Chordwise folding and locking of rotor systems

Patent metadata

Field	Value
Publication number	US-10239605-B2
Application number	US-201615269739-A
Country	US
Kind code	B2
Filing date	Sep 19, 2016
Priority date	Sep 19, 2016
Publication date	Mar 26, 2019
Grant date	Mar 26, 2019

Abstract

An apparatus for chordwise folding and locking of rotor systems includes a grip assembly and a harness disposed at least partially within and coupled to the grip assembly. A rotor blade is rotatably coupled to the grip assembly and the harness. The rotor blade has a radially extended orientation and a stowed orientation. A linkage assembly has a first end, a second end and a pivot joint therebetween. The first end of the linkage assembly is rotatably coupled to the harness and the second end of the linkage assembly is rotatably coupled to the rotor blade. A first lock assembly selectively secures the rotor blade to the grip assembly and the harness when the rotor blade is in the radially extended orientation. A second lock assembly selectively secures the rotor blade relative to the harness when the rotor blade is in the stowed orientation.

First claim

What is claimed is:

1. An apparatus for chordwise folding and locking of rotor systems, the apparatus comprising:
a grip assembly;
a harness disposed at least partially within and coupled to the grip assembly;
a rotor blade rotatably coupled to the grip assembly and the harness, the rotor blade having a radially extended orientation and a stowed orientation;
a linkage assembly having a first end, a second end and a pivot joint therebetween, the first end rotatably coupled to the harness and the second end rotatably coupled to the rotor blade;
a first lock assembly selectively securing the rotor blade to the grip assembly and the harness when the rotor blade is in the radially extended orientation; and
a pawl assembly selectively securing the rotor blade relative to the harness when the rotor blade is in the stowed orientation.

2. The apparatus as recited in claim 1 further comprising a pivot pin coupling the rotor blade to the grip assembly and the harness.

3. The apparatus as recited in claim 1 wherein the linkage assembly further comprises first and second tow links rotatably coupled to the harness, a drag link rotatably coupled to the rotor blade and a latch pin pivotably coupling the first and second tow links to the drag link.

4. The apparatus as recited in claim 3 further comprising first and second bushings respectively rotatably coupling the first and second tow links to the harness.

5. The apparatus as recited in claim 3 further comprising a linkage pin rotatably coupling the drag link to the rotor blade.

6. The apparatus as recited in claim 1 wherein the first lock assembly further comprises a release pin selectively securing the rotor blade to the grip assembly and the harness when the rotor blade is in the radially extended orientation.

7. The apparatus as recited in claim 6 wherein the release pin is removable to allow chordwise folding of the rotor blade relative to the grip assembly and the harness between the radially extended orientation and the stowed orientation.

8. The apparatus as recited in claim 6 wherein the release pin is manually removable to allow chordwise folding of the rotor blade relative to the grip assembly and the harness between the radially extended orientation and the stowed orientation.

9. The apparatus as recited in claim 1 wherein the pawl assembly is disengaged to allow the rotor blade to be released from the stowed orientation.

10. The apparatus as recited in claim 1 wherein the pawl assembly is manually disengaged to allow the rotor blade to be released from the stowed orientation.

11. A method of chordwise folding and locking of rotor systems including a grip assembly, a harness disposed at least partially within and coupled to the grip assembly and a rotor blade rotatably coupled to the grip assembly and the harness, the method comprising:
releasing a first lock selectively securing the rotor blade to the grip assembly and the harness in a radially extended orientation;
folding the rotor blade chordwise relative to the grip assembly and the harness from the radially extended orientation to a stowed orientation while extending a linkage assembly coupled between the harness and the rotor blade; and
securing the rotor blade in the stowed orientation relative to the harness by engaging a pawl assembly.

12. The method as recited in claim 11 wherein releasing the first lock selectively securing the rotor blade to the grip assembly and the harness in the radially extended orientation further comprises removing a release pin securing the rotor blade to the grip assembly and the harness.

13. The method as recited in claim 11 wherein releasing the first lock selectively securing the rotor blade to the grip assembly and the harness in the radially extended orientation further comprises manually removing a release pin securing the rotor blade to the grip assembly and the harness.

14. The method as recited in claim 11 wherein folding the rotor blade chordwise relative to the grip assembly and the harness from the radially extended orientation to the stowed orientation further comprises manually folding the rotor blade chordwise relative to the grip assembly and the harness from the radially extended orientation to the stowed orientation.

15. The method as recited in claim 11 wherein extending the linkage assembly coupled between the harness and the rotor blade further comprises pivoting a drag link, rotatably coupled to the rotor blade, relative to first and second tow links, rotatably coupled to the harness, about a latch pin.

16. The method as recited in claim 11 further comprising:
disengaging the pawl assembly;
rotating the rotor blade relative to the grip assembly and the harness from the stowed orientation to the radially extended orientation while contracting the linkage assembly coupled between the harness and the rotor blade; and
securing the rotor blade to the grip assembly and the harness in the radially extended orientation with the first lock assembly.

17. The method as recited in claim 16 wherein securing the rotor blade to the grip assembly and the harness in the radially extended orientation with the first lock assembly further comprises inserting a release pin.

Assignees

• Bell Helicopter Textron Inc

Inventors

• Foskey Christopher Edward
• Burnett Michael Christopher

Classifications

• B64C29/0033

  the propellers being tiltable relative to the fuselage · CPC title

• B64C11/28 Primary

  Collapsible or foldable blades · CPC title

• B64C27/50

  Blades foldable to facilitate stowage of aircraft · CPC title