ANGULAR ADJUSTMENT COUPLING FOR CONNECTING TWO PIPES OF AN AIRCRAFT

ANGULAR ADJUSTMENT COUPLING FOR CONNECTING TWO PIPES OF AN AIRCRAFT

The invention refers to an angular adjustment coupling (1) for connecting two pipes (10a, 10b) of an aircraft (12), comprising at least two rings (2) having a ramp cross-section to provide thinner and wider sides (2', 2"), and at least three clamps (3), one clamp (3) disposed between the t...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser: LENOIR, Brice Bernard Michel
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
BLASTING
COSMONAUTICS
ENGINEERING ELEMENTS AND UNITS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS
HEATING
JOINTS OR FITTINGS FOR PIPES
LIGHTING
MEANS FOR THERMAL INSULATION IN GENERAL
MECHANICAL ENGINEERING
PARACHUTES
PERFORMING OPERATIONS
PIPES
SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING
THERMAL INSULATION IN GENERAL
TRANSPORTING
WEAPONS
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Beschreibung
Zusammenfassung:The invention refers to an angular adjustment coupling (1) for connecting two pipes (10a, 10b) of an aircraft (12), comprising at least two rings (2) having a ramp cross-section to provide thinner and wider sides (2', 2"), and at least three clamps (3), one clamp (3) disposed between the two rings (2) to fasten one to another at a selectable angular position, and the other two clamps (3) to be disposed between each one of the rings (2) and the pipes (10a, 10b), wherein the two rings (2) have substantially the same ramp cross-section, so that the angular position is selectable between a minimum angular position in which the wider sides (2") of the rings (2) are arranged at diametrically opposite positions, and a maximum angular position in which the wider sides (2") of the rings (2) are arranged at diametrically coincident positions.