Bending-sustaining joint and aircraft

Patent metadata

Field	Value
Publication number	US-9580163-B2
Application number	US-201414529404-A
Country	US
Kind code	B2
Filing date	Oct 31, 2014
Priority date	Nov 1, 2013
Publication date	Feb 28, 2017
Grant date	Feb 28, 2017

Abstract

The present invention relates to a bending-sustaining joint and an aircraft including the same. The bending-sustaining joint includes a body for attaching to a support structure, the body having a first end with a first bore including an internal thread portion and a non-threaded portion; a sleeve including a fitting portion which can be fit into the non-threaded portion of the first bore, a bearing portion for bearing a born member and a through hole; and a bolt member including a thread section and a bolt head which can abut an end face of the sleeve, the thread section of the bolt member being capable of passing through the through hole of the sleeve and being screwed into the internal thread portion of the first bore so as to secure the sleeve to the body.

First claim

What is claimed is:

1. A bending-sustaining joint, comprising
a body for attaching to a support structure, the body having a first end with a first bore including an internal thread portion and a non-threaded portion;
a sleeve including a fitting portion which can be fit into the non-threaded portion of the first bore, a bearing portion for bearing a borne member and a through hole;
wherein the joint further comprises a bolt member including a thread section and a bolt head which can abut an end face of the sleeve, the thread section of the bolt member being capable of passing through the through hole of the sleeve and being screwed into the internal thread portion of the first bore so as to secure the sleeve to the body; and,
wherein the support structure is a bracket formed in a wing of an aircraft, and the borne member is a link member for attaching to a control airfoil of the aircraft.

2. The bending-sustaining joint according to claim 1 , wherein the sleeve further comprises an external thread portion, and
the bending-sustaining joint further comprises a fastening assembly for fitting on the external thread portion of the sleeve so as to hold the borne member between the fastening assembly and an end face of the first end of the body.

3. The bending-sustaining joint according to claim 2 , wherein the fastening assembly comprises a lock nut and a lock washer.

4. The bending-sustaining joint according to claim 3 , wherein the lock washer comprise a first tab which can be fit in a groove formed on an outer circumference of the sleeve and a second tab which can be fit in a groove formed on an outer circumference of the lock nut.

5. The bending-sustaining joint according to claim 2 , wherein the body has a second end with a second bore, the second bore has the symmetrical configuration as that of the first bore, and
the second end of the body is provided with a second sleeve, a second bolt member and a second fastening assembly which have the same configuration as that of the sleeve, the bolt member and the fastening assembly, respectively.

6. The bending-sustaining joint according to claim 1 , wherein the fitting portion of the sleeve is positively fit into the non-threaded portion of the first bore of the body.

7. The bending-sustaining joint according to claim 6 , wherein the fitting portion of the sleeve has a flat portion, the non-threaded portion of the first bore of the body has a matched flat portion.

8. The bending-sustaining joint according to claim 7 , wherein the flat portion of the fitting portion of the sleeve is substantially perpendicular to a radial component of a load applied on the bearing portion of the sleeve by the borne member.

9. The bending-sustaining joint according to claim 1 , wherein there is a predetermined radial gap (t) between the sleeve and the bolt member.

10. The bending-sustaining joint according to claim 1 , wherein the sleeve comprises a step portion for abutting against an end face of the first end of the body.

11. The bending-sustaining joint according to claim 1 , wherein the control airfoil comprises a flap, a slat or a spoiler.

12. An aircraft comprising a bending-sustaining joint according to claim 1 .

13. A bending-sustaining joint, comprising:
a body for attaching to a support structure, the body having a first end with a first bore including an internal thread portion and a non-threaded portion;
a sleeve including a fitting portion which can be fit into the non-threaded portion of the first bore, a bearing portion for bearing a borne member and a through hole;
wherein the joint further comprises a bolt member including a thread section and a bolt head which can abut an end face of the sleeve, the thread section of the bolt member being capable of passing through the through hole of the sleeve and being screwed into the internal thread portion of the first bore so as to secure the sleeve to the body;
wherein the sleeve further comprises an external thread portion;
the bending-sustaining joint further comprises a fastening assembly for fitting on the external thread portion of the sleeve so as to hold the borne member between the fastening assembly and an end face of the first end of the body; and
wherein an adjustment washer is provided between the borne member and the first end of the body.

14. A bending-sustaining joint, comprising:
a body for attaching to a support structure, the body having a first end with a first bore including an internal thread portion and a non-threaded portion;
a sleeve including a fitting portion which can be fit into the non-threaded portion of the first bore, a bearing portion for bearing a borne member and a through hole;
wherein the joint further comprises a bolt member including a thread section and a bolt head which can abut an end face of the sleeve, the thread section of the bolt member being capable of passing through the through hole of the sleeve and being screwed into the internal thread portion of the first bore so as to secure the sleeve to the body; and
wherein a lock plate is provided between the bolt head of the bolt member and the end face of the sleeve, and the bolt head is locked relative to the sleeve via the lock plate.

15. The bending-sustaining joint according to claim 14 , wherein the lock plate is locked to the sleeve via a first lock mechanism, the bolt head is locked to the lock plate via a second lock mechanism.

16. The bending-sustaining joint according to claim 15 , wherein the first lock mechanism comprises a protrusion/recess provided on the lock plate and a recess/protrusion accordingly provided on the sleeve.

17. The bending-sustaining joint according to claim 15 , wherein the second lock mechanism comprises a first lock hole provided on the bolt head, a second lock hole provided on the lock plate and a wire member passing through the first lock hole and the second lock hole.

18. A bending-sustaining joint, comprising:
a body for attaching to a support structure, the body having a first end with a first bore including an internal thread portion and a non-threaded portion;
a sleeve including a fitting portion which can be fit into the non-threaded portion of the first bore, a bearing portion for bearing a borne member and a through hole;
wherein the joint further comprises a bolt member including a thread section and a bolt head which can abut an end face of the sleeve, the thread section of the bolt member being capable of passing through the through hole of the sleeve and being screwed into the internal thread portion of the first bore so as to secure the sleeve to the body; and
wherein the body is attached to the support structure by one of the following manner that:
i) a flange member integrally formed on the body abuts against a first side of the support structure, and a fastening assembly fit on an external thread portion on an outer circumference of the body abuts against a second side of the support structure; and
ii) two fastening assembly fit on an external thread portion on an outer circumference of the body abut against a first side and a second side of the support structure, respectively.

Assignees

• Airbus Sas

Inventors

• Sun Wei
• Chen Hong

Classifications

• F16C11/02 Primary

  Trunnions; Crank-pins (fastening crank-pins to webs, crank-pins integral with cranks F16C3/06, F16C3/22) · CPC title

• B64C9/02 Primary

  Mounting or supporting thereof · CPC title

• B64C9/14

  forming slots · CPC title

• B64C3/50

  by leading or trailing edge flaps · CPC title

• F16B5/02

  by means of fastening members using screw-thread ({F16B5/0004 takes precedence}; construction of screw-threaded connections F16B25/00 - F16B39/00) · CPC title