Inboard beam with pin system for anti-rotation and centrifugal force retention

Patent metadata

Field	Value
Publication number	US-10960970-B2
Application number	US-201816184436-A
Country	US
Kind code	B2
Filing date	Nov 8, 2018
Priority date	Nov 8, 2018
Publication date	Mar 30, 2021
Grant date	Mar 30, 2021

Abstract

An inboard beam includes a body having an upper flange and a lower flange coupled thereto. The upper flange includes a first upper inboard aperture and an upper outboard aperture formed therein. The lower flange includes a first lower inboard aperture and a lower outboard aperture formed therein. An upper beam fitting is coupled to the upper flange and lower beam fitting is coupled to the lower flange. The upper beam fitting includes a first upper inboard post. The upper beam fitting includes an upper outboard post extending parallel to the inboard post. The lower beam fitting includes a first lower inboard post. The lower beam fitting includes a lower outboard post extending parallel to the lower inboard post.

First claim

What is claimed is:

1. An inboard beam assembly, comprising:
an inboard beam, comprising:
a body;
an upper flange coupled to the body, the upper flange having a first upper inboard aperture and an upper outboard aperture formed therein; and
a lower flange coupled to the body, the lower flange having a first lower inboard aperture and a lower outboard aperture formed therein;

an upper beam fitting coupled to the upper flange, the upper beam fitting comprising:
a first upper inboard post, the first upper inboard post being received by the first upper inboard aperture and secured to the upper flange via a threaded extension from the first upper inboard post; and
an upper outboard post and extending parallel to the first upper inboard post, the upper outboard post being received by the upper outboard aperture and secured to the upper flange via a threaded extension from the upper outboard post;

an upper clearance cut formed in the body proximate the upper flange, the upper clearance cut comprising an opening in the body that provides access to the threaded extension from the first upper inboard post and the threaded extension from the upper outboard post;
a lower beam fitting coupled to the lower flange, the lower beam fitting comprising:
a first lower inboard post, the first lower inboard post being received by the first lower inboard aperture and secured to the lower flange via a threaded extension from the first lower inboard post; and
a lower outboard post extending parallel to the first lower inboard post, the lower outboard post being received by the lower outboard aperture and secured to the lower flange via a threaded extension from the lower outboard post.

2. The inboard beam assembly of claim 1 , comprising:
a lower clearance cut formed in the body proximate the lower flange, the lower clearance cut comprising an opening in the body that provides access to the threaded extension from the first lower inboard post and threaded extension from the lower outboard post.

3. The inboard beam assembly of claim 1 , wherein:
the upper beam fitting comprises a second upper inboard post extending generally parallel to the first upper inboard post; and
the lower beam fitting comprises a second lower inboard post extending generally parallel to the first lower inboard post.

4. The inboard beam assembly of claim 1 , wherein:
the first upper inboard post has a diameter larger than a diameter of the upper outboard post; and
the first lower inboard post has a diameter larger than a diameter of the lower outboard post.

5. The inboard beam assembly of claim 1 , wherein the first upper inboard post and the first lower inboard post support centrifugal force and centripetal force.

6. The inboard beam assembly of claim 1 , wherein the upper outboard post and the lower outboard post support anti-rotation forces.

7. A rotor system for an aircraft, the rotor system comprising:
a rotor blade comprising a grip;
a yoke comprising a yoke arm;
an inboard beam assembly coupled to the grip and rotatably coupled to the yoke arm, the inboard beam assembly comprising:
a body;
an upper flange coupled to the body, the upper flange having a first upper inboard aperture and an upper outboard aperture formed therein; and
a lower flange coupled to the body, the lower flange having a first lower inboard aperture and a lower outboard aperture formed therein;

an upper beam fitting coupled to the upper flange, the upper beam fitting comprising:
a first upper inboard post, the first upper inboard post being received by the first upper inboard aperture and secured to the upper flange via a threaded extension from the first upper inboard post; and
an upper outboard post extending parallel to the first upper inboard post, the upper outboard post being received by the upper outboard aperture and secured to the upper flange via a threaded extension from the upper outboard post;

an upper clearance cut formed in the body proximate the upper flange, the upper clearance cut comprising an opening in the body that provides access to the threaded extension from the first upper inboard post and the threaded extension from the upper outboard post;
a lower beam fitting coupled to the lower flange, the lower beam fitting comprising:
a first lower inboard post, the first lower inboard post being received by the first lower inboard aperture and secured to the lower flange via a threaded extension from the first lower inboard post; and
a lower outboard post extending parallel to the first lower inboard post, the lower outboard post being received by the lower outboard aperture and secured to the lower flange via a threaded extension from the lower outboard post.

8. The rotor system of claim 7 , wherein the body comprises:
a lower clearance cut formed in the body proximate the lower flange, the lower clearance cut comprising an opening in the body that provides access to the threaded extension from the first lower inboard post and threaded extension from the lower outboard post.

9. The rotor system of claim 8 , comprising:
upper detents formed in the body proximate the upper flange; and
lower detents formed in the body proximate the lower flange.

10. The rotor system of claim 9 , wherein the body is disposed within the yoke arm.

11. The rotor system of claim 10 , wherein body rotates with respect to the yoke arm about an axis of the yoke arm.

12. The rotor system of claim 11 , wherein the upper detents and the lower detents permit further rotation of the body with respect to the yoke arm than if the upper detents and the lower detents were not present.

13. The rotor system of claim 8 , comprising:
an upper neck region formed in the body proximate the upper flange; and
a lower neck region formed in the body proximate the lower flange.

14. The rotor system of claim 13 , wherein the body is disposed within the yoke arm.

15. The rotor system of claim 14 , wherein body rotates with respect to the yoke arm about an axis of the yoke arm.

16. The rotor system of claim 15 , wherein the upper neck region and the lower neck region permit further rotation of the body with respect to the yoke arm than if the upper neck region and the lower neck region were not present.

17. A method of installing an inboard beam assembly, the method comprising:
arranging an inboard beam in a grip of a rotor blade such that:
a first upper inboard aperture of the inboard beam aligns with a first upper inboard aperture of the grip;
a first lower inboard aperture of the inboard beam aligns with a first lower inboard aperture of the grip;
an upper outboard aperture of the inboard beam aligns with an upper outboard aperture of the grip; and
a lower outboard aperture of the inboard beam aligns with the lower outboard aperture of the grip;

assembling an upper beam fitting such that a first upper inboard post is received through the first upper inboard aperture of the grip and the first upper inboard aperture of the inboard beam and is secured via a threaded extension from the first upper inboard post, wherein the threaded extension from the first upper inboard post is accessible via an upper clearance cut formed in the inboard beam, the upper clearance cut comprising an opening in the inboard beam; and
assembling a lower beam fitting such that a first lower inboard post is received through the first lower inboard aperture of the grip and the first lower inboard aperture of the inboard beam and is secured via a threaded extension from the first lower inboard post.

18. The method of claim 17

Assignees

• Bell Helicopter Textron Inc

Inventors

• Foskey Whitney
• Cravener Kyle Thomas

Classifications

• B64C27/48 Primary

  Root attachment to rotor head · CPC title

• B64C27/39

  with individually articulated blades, i.e. with flapping or drag hinges · CPC title

• B64C11/20

  Constructional features · CPC title

• B64C11/32 Primary

  mechanical · CPC title