATION OF FRICTION JOINT",
  booktitle="Extended Summaries",
  year="2003",
  pages="2",
  publisher="University of Bologna",
  address="Milano Marittima",
  isbn="88-901080-0-2"
}