Detail publikace

EXPERIMENTAL TIGHTENING MOMENT DETERMINATION OF FRICTION JOINT

JURAČKA, J.

Anglický název

EXPERIMENTAL TIGHTENING MOMENT DETERMINATION OF FRICTION JOINT

Typ

Stať ve sborníku v databázi WoS či Scopus

Jazyk

en

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 anglicky

TIGHTENING MOMEN

Vydáno

2003-05-10

Nakladatel

University of Bologna

Místo

Milano Marittima

ISBN

88-901080-0-2

Kniha

Extended Summaries

Strany od–do

85–

Počet stran

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"
}