Abstract:
An engine mount may include a clevis and a lug defining a hole therethrough. A pin may be joined to the clevis and may extend through the hole of the lug with the pin and the lug defining a clearance therebetween. A trigger system may be disposed on the lug and operatively associated with the pin.
Abstract:
A nacelle for a gas turbine engine includes a bifurcation, an outer diameter cowl and a first latch system. The outer diameter cowl extends from the bifurcation and the first latch system is mounted on the outer diameter cowl. The first latch system is spaced along the outer diameter cowl from the bifurcation.
Abstract:
An assembly includes a pin, a fastener, a first element, and a paddle. The pin includes a first channel. The fastener extends within the pin and has a head extending from a first end of the pin. The first element is mounted to the fastener and is capable of translation relative to the pin with rotation of the fastener. The paddle is movably connected to the first element and disposed within the first channel. At least a portion of the paddle extends from the first channel to protrude from the pin with translation of the first element.
Abstract:
An assembly includes a pin, a fastener, a first element, and a paddle. The pin includes a first channel. The fastener extends within the pin and has a head extending from a first end of the pin. The first element is mounted to the fastener and is capable of translation relative to the pin with rotation of the fastener. The paddle is movably connected to the first element and disposed within the first channel. At least a portion of the paddle extends from the first channel to protrude from the pin with translation of the first element.
Abstract:
A blind installation pin assembly for a gas turbine engine includes a pin that defines a bore. A paddle mounted to an end of the pin to pivot about a paddle axis between an install position and a lock position. A T-bolt that passes through the bore, a crosspiece of the T-bolt selectively engageable with the paddle.
Abstract:
An engine mount may include a clevis and a lug defining a hole therethrough. A pin may be joined to the clevis and may extend through the hole of the lug with the pin and the lug defining a clearance therebetween. A trigger system may be disposed on the lug and operatively associated with the pin.
Abstract:
A nacelle for a gas turbine engine includes a upper and lower bifurcations, an inner diameter cowl and a first latch system. The inner diameter cowl extends between the upper and lower bifurcations and the first latch system is mounted on the inner diameter cowl. The first latch system is spaced along the inner diameter cowl between the upper and lower bifurcations.
Abstract:
A blind installation pin assembly for a gas turbine engine includes a pin that defines a bore. A paddle mounted to an end of the pin to pivot about a paddle axis between an install position and a lock position. A T-bolt that passes through the bore, a crosspiece of the T-bolt selectively engageable with the paddle.