ROTATION FITTING FOR THE EMPENNAGE OF AN AIRCRAFT

Rotation fitting secured to a frame (6) of the fuselage of an aircraft and linked to a receiving element secured to the empennage (5) which comprises a central fitting (1) and two side fittings (2,3), the central fitting (1) presenting two lugs (1d,1k) with an opening (1e,1j) each and four side wing...

Full description

Saved in:
Bibliographic Details
Main Author GARCIA SACRISTAN, ANGEL
Format Patent
LanguageEnglish
French
Published 26.06.2007
Subjects
AEROPLANES
AIRCRAFT
AVIATION
BEARINGS
BLASTING
COSMONAUTICS
ELEMENTS OR CRANKSHAFT MECHANISMS
ENGINEERING ELEMENTS AND UNITS
FLEXIBLE SHAFTS
GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS
HEATING
HELICOPTERS
LIGHTING
MECHANICAL ENGINEERING
PERFORMING OPERATIONS
ROTARY BODIES OTHER THAN GEARING ELEMENTS
SHAFTS
THERMAL INSULATION IN GENERAL
TRANSPORTING
WEAPONS
Online AccessGet full text

Cover

More Information
Summary:Rotation fitting secured to a frame (6) of the fuselage of an aircraft and linked to a receiving element secured to the empennage (5) which comprises a central fitting (1) and two side fittings (2,3), the central fitting (1) presenting two lugs (1d,1k) with an opening (1e,1j) each and four side wings (1g, 1f, 1i, 1h), a nd each one of the side fittings (2,3) presenting a lug (2d,3d) with an opening (2e,3e) each and two side wings (2g,2f,3g,3f), the central fitting (1) being secured to a surface of the frame (6) and the side fittings (2,3) in an opposite surface of the frame (6), such that the frame (6) is arranged between the central fitting ( 1) and the two side fittings (2,3), such that the lugs (1d,1k) of the central fitti ng (1) make contact with the lugs (2d,3d) of the side fittings, with all the openin gs (1e,1j,2e,3e) being aligned in order to house a pin (4) associated with the receiving element secured to the empennage (5).
Bibliography:Application Number: CA20062555548