AFT engine mounting link rotational stop collar

Patent metadata

Field	Value
Publication number	US-10029801-B2
Application number	US-201514828145-A
Country	US
Kind code	B2
Filing date	Aug 17, 2015
Priority date	Aug 17, 2015
Publication date	Jul 24, 2018
Grant date	Jul 24, 2018

Abstract

A method and apparatus for suspending a load is provided. A load is connected to a yoke by one or more mounting links. The mounting links are connected to the yoke by a yoke pins and to the load by load mounting pins. The mounting links are connected to the pins by spherical bearings that enable the mounting links to move relative to yoke and to the load to accommodate movement of the load, such as movement caused by thermal expansion of the load. A stop collar is arranged around the load mounting pins to limit free movement of the mounting links about a longitudinal axis so that the mounting links cannot contact the load.

First claim

What is claimed is:

1. An aircraft, comprising:
a wing that includes an engine mounting structure;
a yoke extending from the engine mounting structure, wherein the yoke includes a yoke pin;
an engine, wherein the engine includes an engine mounting pin comprising a cylindrical surface;
an engine mounting link connected to the yoke pin by a first spherical bearing and connected to the engine mounting pin by a second spherical bearing, wherein the engine mounting link can pivot about the first spherical bearing and the second spherical bearing to allow relative motion between the engine mounting pin and the yoke pin; and
a stop collar arranged around the engine mounting pin, wherein the stop collar comprises a cylindrical sleeve that fits around the cylindrical surface, and an outwardly-curved surface having a partial toroidal profile extending from an end of the cylindrical sleeve, the outwardly-curved surface arranged toward the engine mounting link, wherein the stop collar is adapted to contact the engine mounting link to limit rotation of the engine mounting link about a longitudinal axis through the first spherical bearing and the second spherical bearing.

2. The aircraft of claim 1 , wherein the engine mounting pin is connected to the engine between a first engine flange and a second engine flange, and wherein the stop collar is arranged around the engine mounting pin between the first engine flange and the engine mounting link.

3. The aircraft of claim 2 , further comprising a second stop collar arranged around the engine mounting pin between the second engine flange and the engine mounting link.

4. The aircraft of claim 1 , wherein the cylindrical sleeve includes at least one slot therethrough.

5. The aircraft of claim 1 , wherein the stop collar comprises one of: a nickel alloy, an Inconel alloy, a Waspaloy alloy, and corrosion-resistant steel.

6. The aircraft of claim 1 , wherein the engine mounting pin is arranged on the engine at a first location, wherein the aircraft further comprises an engine mount rigidly coupling the engine to the wing at a second location on the engine, and wherein the relative motion between the engine mounting pin and the yoke comprises thermal expansion of the engine between the first and second locations.

7. The aircraft of claim 1 , further comprising:
a second yoke pin;
a second engine mounting pin;
a second engine mounting link connected to the second yoke pin by a third spherical bearing and connected to the second engine mounting pin by a fourth spherical bearing, wherein the second engine mounting link can pivot about the third spherical bearing and the fourth spherical bearing to allow relative motion between the second engine mounting pin and the yoke pin; and
a second stop collar arranged around the second engine mounting pin, wherein the second stop collar is adapted to contact the second engine mounting link to limit rotation of the second engine mounting link about a longitudinal axis through the third spherical bearing and the fourth spherical bearing.

8. The aircraft of claim 1 , wherein the stop collar does not limit rotation of the engine mounting link about axes perpendicular to the longitudinal axis.

9. A suspension system for suspending a load, the suspension system comprising:
a yoke adapted to extend from a support, wherein the yoke includes a yoke pin;
a load mounting pin adapted to carry the load, the load mounting pin comprising a cylindrical surface;
a mounting link connected to the yoke pin by a first spherical bearing and connected to the load mounting pin by a second spherical bearing, wherein the mounting link can pivot about the first spherical bearing and the second spherical bearing to allow relative motion between the load mounting pin and the yoke; and
a stop collar arranged around the load mounting pin, wherein the stop collar comprises a cylindrical sleeve that fits around the cylindrical surface, and an outwardly-curved surface having a partial toroidal profile extending from an end of the cylindrical sleeve, the outwardly-curved surface arranged toward the mounting link, wherein the stop collar is adapted to contact the mounting link to limit rotation of the mounting link about a longitudinal axis through the first spherical bearing and the second spherical bearing.

10. The suspension system of claim 9 , wherein the load mounting pin is connected to the load between a first flange of the load and a second flange of the load, and wherein the stop collar is arranged around the load mounting pin between the first flange of the load and the mounting link.

11. The suspension system of claim 10 , further comprising a second stop collar arranged around the load mounting pin between the second flange of the load and the mounting link.

12. The suspension system of claim 9 , wherein the stop collar comprises one of: a nickel alloy, an Inconel alloy, a Waspaloy alloy, corrosion-resistant steel, a polyvinyl chloride (PVC) plastic polymer, and a nylon polymer.

13. A method for mounting a load from a support, the method comprising:
attaching a yoke to the support, wherein the yoke includes a yoke pin;
arranging the load relative to the yoke;
arranging a mounting link between the yoke and the load, wherein the mounting link includes a first spherical bearing arranged at a first end and a second spherical bearing arranged at a second end;
coupling the mounting link to the yoke by attaching the yoke pin to the yoke and to the first spherical bearing;
arranging a stop collar around a load mounting pin having a cylindrical surface, wherein the stop collar comprises a cylindrical sleeve that fits around the cylindrical surface, and an outwardly-curved surface having a partial toroidal profile extending from an end of the cylindrical sleeve, the outwardly-curved surface arranged toward the mounting link; and
coupling the mounting link to the load by attaching the load mounting pin to the load and to the second spherical bearing, wherein the mounting link can pivot about the first spherical bearing and the second spherical bearing to allow relative motion between the load mounting pin and the yoke, and wherein the stop collar is adapted to contact the mounting link to limit rotation of the mounting link about a longitudinal axis through the first spherical bearing and the second spherical bearing.

14. The method of claim 13 , wherein attaching the load mounting pin to the load comprises connecting the load mounting pin to a first flange of the load and a second flange of the load, and wherein arranging the stop collar around the load mounting pin comprises arranging the stop collar on the load mounting pin between the mounting link and the first flange of the load.

15. The method of claim 14 , further comprising arranging a second stop collar around the load mounting pin between the mounting link and the second flange of the load.

16. The method of claim 13 , further comprising:
arranging a second mounting link between the yoke and the load, wherein the second mounting link includes a third spherical bearing arranged at a third end and a fourth spherical bearing arranged at a fourth end;
coupling the second mounting link to the yoke by attaching a second yoke pin to the yoke and to the third spherical bearing;
arranging a second stop collar around a second load mounting pin; and
coupling the second mounting link to the load by attaching the second load mounting pin to the load and to the fourth spherical bearing, wherein the second mounting link can pivot about the third spherical bearing and the fourth spherical bearing to allo

Assignees

• Boeing Co

Inventors

• Butcher michael r
• Stanescu Adrian

Classifications

• B64D27/12 Primary

  within, or attached to, wings · CPC title

• F02C7/20

  Mounting or supporting of plant; Accommodating heat expansion or creep · CPC title

• B64D27/26

  Operations & Transport · mapped topic

• B64D2027/266

  Operations & Transport · mapped topic

• B64D27/404

  Suspension arrangements specially adapted for supporting vertical loads · CPC title