F - Mech Eng,Light,Heat,Weapons – 42 – B
Patent
F - Mech Eng,Light,Heat,Weapons
42
B
F42B 10/14 (2006.01)
Patent
CA 2499956
The present invention concerns a method for designing a deployment mechanism for a flight surface on an airborne body, including the steps of determining a stowed position of the flight surface, determining a deployed position of the flight surface, identifying a first rotation axis and respective rotation angle and a second rotation axis and respective rotation angle about and through which the flight surface is rotatable in sequence to move the flight surface from the stowed position to the deployed position, or vice versa, and using the identified first and second rotation axes and rotation angles to determine a single equivalent rotation axis and angle, about and through which the flight surface can be rotated from the stowed position to the deployed position, or vice versa.
La présente invention concerne un méthode de conception d'un mécanisme de déploiement pour une surface portante sur un corps aéroporté. Cette méthode consiste à déterminer une position d'arrimage de la surface portante ; déterminer une position déployée de la surface portante ; identifier un premier axe de rotation et un premier angle de rotation correspondant, et un second axe de rotation et un angle de rotation correspondant, selon lesquels la surface portante peut pivoter séquentiellement pour passer de la position d'arrimage à la position de déploiement, ou vice versa ; et utiliser les premiers et seconds axes de rotation et angles de rotation pour déterminer une axe et un angle de rotation équivalents uniques autour desquels et selon lesquels la surface portante peut passer par rotation de la position d'arrimage à la position de déploiement, ou vice versa.
Eisentraut Rudolph A.
Melkers Edgar R.
Raytheon Company
Sim & Mcburney
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