Publication detail

EXPERIMENTAL TIGHTENING MOMENT DETERMINATION OF FRICTION JOINT

JURAČKA, J.

English title

EXPERIMENTAL TIGHTENING MOMENT DETERMINATION OF FRICTION JOINT

Type

Paper in proceedings (conference paper)

Language

en

Original abstract

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.

Keywords in English

TIGHTENING MOMEN

Released

2003-05-10

Publisher

University of Bologna

Location

Milano Marittima

ISBN

88-901080-0-2

Book

Extended Summaries

Pages from–to

85–

Pages count

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"
}