Attachment fitted on a single side

Patent metadata

Field	Value
Publication number	US-2018238372-A1
Application number	US-201615735180-A
Country	US
Kind code	A1
Filing date	Jun 10, 2016
Priority date	Jun 11, 2015
Publication date	Aug 23, 2018
Grant date	—

Abstract

The invention concerns a fastener used to attach structural components that have aligned perforations with a nominal diameter (D), where the fastener comprises a minimum grip plane (Gmin) and a maximum grip plane (Gmax), and
A screw ( 12 ) comprising an enlarged head and a threaded portion ( 22 ); A sleeve ( 30 ) comprising an enlarged head, a cylindrical tubular body and a tapped portion ( 36 ) that engages the threaded portion ( 22 ) of the screw, where the tapped portion ( 36 ) is adjacent to an internally smooth portion of the body ( 34 ) of the sleeve. This smooth portion has a thickness (E), a non-deformable area (A) adjacent to the head of the sleeve and a deformable area (B) adjacent the non-deformable area (A). The sleeve's deformable area (B) can be deformed into a bulb ( 48 ) intended to come into contact with a blind side ( 46 ) of the structural components.

The deformable area (B) extends over a length (L) greater than a minimum length (Lmin) and less than a maximum length (Lmax), such as:
L min= D /2+2 E +( G max− G min);

L max=( E /0.092)
In particular, the invention applies to the assembly of aircraft structures.

First claim

1 . Fastener to attach structural components that have aligned perforations with a nominal diameter (D), and that have a nominal thickness that varies between a minimum thickness and a maximum thickness, with the fastener comprising a minimum grip plane (Gmin) and a maximum grip plane (Gmax), and
a screw comprising an enlarged head at one end and a threaded portion at an opposite end; a sleeve comprising an enlarged head capable of accommodating the head of the screw and intended to come into contact with the first side of the structural components, a cylindrical tubular body capable of accommodating the cylindrical shaft of the screw with clearance and a tapped portion that engages the threaded portion of the screw, where the tapped portion is adjacent to an internally smooth portion of the body of the sleeve said smooth portion having a nominal thickness (E), a non-deformable area (A) adjacent to the head of the sleeve and a deformable area (B) adjacent to the non-deformable area (A); the deformable area (B) of the sleeve has reduced resistance compared to that of the non-deformable area (A), in order to facilitate the radial deformation of the deformable portion into a bulb designed to come into contact with one side of the structural components opposite the first side; characterized in that the deformable area (B) extends across a length (L) that is greater than a minimum length (Lmin) and less than a maximum length (Lmax), where the minimum and maximum lengths (Lmin, Lmax) are defined by the following relationships:
L min= D/ 2+2 E +( G max− G min),  {1}

L max=( E/ 0.092)  {2}

where the start of the deformable area (B) is at most placed in the minimum grip plane (Gmin) of the fastener.

2 . Fastener according to claim 1 , in which the reduction in the resistance of the deformable area (B) is achieved through a local reduction in hardness.

3 . Fastener according to claim 1 , in which the reduction in the resistance of the deformable area (B) is achieved through a local reduction in the nominal thickness (E) of the tubular body.

4 . Fastener according to claim 1 , in which the deformable area (B) has a hardness lower than or equal to 300 HV.

5 . Fastener according to claim 1 , in which the deformable area has a hardness lower than or equal to 220 HV.

6 . Fastener according to claim 1 , in which the sleeve is made of A286-type stainless steel or a titanium alloy.

7 . Fastener according to claim 5 , with a diameter of 6.32 mm, a tubular body nominal thickness (E) of 0.75 mm and a deformable area (B) whose length (L) is between 6.67 mm and 8.152 mm.

8 . Fastener according to claim 5 , with a diameter of 4.80 mm, a tubular body nominal thickness (E) of 0.58 mm and a deformable area (B) whose length (L) is between 5.55 mm and 6.304 mm.

9 . Fastener according to claim 2 , in which the deformable area (B) has a hardness lower than or equal to 300 HV.

10 . Fastener according to claim 2 , in which the deformable area has a hardness lower than or equal to 220 HV.

11 . Fastener according to claim 2 , in which the sleeve is made of A286-type stainless steel or a titanium alloy.

12 . Fastener according to claim 3 , in which the sleeve is made of A286-type stainless steel or a titanium alloy.

13 . Fastener according to claim 4 , in which the sleeve is made of A286-type stainless steel or a titanium alloy.

14 . Fastener according to claim 10 , with a diameter of 6.32 mm, a tubular body nominal thickness (E) of 0.75 mm and a deformable area (B) whose length (L) is between 6.67 mm and 8.152 mm.

15 . Fastener according to claim 10 , with a diameter of 4.80 mm, a tubular body nominal thickness (E) of 0.58 mm and a deformable area (B) whose length (L) is between 5.55 mm and 6.304 mm.

Assignees

• Lisi Aerospace

Inventors

• Villet Antoine
• Naretto Nicolas
• Gay Olivier
• Pailhories Guy

Classifications

• F16B19/1072 Primary

  the pull-mandrel or the like comprising a thread and being rotated with respect to the rivet, thereby mechanically expanding and fastening the rivet (nuts fastened by riveting F16B37/067) · CPC title

• F16B19/10 Primary

  fastened by expanding mechanically · CPC title