Autopilot system, and related components and methods

• US 10,589,845 B2
• Filed: 10/14/2015
• Issued: 03/17/2020
• Est. Priority Date: 11/05/2014
• Status: Active Grant

• Current Assignee: Tzafrir Sheffer, Yarden Sheffer
• Original Assignee: Tzafrir Sheffer, Yarden Sheffer
• Inventors: Sheffer, Tzafrir, Sheffer, Yarden
• Primary Examiner(s): Johnson, Stephen
• Application Number:
  US15/520,788
• Publication Number:
  US 20170313408A1
• Time in Patent Office: 1,616 Days
• CPC Class Codes: B64C 13/04 actuated personally
• CPC Class Codes: B64C 13/0423 yokes or steering wheels for primary flight controls
• CPC Class Codes: B64C 13/0427 for actuating trim
• CPC Class Codes: B64C 13/18 using automatic pilot
• CPC Class Codes: B64C 13/22 readily revertible to personal control
• CPC Class Codes: B64C 9/02 Mounting or supporting thereof
• CPC Class Codes: B64D 43/02 for indicating aircraft speed or stalling conditions
• CPC Class Codes: G01S 19/13 Receivers
• CPC Class Codes: G05D 1/0808 specially adapted for aircraft

Abstract

A device for releasably mounting an autopilot control circuit to a flight control component of an aircraft, includes a frame that holds a component of an autopilot control circuit; a first coupler releasably fastened to the frame and operable to releasably mount the frame to the airframe of an aircraft; and a second coupler releasably fastened to the frame and operable to releasably mount the frame to a flight control component of the aircraft. When the device is releasably mounted in an aircraft'"'"'s cabin and the autopilot control circuit is engaged, the autopilot control circuit controls an aspect of the aircraft'"'"'s flight by moving the second coupler relative to the first coupler. With the device one can releasably mount an autopilot control circuit to an aircraft that does not have one and use the autopilot control circuit and device to control one or more aspects of the aircraft'"'"'s flight.

Claims

1. A device for releasably mounting an autopilot control circuit to a flight control component of an aircraft, the device comprising:

a frame that holds a component of an autopilot control circuit;

a first coupler releasably fastened to the frame and operable to releasably mount the frame to an airframe of an aircraft; and

a second coupler releasably fastened to the frame and operable to releasably mount the frame to a flight control component of the aircraft.

2. The device of claim 1 wherein the second coupler is operable to releasably mount the frame to an aircraft'"'"'s control yoke.

3. The device of claim 1 wherein the second coupler is operable to releasably mount the frame to an aircraft'"'"'s stick.

4. The device of claim 1 wherein the frame includes:

a first portion releasably fastened to the first coupler; and

a second portion releasably fastened to the second coupler, and moveable relative to the first portion.

5. The device of claim 1 wherein the frame includes:

a first portion releasably fastened to the first coupler;

a second portion having an end that is;

releasably fastened to the second coupler, and

pivotable relative to the second portion.

6. The device of claim 5 wherein the second portion'"'"'s end is slidable relative to the first portion when the end is releasably fastened to the second coupler.

7. The device of claim 1 wherein the component of the autopilot control circuit includes a control circuit that moves an end of a second portion of the frame away from a first portion of the frame.

8. The device of claim 1 wherein the component of the autopilot control circuit includes a control circuit that pivots an end of a second portion of the frame relative to the frame'"'"'s second portion.

9. The device of claim 1 wherein the component of the autopilot control circuit includes:

a control circuit that moves an end of a second portion of the frame away from a first portion of the frame;

another control circuit that pivots an end of a second portion of the frame relative to the frame'"'"'s second portion;

a control unit operable to send signals to each of the control circuits to cause each to move the frame'"'"'s second portion; and

a user interface operable to receive input from a person, convey the input to the control unit, and display information.

10. The device of claim 1 wherein the first coupler includes:

a clamp operable to releasably mount the first coupler to the airframe of an aircraft, and

a receptacle configured to receive and hold a portion of a ball that extends from a first portion of the frame.

11. The device of claim 1 wherein the second coupler includes:

a clamp operable to releasably mount the second coupler to the flight control component of the aircraft, and

a receptacle configured to receive and hold a pin that extends from an end of a second portion of the frame.

12. The device of claim 11 wherein the pin includes a longitudinal axis, the receptacle includes a cylinder having a longitudinal axis, and the pin is held by the cylinder such that the longitudinal axes of the pin and the cylinder are aligned and the pin is slidable relative to the cylinder along the cylinder'"'"'s longitudinal axis.

13. The device of claim 11 wherein the pin includes a longitudinal axis, the receptacle includes a yoke having a slot, and the pin is held by the yoke such that the longitudinal axes of the pin is substantially perpendicular to the yoke'"'"'s slot and the pin is slidable relative to the yoke along the yoke'"'"'s slot.