Aircraft engine attachment pylon having a rear engine attachment provided with a self-locking nut

1. An attachment pylon for an aircraft engine, the pylon comprising:

a rigid structure forming a caisson; and

a mounting system of the engine mounted fixed on the rigid structure and comprising a rear engine attachment comprising an attachment body on which is articulated at least one shackle, the rear engine attachment also comprising at least one lateral fitting arranged on either side of the caisson, each lateral fitting comprising a first portion pierced by first assembly holes to enable the lateral fitting to be fixed to the caisson, and comprising a second portion defining a fixing surface in contact with a fixing surface provided on the rear engine attachment body,

wherein the second portion includes a housing orifice receiving a self-locking nut cooperating with a fixing screw supported against the rear engine attachment body, and in any transversal section passing through the housing orifice, a longitudinal axis of the fixing screw passes through the first assembly holes.

2. An attachment pylon for an aircraft engine, the pylon comprising:

a rigid structure forming a caisson; and

a mounting system of the engine mounted fixed on the rigid structure and comprising a rear engine attachment comprising an attachment body on which is articulated at least one shackle, the rear engine attachment also comprising at least one lateral fitting arranged on either side of the caisson, each lateral fitting comprising a first portion pierced by first assembly holes to enable the lateral fitting to be fixed to the caisson, and comprising a second portion defining a fixing surface in contact with a fixing surface provided on the rear engine attachment body,

wherein the second portion includes a housing orifice receiving a self-locking nut cooperating with a fixing screw supported against the rear engine attachment body, and in any transversal section passing through the housing orifice, a longitudinal axis of the fixing screw passes through the first assembly holes,

wherein the rigid structure forming a caisson comprises two lateral panels and a longeron facing the rear engine attachment body, the longeron comprising two lateral wings mounted fixed respectively on the two lateral panels, and the first portion of each of the two lateral fittings of the rear attachment is interposed between one of the two lateral wings and its associated lateral panel.

3. The attachment pylon as claimed in claim 2 , wherein the longeron comprises a reinforcement for housing each first portion.

4. An attachment pylon for an aircraft engine, the pylon comprising:

a rigid structure forming a caisson; and

a mounting system of the engine mounted fixed on the rigid structure and comprising a rear engine attachment comprising an attachment body on which is articulated at least one shackle, the rear engine attachment also comprising at least one lateral fitting arranged on either side of the caisson, each lateral fitting comprising a first portion pierced by first assembly holes to enable the lateral fitting to be fixed to the caisson, and comprising a second portion defining a fixing surface in contact with a fixing surface provided on the rear engine attachment body,

wherein the second portion includes a housing orifice receiving a self-locking nut cooperating with a fixing screw supported against the rear engine attachment body, and in any transversal section passing through the housing orifice, a longitudinal axis of the fixing screw passes through the first assembly holes,

wherein the housing orifice receiving the self-locking nut is arranged entirely externally relative to the rigid structure forming a caisson, between the caisson and the rear engine attachment body.

5. The attachment pylon as claimed in claim 1 , wherein the caisson is formed by assembling an upper longeron, a lower longeron, two lateral panels, and transversal grooves connecting the longerons and panels, the fixing surface and the rear engine attachment body being located under and at a distance from the lower longeron.

6. The attachment pylon as claimed in claim 1 , wherein the rear engine attachment further comprises at least one vertical shear slug passing through the attachment body, the shear slug being capable of ensuring thrust force collection exerted according to a transversal direction of the pylon.

7. The attachment pylon as claimed in claim 1 , wherein the fixing surface of each of the lateral fittings of the rear engine attachment takes a form of a surface plane oriented according to a plane defined by a transversal direction and a longitudinal direction of the pylon.

8. The attachment pylon as claimed in claim 1 , wherein the rear engine attachment defines two half-fasteners each capable of ensuring thrust force collection exerted according to a vertical direction of the pylon.

9. An aircraft engine assembly comprising:

an attachment pylon as claimed in claim 1 ; and

an engine mounted fixed on the pylon.

10. An aircraft comprising at least one engine assembly as claimed in claim 9 .

11. The attachment pylon as claimed in claim 1 , wherein the lateral fitting is fixed to the caisson by bolts in said first assembly holes, and wherein said bolts are oriented perpendicular to said fixing screw.

12. The attachment pylon as claimed in claim 1 , wherein the lateral fitting is fixed to the caisson by assembly devices in said first assembly holes, said assembly devices extending along a direction oriented transversally relative to said attachment pylon, and wherein said fixing screw extend along a vertical direction.