A structure attachment for a hanging support system includes an attachment body and a structure fastener coupled to the attachment body and configured to fasten the structure attachment to a structural support. A rod fastener is coupled to the attachment body and defines at least one threaded opening configured to mate with a threaded rod. The rod fastener is selectively movable relative to the structure fastener to adjust an angle between an axis of the threaded opening and a longitudinal axis of the structure fastener.

One example of a duct support for a rotorcraft includes a stabilizing mechanism configured to transfer a weight of a duct to an airframe of the rotorcraft, where the duct undergoes thermal expansion. The stabilizing mechanism includes a first stabilizing member attached to the duct, a second stabilizing member attached to the rotorcraft, and a coupling mechanism where the coupling mechanism is configured to couple the first stabilizing member to the second stabilizing member and accommodate thermal expansion of the duct by allowing for movement of the first stabilizing member relative to the second stabilizing member. In an example, the duct is an exhaust duct of an engine of the rotorcraft and heat from the engine cause the exhaust duct to undergo the thermal expansion.

One example of a duct support for a rotorcraft includes a stabilizing mechanism configured to transfer a weight of a duct to an airframe of the rotorcraft, where the duct undergoes thermal expansion. The stabilizing mechanism includes a first stabilizing member attached to the duct, a second stabilizing member attached to the rotorcraft, and a coupling mechanism where the coupling mechanism is configured to couple the first stabilizing member to the second stabilizing member and accommodate thermal expansion of the duct by allowing for movement of the first stabilizing member relative to the second stabilizing member. In an example, the duct is an exhaust duct of an engine of the rotorcraft and heat from the engine cause the exhaust duct to undergo the thermal expansion.

The present application discloses a hose that uses pressure to lock itself into a fixed position. The basic structure may comprise an internal flexible tube which contains a fluid and a mechanical exoskeleton. The mechanical exoskeleton may move freely without pressure, but may lock into place once the tube is pressurized.

The present application discloses a hose that uses pressure to lock itself into a fixed position. The basic structure may comprise an internal flexible tube which contains a fluid and a mechanical exoskeleton. The mechanical exoskeleton may move freely without pressure, but may lock into place once the tube is pressurized.

Embodiments of the invention provide a system and method of using a grapple assembly comprising grapple arms, mecanum wheels, and drive motors. The grapple assembly may use the grapple arms to grasp a pole and support the pole using the mecanum wheels. The drive motors may be configured to drive the mecanum wheels to rotate the mecanum wheels to provide translation and rotation of the pole. The method may be used for positioning and setting a pole, such as a utility pole.

Embodiments of the invention provide a system and method of using a grapple assembly comprising grapple arms, mecanum wheels, and drive motors. The grapple assembly may use the grapple arms to grasp a pole and support the pole using the mecanum wheels. The drive motors may be configured to drive the mecanum wheels to rotate the mecanum wheels to provide translation and rotation of the pole. The method may be used for positioning and setting a pole, such as a utility pole.

A casing spacer which allows for the positioning of a carrier pipe or set of carrier pipes in a desirable location inside a casing pipe.

One example of a duct support for a rotorcraft includes a stabilizing mechanism configured to transfer a weight of a duct to an airframe of the rotorcraft, where the duct undergoes thermal expansion. The stabilizing mechanism includes a first stabilizing member attached to the duct, a second stabilizing member attached to the rotorcraft, and a coupling mechanism where the coupling mechanism is configured to couple the first stabilizing member to the second stabilizing member and accommodate thermal expansion of the duct by allowing for movement of the first stabilizing member relative to the second stabilizing member. In an example, the duct is an exhaust duct of an engine of the rotorcraft and heat from the engine cause the exhaust duct to undergo the thermal expansion.

One example of a duct support for a rotorcraft includes a stabilizing mechanism configured to transfer a weight of a duct to an airframe of the rotorcraft, where the duct undergoes thermal expansion. The stabilizing mechanism includes a first stabilizing member attached to the duct, a second stabilizing member attached to the rotorcraft, and a coupling mechanism where the coupling mechanism is configured to couple the first stabilizing member to the second stabilizing member and accommodate thermal expansion of the duct by allowing for movement of the first stabilizing member relative to the second stabilizing member. In an example, the duct is an exhaust duct of an engine of the rotorcraft and heat from the engine cause the exhaust duct to undergo the thermal expansion.