Nozzle, dynamic projection device, coating method and associated repair method

Abstract

NOZZLE, DYNAMIC SPRAYING DEVICE, COATING METHOD AND ASSOCIATED REPAIR METHOD One aspect of the invention relates to a nozzle (1) comprising: - a projection gas supply duct (2), - a mixing chamber (3) for projection gas and powder material in an accelerated mixture connected, by an upstream end (31), to the projection gas supply duct (2), - a projection duct (4) for the accelerated mixture connected to a downstream end (32) of the mixing chamber (3), characterized in that: - the projection gas supply duct (2) is U-shaped with a first branch (21) oriented along a first axis (X) and a second branch (22) oriented along a second axis (Y) perpendicular to the first axis (X), the first branch (21) being connected to the upstream end (31), - the projection duct (4) for the accelerated mixture extends rectilinearly along the along the first axis (X) and comprises a projection opening (41).Figure to be published with the abstract: Figure 6.

Description

Title of the invention: Nozzle, dynamic projection device, associated coating method and repair method TECHNICAL FIELD OF THE INVENTION

[0001] The technical field of the invention is that of the repair of aircraft turbomachine parts.

[0002] The present invention relates to a nozzle, a device for dynamic projection by gas of powder material, a method of coating by dynamic projection and a method for repairing an annular contact flange of an aircraft turbomachine associated therewith. TECHNOLOGICAL BACKGROUND OF THE INVENTION

[0003] Frequently, in the context of the repair of aircraft turbomachine components, problems arise regarding the accessibility of these components. These problems exist, for example, for damage linked to wear by friction of the annular contact flange between the engine and the reverser of a turbomachine (in English "J-Ring"), for which no industrially applicable structural repair solution is known. In the event of excessive wear, this annular contact flange is replaced entirely. Such an annular contact flange 11 is shown in [Fig.l].

[0004] Replacing an aluminum J-Ring is a complex and lengthy operation. Thus, it would be beneficial to find an alternative to replacing this part that would allow it to be repaired under the wing, i.e., when the part is still installed on the turbomachine, and also allow the aircraft to be released quickly.

[0005] A dynamic spray repair method (in English “cold spray”), called recharging, can be implemented with a nozzle for spraying by direct jet of metal powder at very high speed to fill damage to the surface of worn parts.

[0006] [Fig. 2] schematically represents a conventional projection device 50 provided with a nozzle 10. This device 50 comprises, among other things, a nozzle 10 and a projection torch 60 located in the longitudinal extension of the nozzle 10. The conventional device 50 is placed opposite a surface to be recharged S, in other words to be coated with an initially powdery material. [Fig. 3] is a sectional view of the geometry of an annular contact flange of the “J-Ring” type 11 as well as a zone Z, to be repaired, of this annular contact flange 11. It can be observed, as illustrated in Figures 4 and 5, that a projection device as illustrated in [Fig. 2] cannot be inserted into this architecture without interfering with other components adjacent to the annular contact flange 11. In other words, the geometry of the “J-Ring” type annular contact flange 11 makes it impossible to use a conventional projection device 50 as illustrated in [Fig.2]. Summary of the invention

[0007] The invention offers a solution to the problems mentioned above, making it possible to overcome the aforementioned accessibility and space requirements problems in order to repair a “J-Ring” type turbomachine part under the wing, or any other type of part whose geometry does not allow the use of a conventional repair device.

[0008] A first aspect of the invention relates to a nozzle comprising: - a projection gas supply duct, - a mixing chamber for projection gas and powdered material in an accelerated mixture connected, by an upstream end, to the projection gas supply duct, - a conduit for projecting the accelerated mixture connected to a downstream end of the mixing chamber, - the projection gas supply duct being U-shaped with a first branch oriented along a first axis and a second branch oriented along a second axis perpendicular to the first axis, the first branch being connected to the upstream end, - the accelerated mixture projection conduit extending rectilinearly along the first axis and comprises a projection opening.

[0009] Thanks to the invention, it is possible to position the nozzle according to the invention so that, after integration into a gas projection device, the projection direction and the gas injection direction are different.

[0010] A second aspect of the invention relates to a device for dynamic projection by gas of powdered material comprising a nozzle as previously described and - a projection torch extending along the second axis and connected to the second branch of the projection gas supply conduit, - a powder material feed pipe connected to the mixing chamber.

[0011] Thus, the dynamic gas projection device according to the invention is more compact and can be inserted into tight spaces such as the space around a J-Ring type contact flange. Repair of such components "under" the wing, i.e., still installed on a turbomachine, is thus possible and it is no longer necessary to completely replace these components. This under-wing repair saves time compared to a complete replacement.

[0012] Advantageously, the powder material supply conduit extends along a third axis perpendicular to the first axis and the second axis.

[0013] A third aspect of the invention relates to a method of coating by dynamic projection of powder (metallic or partially metallic) on a metal part implemented by a dynamic projection device as described previously, comprising the following steps: - positioning of a surface to be coated opposite the projection opening, - high-speed gas injection into the projection torch, - injection of a powder into the powder material feed duct, - projection of the mixture formed by the high-speed gas and the powder via the projection duct onto the surface to be coated.

[0014] In the present disclosure, the powder may be metallic or partially metallic.

[0015] Advantageously, the high-speed gas is a cold gas.

[0016] In this disclosure, the term "cold gas" refers to a high-speed gas having a temperature below 750°C.

[0017] Advantageously, the powder is composed mainly of aluminum or aluminum alloy. This is particularly suitable for a part made of aluminum or aluminum alloy.

[0018] A fourth aspect of the invention relates to a method for repairing an annular contact flange of an aircraft turbomachine implemented by a dynamic projection device as described previously, comprising the following steps: • positioning a part of the annular contact flange to be repaired opposite the projection opening, • high-speed gas injection into the projection torch, • injection of a metal powder into the powder material feed duct, • projection of the mixture formed by the high-speed gas and the metal powder via the projection conduit onto said part, • the annular contact flange being installed on a turbomachine.

[0019] The invention and its various applications will be better understood by reading the following description and examining the accompanying figures. BRIEF DESCRIPTION OF THE FIGURES

[0020] The figures are presented for information purposes only and in no way limit the invention. • [Fig.l] shows a “J-Ring” type contact ring flange installed on an aircraft turbomachine reverser. • [Fig.2] shows a dynamic projection device according to the prior art. • [Fig.3] is a side view of an annular contact flange such as that of [Fig.l]. • [Fig.4] schematically represents a virtual intersection of a dynamic projection device according to the prior art with an annular contact flange of the “J-Ring” type. • [Fig.5] schematically represents another virtual intersection of a dynamic projection device according to the prior art with an annular contact flange of the “J-Ring” type. • [Fig.6] represents a nozzle according to an exemplary embodiment of the invention. • [Fig.7] represents a perspective view of a projection device dynamic according to an exemplary embodiment of the invention, in functional position. • [Fig.8] represents a profile view of the dynamic projection device of [Fig.7] in the functional position for repairing a “J-Ring” type contact ring flange. DETAILED DESCRIPTION

[0021] The figures are presented for information purposes only and in no way limit the invention. Unless otherwise specified, the same element appearing in different figures has a single reference.

[0022] A first object of the invention concerns a nozzle 1, shown in [Fig.6].

[0023] The nozzle 1 of [Fig.6] comprises: - a projection gas supply duct 2, - a mixing chamber 3 for spray gas and powdered material in an accelerated mixture connected, by an upstream end 31, to the spray gas supply conduit 2, - a projection conduit 4 of the accelerated mixture connected to a downstream end 32 of the mixing chamber 3.

[0024] The terms upstream and downstream are defined relative to the direction of propagation of the accelerated mixture, from the mixing chamber 3 towards a surface to be recharged.

[0025] The projection gas supply conduit 2 is U-shaped with a first branch 21 oriented along a first axis X and a second branch 22 oriented along a second axis Y perpendicular to the first axis X. The first branch 21 is connected to the upstream end 31.

[0026] The projection conduit 4 of the accelerated mixture extends rectilinearly along the first axis X and comprises a projection opening 41 through which the accelerated mixture is projected from the mixing chamber 3. This supply after the bends makes it possible to avoid clogging of the nozzle 2.

[0027] A second object of the invention relates to a device for dynamic projection by gas 5 of powdered material comprising a nozzle 1 such as the nozzle 1 shown in [Fig.6]. An example of this dynamic projection device 5 is shown in [Fig.7],

[0028] The dynamic projection device 5 further comprises: - a projection torch 6 extending along the second axis Y and connected to the second branch 22 of the projection gas supply conduit 2, - a powder material feed conduit 7 connected to the mixing chamber 3.

[0029] In [Fig.7] is also shown a surface to be reloaded 8, in other words to be coated with metal powder by the dynamic projection device 5. Furthermore, geometric elements 9 are also shown in [Fig.7]. These geometric elements 9 do not allow the use of a conventional projection device 50 such as that shown in [Fig.2]. Indeed, these would interfere with the projection torch 60, which could not be positioned in the extension of the nozzle 10, as already illustrated in Figures 4 and 5.

[0030] As visible in [Fig.7], the positioning of the projection torch 6 along the second axis Y, here vertical, makes it possible to insert the dynamic projection device 5 into the space available between the surface to be reloaded 8 and the geometric elements 9. Thus, the projection of metal powder onto the surface to be repaired 8 is made possible.

[0031] Advantageously, the powder material supply duct 7 is connected to the mixing chamber 3, in other words, downstream of the projection gas supply duct 2. This position of the junction between the powder material supply duct 7 and the nozzle 1 prevents deterioration of the latter. Indeed, tests have shown that a powder supply upstream of the “U” shape of the projection gas supply duct 2 causes perforation of the nozzle 1 or clogging and makes it unusable in this configuration.

[0032] [Fig.8] is a side view of the dynamic projection device 5 of [Fig.7] in the operational projection position on a “J-Ring” type annular contact flange 11. It can be seen in [Fig.8] that the geometry of the dynamic projection device 5 allows its insertion so as to position the projection conduit 4 substantially perpendicular to the inner surface of the “J-Ring” type annular contact flange 11.

[0033] A method of under-wing repair of a “J-Ring” type contact ring flange 11 having worn parts is now described.

[0034] The annular contact flange 11 is installed on an aircraft turbomachine.

[0035] The dynamic projection device 5 previously described, as illustrated in [Fig.7], is installed so that the projection conduit 4 is approximately perpendicular to a surface to be recharged, with, opposite the surface to be recharged, the projection opening.

[0036] Preferably, the projection principle is a dynamic projection by gas cold (“cold spray”).

[0037] Gas is fed into the dynamic projection device 5 via the projection torch 6 and then the projection gas supply conduit 2. The gas is, for example, nitrogen or helium. The gas is a very high-speed gas. A powder material is fed into the dynamic projection device 5 via the powder material supply conduit 7. For example, the powder material is an aluminum powder.

[0038] The gas and the powder material mix in the mixing chamber 3 to form an accelerated mixture.

[0039] The accelerated mixture is then propelled at a supersonic speed and ejected from the dynamic projection device 5 via the projection opening 41 towards the surface to be recharged. Once propelled out of the nozzle 1, the solid particles forming the accelerated mixture, after a certain projection distance, collide with the surface to be recharged. The particles pile up and form a coating on the surface to be recharged.

[0040] The projection device 5 can then be moved to repeat the reloading process in order to reload another surface of the annular contact flange.

[0041] The repair method previously described for an annular contact flange can be adapted to any other component whose shape and arrangement in a turbomachine does not allow the use of a conventional projection device, such as that of [Fig.l].

Claims

Claims

1. A device for dynamic gas projection (5) of powdered material comprising a nozzle (1) comprising: - a projection gas supply duct (2), - a mixing chamber (3) for mixing projection gas and powdered material into an accelerated mixture connected, by an upstream end (31), to the projection gas supply duct (2), - a projection duct (4) of the accelerated mixture connected to a downstream end (32) of the mixing chamber (3), - the projection gas supply duct (2) is U-shaped with a first branch (21) oriented along a first axis (X) and a second branch (22) oriented along a second axis (Y) perpendicular to the first axis (X), the first branch (21) being connected to the upstream end (31), - the projection duct (4) of the accelerated mixture extends rectilinearly along the first axis (X) and comprises a projection opening (41),and: - a projection torch (6) extending along the second axis (Y) and connected to the second branch (22) of the projection gas supply conduit (2), - a powder material supply conduit (7) connected to the mixing chamber (3), characterized in that the powder material supply conduit (7) extends along a third axis perpendicular to the first axis (X) and to the second axis (Y).,

2. Method for coating by dynamic powder projection on a metal part implemented by a dynamic powder projection device (5) according to the preceding claim, comprising the following steps: - positioning a surface to be coated opposite the projection opening (41), - injecting high-speed gas into the projection torch (6), - injecting a powder into the powder material supply conduit (7), - projecting the mixture formed by the high-speed gas and the powder via the projection conduit (4) onto the surface to be coated.

3. Coating method according to claim 2, characterized in that the

4.

5. high speed gas is cold gas. Coating method according to one of claims 2 or 3, characterized in that the powder is composed mainly of aluminum or aluminum alloy. Method for repairing an annular contact flange (11) of an aircraft turbomachine implemented by a dynamic projection device (5) according to claim 1, comprising the following steps: - positioning a part of the annular contact flange (11) to be repaired opposite the projection opening (41), - high-speed gas injection into the projection torch (6), - injection of a metal powder into the powder material supply duct, - projection of the mixture formed by the high-speed gas and the metal powder via the projection duct (4) onto said part, characterized in that the annular contact flange (11) is installed on a turbomachine.

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