Publication detail

EXPERIMENTAL TIGHTENING MOMENT DETERMINATION OF FRICTION JOINT

JURAČKA, J.

Original Title

EXPERIMENTAL TIGHTENING MOMENT DETERMINATION OF FRICTION JOINT

Type

conference paper

Language

English

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

TIGHTENING MOMEN

Authors

JURAČKA, J.

RIV year

2003

Released

10. 5. 2003

Publisher

University of Bologna

Location

Milano Marittima

ISBN

88-901080-0-2

Book

Extended Summaries

Edition

NEUVEDENO

Edition number

NEUVEDENO

Pages from

85

Pages to

86

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"
}