초록 ▼

An adapting part is designed to be held on a casing of a turbo-engine, partially covering the casing. The adapting part includes, in the extension of one of its axial ends, a first connector to engage with a first complementary connector associated with the casing to form a sliding connection. The a

An adapting part is designed to be held on a casing of a turbo-engine, partially covering the casing. The adapting part includes, in the extension of one of its axial ends, a first connector to engage with a first complementary connector associated with the casing to form a sliding connection. The adapting part also includes, at its other axial end, a second connector to be secured to a second complementary connector associated with the casing to form a rigid connection.

대표청구항 ▼

1. An adapting part designed to transmit forces between a tubular casing of a turbo-engine and a suspension of the turbo-engine to a pylon of an aircraft, by partially covering the tubular casing, the adapting part comprising: a hoop portion of predetermined angular sector;suspension devises arrange

1. An adapting part designed to transmit forces between a tubular casing of a turbo-engine and a suspension of the turbo-engine to a pylon of an aircraft, by partially covering the tubular casing, the adapting part comprising: a hoop portion of predetermined angular sector;suspension devises arranged on a face of the hoop portion which faces outwards and designed to connect the adapting part to the suspension;in an extension of a first axial end of the adapting part, a projecting tab extending axially from the hoop portion and configured to engage with a groove of a connecting member associated with said tubular casing to form an axial sliding connection; andat a second axial end of the adapting part, a flange configured to be secured to a flange of said tubular casing to form a rigid connection,wherein the projecting tab is entirely circular or extends circumferentially over the predetermined angular sector. 2. The adapting part as claimed in claim 1, wherein the flange is entirely circular or extends circumferentially over the predetermined angular sector. 3. The adapting part as claimed in claim 1, wherein the predetermined angular sector of the hoop portion is equal to 120°. 4. A system, comprising: an adapting part comprising: a hoop portion of predetermined angular sector;suspension devises arranged on a face of the hoop portion which faces outwards and designed to connect the adapting part to the suspension;in an extension of a first axial end of the adapting part, a projecting tab extending axially from the hoop portion; andat a second axial end of the adapting part, a flange,wherein the projecting tab is entirely circular or extends circumferentially over the predetermined angular sector:a tubular casing of a turbo-engine arranged for holding, to the tubular casing, the adapting part;a groove of a connecting member associated with said tubular casing which engages with the projecting tab of the adapting part to form an axial sliding connection in a first axial end of the tubular casing; anda flange of said tubular casing which engages with the flange of the adapting part to form a rigid connection in a second axial end of the tubular casing. 5. The system as claimed in claim 4, wherein the connecting member is fitted on one end flange of said tubular casing. 6. The system as claimed in claim 4, wherein the connecting member radially extends to one end flange of said tubular casing. 7. A suspension for a turbo-engine on a pylon of an aircraft, comprising: a front suspension bracket mounted on an intermediate casing of the turbo-engine;a rear suspension bracket mounted on an inter-turbine casing of the turbo-engine; andwherein an adapting part as claimed in claim 1 connects the rear suspension bracket to the inter-turbine casing of the turbo-engine. 8. A turbo-engine attached to a pylon of an aircraft, comprising: a front suspension bracket mounted on an intermediate casing of the turbo-engine;a rear suspension bracket mounted on an inter-turbine casing of the turbo-engine; anda system as claimed in claim 4,wherein the adapting part of the system connects the rear suspension bracket to the inter-turbine casing of the turbo-engine.