This application is based upon and claims the benefit of priority from British Patent Application Number 1615328.0 filed 9 Sep. 2016, the entire contents of which are incorporated herein by reference.
The present disclosure relates to an articulating coupling assembly of the sort used to secure an end of a pipe or shaft to a fixed component whilst allowing some freedom of axial and/or angular movement of the pipe or shaft with respect to the fixed component. More particularly, but without limitation, the invention relates to such articulating couplings used to secure an oil service pipe of a gas turbine engine to a support structure within the engine.
In gas turbine engines, there is a need to feed fluids such as oil to various moving components within the engine. This presents a need for feed and scavenger pipes extending between a fluid source and these components, often radially across the engine. Such pipes are retained in position by being coupled to support structures provided within the engine. Due to large thermal differences arising in its environment during the operation of the engine, the pipe must be allowed to move radially and articulate relative to the engine support structures throughout engine operation. It is known to achieve this by inclusion of a spherical bearing adjacent where an end of the pipe is coupled to a support structure. The spherical bearing allows some articulation between the pipe and the support structure to compensate for differential thermal resizing between connected elements. To protect the pipe from consequences of torque on the pipe applied during the installation of a connecting pipe, it is known to use a coupling which incorporates an anti-rotation feature.
It is understood that large temperature differences and relative displacements acting on the pipe may be a cause of wear on the location and anti-rotation features of the coupling assembly. Such wear can become problematic if it results in dislocation or leakage of fluid from coupled pipes.
A known articulating coupling assembly is illustrated in
The spherical bearing 5 permits a small degree of relative angular and axial movement between the pipe end 1 and the flanged collar 2 to accommodate thermal resizing during thermal cycles arising in the environment of the pipe end 1, for example due to the operation of a gas turbine engine in which the pipe is located. Bolts (not shown) may be used to secure the flange 3 to a support structure (not shown) by means of bolt holes 3a. The support structure may be a circumferential casing arranged around an axis of a gas turbine engine in which the pipe is located. The end feed fitting 4 is configured to fit snugly within the bore of the flanged collar 2 and may incorporate a seal for preventing leakage from the pipe end through the flanged collar 2 in a direction distal from the flange 3.
The present invention provides an alternative articulating coupling assembly with some advantages over the described known arrangement.
In accordance with the present disclosure there is provided an articulating coupling assembly for coupling a pipe end to a support structure, the assembly comprising; a pipe end fitting configured for fitting over a free end of a pipe, the fitting equipped with a spherical bearing,
the spherical bearing having a maximum diameter not greater than the pipe end fitting,
a flanged collar configured to receive the pipe end fitting in a snug fit,
a radially outer wall of the spherical bearing having one or more slots extending along the bearing in a direction parallel to the axial direction of said pipe,
a radially inner wall of the flanged collar having one or more radially inwardly protruding dogs proportioned to be received snugly in the one or more slots of the radially outer wall of the spherical bearing.
The number of slots in the spherical bearing may be greater than or equal to the number of dogs provided on the flanged collar. The spherical bearing may have a circumferential array of slots. The slots may be equally spaced. For example, the number of dogs is a factor of the number of slots. The dogs may be equally spaced around the circumference of the flanged collar. In one embodiment, there are 3 equally spaced dogs and 9 equally spaced slots and the dogs are arranged to engage in every third slot.
The assembly may accommodate a single skinned pipe. Alternatively the assembly may accommodate a double skinned pipe. Where a double skinned pipe is accommodated, the spherical bearing may be joined with the inner skin, the outer skin may have an inner diameter approximately equal to the maximum outer diameter of the spherical bearing. In the latter case, by providing more slots than dogs, a continuous channel can be provided between inner and outer skins of a double skinned pipe across the coupling.
A support structure to which the assembly is coupled may comprise an orifice through which the coupling assembly is received.
The assembly may further comprise a long reach nut configured to be insertable through the flanged collar and connect with the pipe end fitting. A connecting pipe may be received in the long reach nut whereby to connect pipes on opposite sides of a wall of the support structure.
By way of example, an embodiment of an articulating coupling assembly in accordance with the invention will now be described with reference to the accompanying figures in which;
As can be seen in
A long reach nut 39 is inserted from the flanged end of the flanged collar 33 and threads onto the pipe end fitting 34. The long reach nut 39 is proportioned to provide a small clearance between it and other adjacent components. A connecting pipe (not shown) may be connected by means of this long reach nut 39, for example with an inner skin inserted into the bore of the long reach nut 39 and an outer skin locating around an outer wall of the long reach nut 39.
As stated,
In an alternative arrangement, the spherical bearing may be arranged around both skins of the double skinned pipe and the coupling assembled as if the outer skin were a single skin pipe.
Whilst specific examples herein refer to feed and scavenger pipes for use in a gas turbine engine, the skilled person will understand the assembly of the invention has much wider application for coupling pipes of a range of sizes and uses and in a range of operating environments. The coupling assembly of the invention is, however, of particular value in gas turbine engine applications since it is resilient to the high forces and temperatures encountered therein and is more compact and lightweight than prior known arrangements used in such environments.
It will be understood that the invention is not limited to the embodiments above-described and various modifications and improvements can be made without departing from the concepts described herein and claimed in the appended claims. Except where mutually exclusive, any of the features may be employed separately or in combination with any other features and the disclosure extends to and includes all combinations and sub-combinations of one or more features described herein.
Number | Date | Country | Kind |
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1615328.0 | Sep 2016 | GB | national |