Rear attachment of an aircraft engine comprising break detectors
US-2018327102-A1 · Nov 15, 2018 · US
US10358227B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10358227-B2 |
| Application number | US-201715677200-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 15, 2017 |
| Priority date | Aug 15, 2017 |
| Publication date | Jul 23, 2019 |
| Grant date | Jul 23, 2019 |
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An interface apparatus including a load bearing member configured for coupling to a structure, and an attachment member coupled to the load bearing member, wherein the load bearing member is configured to react loads, from the attachment member to the structure, in at least a first direction while simultaneously providing free movement of the attachment member in at least a second direction.
Opening claim text (preview).
What is claimed is: 1. An interface apparatus comprising: a load bearing member configured for coupling to a structure, the load bearing member comprising a baseplate having first locking members, and a bearing housing having second locking members that are configured to engage the first locking members; and an attachment member coupled to the load bearing member; wherein the load bearing member is configured to react loads, from the attachment member to the structure, in at least a first direction while simultaneously providing free movement of the attachment member in at least a second direction, and the first locking members and the second locking members each comprise a series of protruding members. 2. The interface apparatus of claim 1 , wherein the load bearing member has a longitudinal axis and a lateral axis and the load bearing member is configured to react loads, from the attachment member to the structure, along at least the lateral axis. 3. The interface apparatus of claim 2 , wherein the load bearing member provides free movement of the attachment member in at least one direction transverse to the longitudinal axis. 4. The interface apparatus of claim 2 , wherein the load bearing member provides free movement of the attachment member along at least the longitudinal axis. 5. The interface apparatus of claim 2 , wherein the load bearing member provides free pivoting movement of the attachment member about the longitudinal axis. 6. The interface apparatus of claim 1 , wherein: the baseplate is configured for coupling to the structure; the bearing housing is coupled to the baseplate; and the load bearing member further comprises a bearing, the attachment member being coupled to the bearing; wherein the bearing housing is configured to house the bearing so as to constrain the bearing in at least the first direction and to provide free movement of the bearing in at least the second direction. 7. The interface apparatus of claim 1 , wherein the attachment member is configured for coupling with a secondary structure. 8. An interface apparatus comprising: a bearing housing configured for coupling to a structure and having a longitudinal axis; and a barrel bearing having a cylindrical body, extending along the longitudinal axis of the bearing housing, and an attachment member coupled thereto; wherein the bearing housing is configured to house the barrel bearing so as to constrain the barrel bearing in at least a first direction and to provide free movement of the barrel bearing in at least a second direction along the longitudinal axis, wherein the bearing housing, housing the barrel bearing, is configured to react loads, from the attachment member to the structure, in at least the first direction while simultaneously providing free movement of the attachment member in at least the second direction; wherein the barrel bearing includes a bearing aperture and the attachment member is slidably disposed within the bearing aperture. 9. The interface apparatus of claim 8 , wherein the bearing aperture is configured to guide linear movement of the attachment member relative to the barrel bearing. 10. The interface apparatus of claim 8 , wherein the barrel bearing is configured to provide the attachment member with at least three degrees of freedom movement relative to the bearing housing. 11. The interface apparatus of claim 8 , wherein the bearing housing includes a first aperture, where the barrel bearing is slidably disposed within the first aperture. 12. The interface apparatus of claim 8 , wherein the bearing housing includes a second aperture having at least one stop surface, the at least one stop surface being configured to limit movement of the attachment member in at least the second direction. 13. The interface apparatus of claim 12 , wherein the at least one stop surface is configured to limit movement of the attachment member in at least the second direction along the longitudinal axis of the bearing housing. 14. The interface apparatus of claim 8 , wherein the attachment member rotates relative to the barrel bearing. 15. The interface apparatus of claim 8 , wherein the barrel bearing is configured to provide at least one degree of freedom pivoting movement of the attachment member relative to the bearing housing. 16. A method comprising: reacting loads, from an attachment member to a structure, in at least a first direction with a load bearing member coupled to the structure where the attachment member is coupled to the load bearing member; constraining a barrel bearing in a bearing housing of the load bearing member in at least the first direction, the barrel bearing having a cylindrical body that extends along a longitudinal axis of the load bearing member; simultaneously providing free movement of the attachment member, with the load bearing member, in at least a second direction; and guiding, with an aperture of the barrel bearing, linear movement of the attachment member relative to the barrel bearing. 17. The method of claim 16 , wherein the load bearing member has the longitudinal axis and a lateral axis, the method further comprising reacting loads, with the load bearing member, from the attachment member to the structure, along at least the lateral axis. 18. The method of claim 17 , further comprising providing, with the load bearing member, free pivoting movement of the attachment member about the longitudinal axis. 19. The method of claim 16 , wherein the bearing housing is coupled to a baseplate and the baseplate is coupled to the structure, the method further comprising: providing free movement of the barrel bearing in at least the second direction, where the attachment member is coupled to the barrel bearing. 20. The method of claim 19 , wherein the load bearing member has the longitudinal axis and a lateral axis, the method further comprising reacting loads, with the load bearing member, from the attachment member to the structure, along at least the lateral axis.
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