초록 ▼

Means for mounting an engine component to the exterior of an engine\s case that is mounted in an aircraft with limited access including a blind mount. The mount includes an elongated bracket fixed to the exterior of the engine case with a clevis at one end of the bracket to receive a blind mount on

Means for mounting an engine component to the exterior of an engine\s case that is mounted in an aircraft with limited access including a blind mount. The mount includes an elongated bracket fixed to the exterior of the engine case with a clevis at one end of the bracket to receive a blind mount on said engine component. Camming means operatively connected to an accessible torquing member secures the engine component in place. Hook elements on the bracket engage said engine component to allow the operator to free his hands to operate the torquing means. The mount is designed to be compatible with the existing vibratory isolation system built into the engine component.

대표청구항 ▼

Means for removably mounting an engine component to the case of an engine that is adapted to be mounted in an aircraft comprising an elongated bracket having means for mounting said bracket to said case, said elongated bracket having at one end a clevis defining a pair of support arms adapted to rel

Means for removably mounting an engine component to the case of an engine that is adapted to be mounted in an aircraft comprising an elongated bracket having means for mounting said bracket to said case, said elongated bracket having at one end a clevis defining a pair of support arms adapted to releasably support a pedestal attached to the engine component, movable means attached to said clevis for securing said pedestal in position, torquing means supported to said elongated bracket having a tool engagement end remotely spaced from said moveable means operatively connected to said movable means for positioning said movable means to engage and disengage said pedestal for attaching and releasing said engine component, said torquing means being engagable from an access opening formed in a wall of said aircraft, said elongated bracket including a pair of axially extending arms each of which include hook means attached to the ends thereof adapted to engage complementing pedestals formed on said engine component to releaseably support said engine component whereby the operator can free himself from holding said engine component in place during installation and removal of said engine component.