Winch system for an airborne payload control system

Patent metadata

Field	Value
Publication number	US-10519013-B2
Application number	US-201715444686-A
Country	US
Kind code	B2
Filing date	Feb 28, 2017
Priority date	Feb 28, 2017
Publication date	Dec 31, 2019
Grant date	Dec 31, 2019

Abstract

A method for a winch system includes receiving, from a controller, instructions to spool a payload line, the payload line comprising a first end and a second end, the first end coupled to a main reel of the winch system and the second end configured to couple to a payload. The method further includes operating, based on the instructions, one or more of a first motor of the winch system and a second motor of the winch system, wherein the one or more of the first motor and the second motor are operated in order to control a position of the second end of the payload line.

First claim

What is claimed is:

1. A winch system for use in an aircraft, the winch system comprising:
a payload line comprising a sensor, a first end and a second end, wherein:
the second end is operable to couple to a payload; and
the sensor is operable to detect information about the payload line and transmit the detected information to at least one controller;

a main reel about which the payload line is wound;
a first motor operable to turn the main reel in a first and a second direction in response to receiving instructions from the at least one controller, wherein turning the main reel in the first direction feeds the payload line out, and turning the wheel in the second direction reels the payload line in;
a first pinch roller and a second pinch roller between which the payload line is threaded, wherein the first and the second pinch rollers are configured to maintain tension on the payload line; and
a second motor operable to turn the first and the second pinch rollers in response to receiving instructions from the at least one controller, wherein turning the pinch rollers in the first direction feeds the payload line out, and turning the pinch rollers in the second direction reels the payload line in;
wherein:
the first and the second motors cooperate to feed out and reel in the payload line; and
one or more of the main reel or the first and the second pinch rollers is turned based on information detected by the sensor in order to control a position or the second end of the payload line when the aircraft is airborne.

2. The winch system of claim 1 , wherein feeding the payload line out comprises:
the first motor applying a braking function; and
the second motor turning the pinch rollers in the first direction.

3. The winch system of claim 1 , wherein reeling in the payload line in comprises:
the first motor turning the main reel in the second direction; and
the second motor applying a braking function.

4. The winch system of claim 1 , further comprising the at least one controller, the at least one controller operable to provide instructions to each of the first and the second motors, wherein the instructions cause one or more of the first and the second motors to turn or apply a braking function to one or more of the main reel and the pinch rollers.

5. The winch system of claim 4 , further comprising:
a first encoder associated with the first motor, the first encoder operable to detect information about the payload line on the main reel; and
a second encoder associated with the second motor, the second encoder operable to detect information about the payload line between the first and the second pinch rollers.

6. The winch system of claim 5 , wherein the at least one controller is configured to:
receive information from one or more of the first and the second encoders; and
based on the received information, provide instructions to one or more of the first or the second motors to adjust one or more of:
the speed of the payload line;
the acceleration of the payload line; and
the position of the payload line.

7. The winch system of claim 1 , further comprising a locking mechanism operable to prevent the main reel from turning.

8. The winch system of claim 7 , wherein the pinch rollers are configured to cut the payload line, wherein cutting the payload line comprises:
locking the main reel using the locking mechanism; and
increasing the speed of the second motor.

9. The winch system of claim 1 , further comprising a servo motor operable to move a sliding shaft, wherein:
the sliding shaft comprises a guide hole through which the payload line is threaded; and
moving the sliding shaft causes the payload line to be distributed around the main reel in a substantially even manner.

10. A controller of a winch system for use in an aircraft, the controller operable to:
receive, from a sensor of the winch system, information about a payload line, the payload line comprising a first end and a second end;
provide instructions to at least one motor of the winch system based on the information received from the sensor in order to control a position of the second end of the payload line when the aircraft is airborne, wherein the winch system comprises:
a first motor operable to turn a main reel of the winch system in a first and a second direction, wherein turning the main reel in the first direction feeds the payload line out and turning the main reel in the second direction reels the payload line in; and
a second motor operable to turn a first pinch roller and a second pinch roller of the winch system, wherein turning the pinch rollers in the first direction feeds the payload line out, and turning the pinch rollers in the second direction reels the payload line in;

wherein the first and the second motors cooperate to feed out and reel in the payload line.

11. The controller of claim 10 , wherein feeding the payload line out comprises:
the first motor applying a braking function; and
the second motor turning the pinch rollers in the first direction.

12. The controller of claim 10 , wherein reeling in the payload line in comprises:
the first motor turning the main reel in the second direction; and
the second motor applying a braking function.

13. The controller of claim 10 , further comprising:
receiving information about the payload line on the main reel from a first encoder associated with the first motor; and
receiving information about the payload line between the first and the second pinch rollers from a second encoder associated with the first and the second pinch rollers.

14. The controller of claim 13 , wherein the instructions provided to one or more of the first and the second motors are based on the information received from one or more of the first and the second encoders.

15. The controller of claim 14 , wherein the instructions to one or more of the first or the second motors comprise an instruction to adjust one or more of:
the speed of the payload line;
the acceleration of the payload line; and
the position of the payload line.

16. A method for a winch system for use in an aircraft, the method comprising:
receiving, from a sensor, information about a payload line, wherein the payload line comprises a first end and a second end, the first end coupled to a main reel of the winch system and the second end configured to couple to a payload;
receiving, from a controller, instructions to spool the payload line based on the information received from the sensor; and
operating, based on the instructions, one or more of a first motor of the winch system and a second motor of the winch system, wherein the one or more of the first motor and the second motor are operated in order to control a position of the second end of the payload line when the aircraft is airborne.

17. The method of claim 16 , wherein the instructions to spool the payload line comprise instructions to reel in or reel out the payload line.

18. The method of claim 17 , wherein reeling the payload line out comprises:
applying, by the first motor, a braking function; and
turning, by the second motor, the pinch rollers in the first direction.

19. The method of claim 17 , wherein reeling in the payload line in comprises:
turning, by the first motor, the main reel in the second direction; and
applying, by the second motor, a braking function.

20. The method of claim 16 , further comprising:
receiving information about one or more of:
the payload line on the main reel;
the payload line be

Assignees

• Lockheed Corp

Inventors

• Curran Matthew
• Gamble Dustin E
• Jennings Gordon
• Neel Justin

Classifications

• B66D2700/0141

  Electrically actuated · CPC title

• B64D1/08

  the articles being load-carrying devices · CPC title

• B66D2700/0108

  with devices for paying out or automatically tightening the cable · CPC title

• B66D1/12

  incorporating electric motors · CPC title

• B64D1/22

  Taking-up articles from earth's surface · CPC title