Homing load detecting device for rescue hoist and winch assemblies
AssigneeHornet Acquisitionco, LLC
InventorsSanith Kurumpilavu Subramanian, Nagesh Sadashivaiah, Robert A. Blaser, Arthur A. Martinez
Life of this patent
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Abstract
A fixture is described. The fixture is for detecting forces between a hook assembly and a bell mouth of a rescue hoist. The fixture couples to the bell mouth such that the fixture is affixed to a main housing of the rescue hoist. A cable of the rescue hoist extends through the bell mouth and the fixture. The cable includes a distal end coupled to the hook assembly. The cable is retractable causing the hook assembly to abut the fixture. The fixture may then detect the force. The force may be used to provide an indication to a crew of an aircraft that the force is below a minimum homing load or above a maximum homing load.
Claims20
A fixture comprising:
- a surface;
- a cylindrical wall extending from the surface;
- wherein the cylindrical wall is configured to receive at least a portion of a bell mouth of a rescue hoist;
- a body portion extending from the surface and disposed within the cylindrical wall;
- and
- a sensor configured to detect a force and generate a signal indicative of the force;
- wherein the surface and the body portion define a through hole, the through hole concentric to an axis of the cylindrical wall;
- wherein a cable of the rescue hoist is configured to extend through the through hole when the fixture is coupled to the bell mouth;
- wherein the body portion abuts the bell mouth when the fixture is coupled to the bell mouth;
- wherein the surface and the body portion define a first slotted through hole, a second slotted through hole, and a third slotted through hole;
- wherein the first slotted through hole, the second slotted through hole, and the third slotted through hole each extend radially outward from the axis of the cylindrical wall;
- wherein the first slotted through hole, the second slotted through hole, and the third slotted through hole are arranged at a one-hundred-and-twenty degree angle relative to each other;
- and
- wherein the surface, the cylindrical wall, and the body portion define a rectangular slot from an outer diameter of the cylindrical wall up to the second slotted through hole.
A rescue hoist comprising:
- a motor configured to drive a cable drum of the rescue hoist;
- a cable disposed on the cable drum, wherein an end of the cable extends through a bell mouth of the rescue hoist;
- a hook assembly disposed on the end of the cable;
- a fixture coupled to the bell mouth, wherein the hook assembly abuts the fixture when the hook assembly is in a homed position, the fixture comprising:
- a surface;
- a cylindrical wall extending from the surface, wherein at least a portion of the bell mouth is disposed within the cylindrical wall;
- a body portion extending from the surface and disposed within the cylindrical wall,
- wherein the bell mouth abuts the body portion;
- and
- a sensor configured to detect a force between the bell mouth and the hook assembly and generate a signal indicative of the force;
- wherein the surface and the body portion define a through hole, the through hole concentric to an axis of the cylindrical wall, wherein the cable extends through the through hole;
- wherein the surface and the body portion define a first slotted through hole, a second slotted through hole, and a third slotted through hole;
- wherein the first slotted through hole, the second slotted through hole, and the third slotted through hole each extend radially outward from the axis of the cylindrical wall;
- wherein the first slotted through hole, the second slotted through hole, and the third slotted through hole are arranged at a one-hundred-and-twenty degree angle relative to each other;
- and
- wherein the surface, the cylindrical wall, and the body portion define a rectangular slot from an outer diameter of the cylindrical wall up to the second slotted through hole.
A system comprising:
- an aircraft comprising a cockpit panel;
- and
- a rescue hoist coupled to the aircraft, the rescue hoist comprising:
- a motor configured to drive a cable drum of the rescue hoist;
- a cable disposed on the cable drum, wherein an end of the cable extends through a bell mouth of the rescue hoist;
- a hook assembly disposed on the end of the cable;
- a fixture coupled to the bell mouth, wherein the hook assembly abuts the fixture when the hook assembly is in a homed position, the fixture comprising:
- a surface;
- a cylindrical wall extending from the surface, wherein at least a portion of the bell mouth is disposed within the cylindrical wall;
- a body portion extending from the surface and disposed within the cylindrical wall, wherein the bell mouth abuts the body portion;
- and
- a sensor configured to detect a force between the bell mouth and the hook assembly and generate a signal indicative of the force;
- wherein the surface and the body portion define a through hole, the through hole concentric to an axis of the cylindrical wall, wherein the cable extends through the through hole,
- wherein the surface and the body portion define a first slotted through hole, a second slotted through hole, and a third slotted through hole,
- wherein the first slotted through hole, the second slotted through hole, and the third slotted through hole each extend radially outward from the axis of the cylindrical wall,
- wherein the first slotted through hole, the second slotted through hole, and the third slotted through hole are arranged at a one-hundred-and-twenty degree angle relative to each other, and
- wherein the surface, the cylindrical wall, and the body portion define a rectangular slot from an outer diameter of the cylindrical wall up to the second slotted through hole.
A fixture comprising:
- a surface;
- a cylindrical wall extending from the surface;
- wherein the cylindrical wall is configured to receive at least a portion of a bell mouth of a rescue hoist;
- a body portion extending from the surface and disposed within the cylindrical wall;
- a first sensor of a plurality of sensors, the first sensor configured to detect a force and generate a signal indicative of the force;
- and
- one or more wires;
- wherein the surface and the body portion define a through hole;
- wherein a cable of the rescue hoist is configured to extend through the through hole when the fixture is coupled to the bell mouth;
- wherein the body portion abuts the bell mouth when the fixture is coupled to the bell mouth;
- wherein the surface, the cylindrical wall, and the body portion define a groove disposed around an outer diameter of the body portion;
- wherein the body portion defines a blind slotted hole extending radially outward from the sensor up to the groove;
- wherein the one or more wires are disposed within the groove;
- and
- wherein the one or more wires couple the sensor to the processor by which the processor is configured to receive the signal.
A rescue hoist comprising:
- a motor configured to drive a cable drum of the rescue hoist;
- a cable disposed on the cable drum, wherein an end of the cable extends through a bell mouth of the rescue hoist;
- a hook assembly disposed on the end of the cable;
- a fixture coupled to the bell mouth, wherein the hook assembly abuts the fixture when the hook assembly is in a homed position, the fixture comprising:
- a surface;
- a cylindrical wall extending from the surface, wherein at least a portion of the bell mouth is disposed within the cylindrical wall;
- a body portion extending from the surface and disposed within the cylindrical wall, wherein the bell mouth abuts the body portion;
- a first sensor of a plurality of sensors, the first sensor configured to detect a force between the bell mouth and the hook assembly and generate a signal indicative of the force;
- and
- one or more wires;
- wherein the surface and the body portion define a through hole, wherein the cable extends through the through hole;
- wherein the surface, the cylindrical wall, and the body portion define a groove disposed around an outer diameter of the body portion;
- wherein the body portion defines a blind slotted hole extending radially outward from the sensor up to the groove;
- wherein the one or more wires are disposed within the groove;
- and
- wherein the one or more wires couple the sensor to the processor by which the processor is configured to receive the signal.
A system comprising:
- an aircraft comprising a cockpit panel;
- and
- a rescue hoist coupled to the aircraft, the rescue hoist comprising:
- a motor configured to drive a cable drum of the rescue hoist;
- a cable disposed on the cable drum, wherein an end of the cable extends through a bell mouth of the rescue hoist;
- a hook assembly disposed on the end of the cable;
- a fixture coupled to the bell mouth, wherein the hook assembly abuts the fixture when the hook assembly is in a homed position, the fixture comprising:
- a surface;
- a cylindrical wall extending from the surface, wherein at least a portion of the bell mouth is disposed within the cylindrical wall;
- a body portion extending from the surface and disposed within the cylindrical wall, wherein the bell mouth abuts the body portion;
- a first sensor of a plurality of sensors, the first sensor configured to detect a force between the bell mouth and the hook assembly and generate a signal indicative of the force;
- and
- one or more wires;
- wherein the surface and the body portion define a through hole, wherein the cable extends through the through hole,
- wherein the surface, the cylindrical wall, and the body portion define a groove,
- wherein the body portion defines a blind slotted hole extending radially outward from the sensor up to the groove,
- wherein the one or more wires are disposed within the blind slotted hole and the groove,
- wherein the one or more wires couple the sensor to the processor by which the processor is configured to receive the signal, and
- wherein the groove is disposed around an outer diameter of the body portion;
- wherein the sensor is a first sensor of a plurality of sensors;
- wherein the one or more wires are disposed in the groove.
Dependencies are inferred from the claim text.