Abstract: A housing for a gas turbine engine accessory includes an enclosure having a drive end with an opening and a closure. The closure is seated in the opening, defines therethrough a shaft aperture and has a v-band flange extending about a periphery of the closure to limit load carried by the enclosure when the engine accessory is mounted to an accessory gearbox mount in a cantilevered arrangement. Engine accessories for gas turbine engines and mounting arrangements for gas turbine engine accessories are also described.

Abstract: A bracket assembly for supporting terminal leads in an auxiliary generator of an aircraft, which includes a first bracket adapted and configured to be fastened to a stator housing of the generator to retain a main stator within the stator housing, and a second bracket adapted and configured to be fastened to a top surface of the first bracket to support a plurality of terminal leads in such a manner so that they are not susceptible to damage from resonance and vibration.

Abstract: A cross rod for use in a toggle mechanism including a first section, a second section and a midsection between the first section and the second section. The midsection includes a flange having a through hole. The first section has a first diameter, the second section has a second diameter, and the midsection has a third diameter. The third diameter being larger than at least one of the first diameter and the second diameter.

Abstract: A bracket assembly for supporting terminal leads in an auxiliary generator of an aircraft, which includes a first bracket adapted and configured to be fastened to a stator housing of the generator to retain a main stator within the stator housing, and a second bracket adapted and configured to be fastened to a top surface of the first bracket to support a plurality of terminal leads in such a manner so that they are not susceptible to damage from resonance and vibration.

Abstract: A housing for a gas turbine engine accessory includes an enclosure having a drive end with an opening and a closure. The closure is seated in the opening, defines therethrough a shaft aperture and has a v-band flange extending about a periphery of the closure to limit load carried by the enclosure when the engine accessory is mounted to an accessory gearbox mount in a cantilevered arrangement. Engine accessories for gas turbine engines and mounting arrangements for gas turbine engine accessories are also described.

Abstract: A clevis for use in a toggle mechanism of a ram air turbine actuator is provided comprising a first side; a second side parallel to the first side; a first set of parallel pivot holes; second set of parallel pivot holes; a set of parallel through holes; and a helicoil blind hole. The second side rigidly connected to the first side via at least one brace perpendicular to the first side and the second side. The helicoil blind hole being located in the first side and extending into the at least one brace. The first side having a first hole of the first set of parallel pivot holes, a first hole of the second set of parallel pivot holes, and a first hole of the set of parallel through holes. The second side having the hole pattern reflective of the first side, composed of second holes.

Abstract: A clevis for use in a toggle mechanism of a ram air turbine actuator is provided comprising a first side; a second side parallel to the first side; a first set of parallel pivot holes; second set of parallel pivot holes; a set of parallel through holes; and a helicoil blind hole. The second side rigidly connected to the first side via at least one brace perpendicular to the first side and the second side. The helicoil blind hole being located in the first side and extending into the at least one brace. The first side having a first hole of the first set of parallel pivot holes, a first hole of the second set of parallel pivot holes, and a first hole of the set of parallel through holes. The second side having the hole pattern reflective of the first side, composed of second holes.

Abstract: A cross rod for use in a toggle mechanism including a first section, a second section and a midsection between the first section and the second section. The midsection includes a flange having a through hole. The first section has a first diameter, the second section has a second diameter, and the midsection has a third diameter. The third diameter being larger than at least one of the first diameter and the second diameter.

Abstract: A driveshaft for an aircraft ram air turbine includes a tubular body and a flange. The tubular body defines an axis of rotation and includes a forward portion and a frusto-conical portion located rearward of the forward portion. The flange adjoins the forward portion of the tubular body opposite the frusto-conical portion, and has a forward face and an opposite rear face. A ratio of an outer diameter of the forward portion of the tubular body to an inner diameter of the forward portion of the tubular body is in a range of approximately 1.423 to 1.425.