Tension torsion strap

Patent metadata

Field	Value
Publication number	US-10604247-B2
Application number	US-201615580174-A
Country	US
Kind code	B2
Filing date	Jun 9, 2016
Priority date	Jun 11, 2015
Publication date	Mar 31, 2020
Grant date	Mar 31, 2020

Abstract

A tension torsion strap by which a blade is connectable with a hub of a propulsor is provided. The tension torsion strap includes an elongate body formed to define attachment features at opposite ends thereof, the attachment features being connectable to the blade at one of the opposite ends and to the hub at the other of the opposite ends, fibrous materials extending along the elongate body and around the attachment features and pretension flanges elastically interposable between the hub and the elongate body. The pretension flanges are configured to maintain pretension in the fibrous materials above a predefined pretension level when the attachment features are connected to the blade and the hub.

First claim

What is claimed is:

1. A tension torsion strap by which a blade is connectable with a hub of a propulsor, the tension torsion strap comprising:
an elongate body formed to define attachment features at opposite ends thereof, the attachment features being connectable to the blade at one of the opposite ends and to the hub at the other of the opposite ends;
fibrous materials extending along the elongate body and around the attachment features; and
pretension flanges elastically interposable between the hub and the elongate body, the pretension flanges being affixable to one of the opposite ends of the elongate body such that a distal end of the pretension flanges is abuttable with the hub, wherein the pretension flanges are operable to maintain pretension in the fibrous materials above a predefined pretension level when the attachment features are connected to the blade and the hub.

2. The tension torsion strap according to claim 1 , wherein the elongate body comprises an I-beam.

3. The tension torsion strap according to claim 1 , wherein the elongate body comprises a strap casing to encompass the fibrous materials.

4. The tension torsion strap according to claim 3 , wherein the strap casing comprises urethane.

5. The tension torsion strap according to claim 1 , wherein the attachment features comprise racetrack-shaped spools.

6. The tension torsion strap according to claim 1 , wherein the fibrous materials have a spherical cross-sectional shape at each of the opposite ends.

7. The tension torsion strap according to claim 1 , wherein the pretension flanges each comprise:
a plate element affixable to one of the opposite ends of the elongate body;
a flange abuttable with the hub; and
an elastic member by which the flange is coupled with the plate element.

8. The tension torsion strap according to claim 1 , wherein the predefined pretension level is a percentage of an expected centrifugal force load.

9. A propulsor, comprising:
a hub including first and second plates respectively formed to define attachment through-holes at blade locations;
a hub casing including an interior part surrounding the hub and hub arm parts extending outwardly from the interior part at the blade locations; and
tension torsion straps in accordance with claim 1 , the tension torsion straps being extendable through the hub arm parts to connect blades with the hub at the blade locations.

10. The propulsor according to claim 9 , further comprises oblong fasteners which are extendable through the attachment through-holes and the attachment features.

11. The propulsor according to claim 9 , further comprising pretension assemblies respectively disposed at each of the hub arm parts.

12. The propulsor according to claim 11 , wherein the pretension flanges are elastically interposable between a corresponding one of the pretension assemblies and the elongate body and are configured to maintain pretension in the fibrous materials of a percentage of an expected centrifugal force load.

13. A method of applying pretension to a tension torsion strap by which a blade is connectable with a hub of a propulsor,
the hub comprising a hub casing including an interior part and hub arm parts such that the interior part surrounds the hub and the hub arm parts extend outwardly from the interior part, the method comprising:
arranging pretension assemblies in a first, non-tightening position on the hub arm parts;
connecting tension torsion straps to the hub and blades; and
adjusting the pretension assemblies to assume a second, tightening position on the hub arm parts and against pretension flanges of the tension torsion straps, wherein in the second, tightening position a jam nut of the pretension assemblies is arranged in contact with a retainer of the pretension assemblies.

14. The method according to claim 13 , further comprising securing the pretension assemblies in the second, tightening position.

Assignees

• Sikorsky Aircraft Corp

Inventors

• Darrow Jr David A
• Waldo Ron William
• Richards Joshua
• Haydel Kristopher Michael
• Halcom Lance

Classifications

• B64C27/48 Primary

  Root attachment to rotor head · CPC title

• B64C27/33

  having flexing arms · CPC title

• B64C27/10

  arranged coaxially · CPC title