Method for fastening gearbox housing components using reduced shank fasteners

Patent metadata

Field	Value
Publication number	US-11415162-B2
Application number	US-202117490420-A
Country	US
Kind code	B2
Filing date	Sep 30, 2021
Priority date	May 1, 2018
Publication date	Aug 16, 2022
Grant date	Aug 16, 2022

Abstract

A method of fastening gearbox housing components together, comprising: selecting a gearbox housing fastener comprising a straight shaft having a longitudinal axis, a first threaded portion, a single cylindrical central portion, and a second threaded portion, wherein the first and second threaded portions are separated by the cylindrical portion, wherein the cylindrical portion comprises a single reduced diameter that is less than first and second minor diameters of the first and second threaded portions, the first and second threaded portions are chamfered, and the fastener comprises a material having a tensile strength along the longitudinal axis that is greater than a sheer strength at the cylindrical portion; and fastening the gearbox housing components together with the fastener, wherein the first and third gearbox housing components are fastened with the first and second threaded portions, and the second gearbox housing component is positioned around the single cylindrical central portion.

First claim

What is claimed is:

1. A method of fastening a first, a second and a third gearbox housing components together, comprising:
selecting a gearbox housing fastener comprising a single straight shaft having a longitudinal axis, a first threaded portion, a single cylindrical central portion, and a second threaded portion, wherein the first and second threaded portions separated by the single cylindrical central portion, wherein:
the single cylindrical central portion comprises a single reduced diameter that is less than a first minor diameter of the first threaded portion and a second minor diameter of the second threaded portion,
the first and second threaded portions are chamfered to reduce friction on leading threads, and
the gearbox housing fastener comprises a material that has a tensile strength along the longitudinal axis that is greater than a sheer strength at the single cylindrical central portion; and

fastening the first, second and third gearbox housing components together with the gearbox housing fastener, wherein the first and third gearbox housing components are fastened with the first and second threaded portions, or one or more nuts attached thereto, and the second gearbox housing component is positioned around the single cylindrical central portion, wherein the gearbox housing fastener provides a clearance between the second gearbox housing component and the single cylindrical central portion of the gearbox fastener.

2. The method of claim 1 , wherein the chamfer of the first threaded portion, the second threaded portion, or both the first and second threaded portions, has between 35 and 55 degrees.

3. The method of claim 1 , wherein the straight shaft is high nickel chromium steel, chromium molybdenum steel or high-carbon steel.

4. The method of claim 1 , wherein the straight shaft is EN29, EN27, EN36 or EN39 steel.

5. The method of claim 1 , wherein the first and second threaded portions have different diameters.

6. The method of claim 1 , wherein the first and second threaded portions have different lengths.

7. The method of claim 1 , further comprising stamping an indicia stamped at a first face at a first end of the fastener, a second face at a second end of the fastener, or both.

8. The method of claim 1 , wherein the first, second and third gearbox housing components are components of a rotorcraft gearbox housing.

9. The method of claim 1 , wherein the second gearbox component is a shim.

10. A method of fastening a first, a second and a third gearbox housing components together, comprising:
fastening the first, second and third gearbox housing components together with a gearbox housing fastener, wherein:
the gearbox housing fastener comprising a single straight shaft having a longitudinal axis, a first threaded portion, a single cylindrical central portion, and a second threaded portion, wherein the first and second threaded portions separated by the single cylindrical central portion, wherein:
the single cylindrical central portion comprises a single reduced diameter that is less than a first minor diameter of the first threaded portion and a second minor diameter of the second threaded portion,
the first and second threaded portions are chamfered to reduce friction on leading threads, and
the gearbox housing fastener comprises a material that has a tensile strength along the longitudinal axis that is greater than a sheer strength at the single cylindrical central portion, and

the first and third gearbox housing components are fastened with the first and second threaded portions, or one or more nuts attached thereto, and the second gearbox housing component is positioned around the single cylindrical central portion, wherein the gearbox housing fastener provides a clearance between the second gearbox housing component and the single cylindrical central portion of the gearbox fastener.

11. The method of claim 10 , wherein the chamfer of the first threaded portion, the second threaded portion, or both the first and second threaded portions, has between 35 and 55 degrees.

12. The method of claim 10 , wherein the straight shaft is high nickel chromium steel, chromium molybdenum steel or high-carbon steel.

13. The method of claim 10 , wherein the straight shaft is EN29, EN27, EN36 or EN39 steel.

14. The method of claim 10 , wherein the first and second threaded portions have different diameters.

15. The method of claim 10 , wherein the first and second threaded portions have different lengths.

16. The method of claim 10 , further comprising stamping an indicia stamped at a first face at a first face of the fastener, a second face at a second end of the fastener, or both.

17. The method of claim 10 , wherein the first, second and third gearbox housing components are components of rotorcraft gearbox housing.

18. The method of claim 10 , wherein the second gearbox component is a shim.

Assignees

• Textron Innovations Inc

Inventors

• Poster Scott David

Classifications

• F16B33/02 Primary

  Shape of thread; Special thread-forms ({F16B25/00 takes precedence; used to remove paint or dirt layers F16B35/007, F16B37/002}; used as screw-locking device F16B39/30) · CPC title

• F16B33/04

  in view of tensile load · CPC title

• B64C27/14

  Direct drive between power plant and rotor hub · CPC title

• F16B31/04 Primary

  for maintaining {a} tensile load · CPC title

• F16H57/02

  Gearboxes; Mounting gearing therein · CPC title