FIELD OF THE INVENTION
This invention relates to flange connections and seals between structures in general, and between fluid communication and containment structures in particular.
BACKGROUND OF THE INVENTION
Connection flanges normally provide a planar interface between structural and/or fluid communication and containment elements. However, a planar interface does not provide self-centering. Centering has been achieved with body-bound bolts with tight clearance, but this can cause stuck bolts and differential expansion stress. Spigots have been used in which a component has an annular lip that is received in the end of an opposed component for centering. Standardized planar flange interfaces also allow unauthorized third party components to be used in an assembly.
BRIEF DESCRIPTION OF THE DRAWINGS
The invention is explained in the following description in view of the drawings that show:
FIG. 1 is a sectional side view of a prior art gas turbine combustor with an outer casing attached to an engine casing by a bolted flange connection.
FIG. 2 is a sectional side view of a bolted flange connection with a curved interface according to aspects of an embodiment of the invention.
FIG. 3 is a sectional side view of a bolted flange connection with a curved interface and a ring seal according to aspects of an embodiment of the invention.
FIG. 4 is a view of the embodiment of FIG. 3 with the flanges separated.
FIG. 5 is a perspective view of exemplary geometry of toric flanges.
FIG. 6 is a perspective view of exemplary geometry of a flange around a non-circular periphery of a component.
FIG. 7 is a sectional side view of a pilot fuel nozzle bolted by a flange to a combustor head.
DETAILED DESCRIPTION OF THE INVENTION
FIG. 1 shows a can-annular type combustor 20 of a gas turbine engine. The combustor has an outer casing 22, which is attached to another structure such as an engine casing 24 by a bolted flange connection 26 between a first flange 28 and a second flange 30 with a planar interface 32. The combustor may have a pilot nozzle 36 attached to a combustor head 38 by a bolted flange 40. Such prior art bolted flange connections 26, 40 may be improved by designs taught below.
FIG. 2 shows a connection 26A between a first flange 28A and a second flange 30A with a curved interface 32A, which may be toric. “Toric” herein means an annular portion of a surface of revolution of a curve—for example an annular portion of a surface of revolution of a circle or ellipse about an axis in the plane of the circle or ellipse that does not intersect the circle or ellipse. A compliant gasket (not shown) may be provided in the interface 32B as known in the art of engine gaskets.
FIG. 3 shows a flange connection 26B with a curved interface 32B between a first flange 28B and a second flange 30B. This embodiment has a ring seal 42 in a seal slot 44 in the first or second flange.
The curved interface provides the following benefits:
a) Greater contact area than a corresponding planar interface with the same inner and outer peripheries. This decreases fluid leakage by increasing resistance to flow by increasing the length of the leakage path.
b) Self centering and alignment of the opposed structures 22, 24, without the need for spigots or body-centered bolts. Centering and alignment is important for reliable, repeatable assembly of gas turbine engine components for maintenance.
c) Exclusion of outdated or unauthorized replacement parts that do not have the matching curved contact surface.
FIG. 4 shows flanges 28B, 30B separated for clarity. Each flange has a curved primary contact surface 29B, 31B. “Primary” means a contact surface of the interface 32B (FIG. 3), as distinct from a secondary surface such as the ring seal slot 44, which may also be toric. The primary contact surfaces 29B, 31B are curved C as seen in an axial section of each flange as shown. “Axial” means related to the rotation axis of a surface of revolution 29B, 31B. An axial section plane is a plane of the axis of revolution of the surface 29B, 31B. The curve C defining a primary contact surface in an axial section may be a circular arc with a span angle A of at least 40 degrees or at least 50 degrees in some embodiments. Whether or not the curve C is circular it may have a maximum departure D, from a straight line L drawn between the ends 34, 35 of the curve C, of at least 5% of the length of the line L, or at least 10% in some embodiments.
FIG. 5 shows an exemplary geometry of toric primary contact surfaces 29C, 31C of opposed flanges 28C, 30C with respective sets of bolt holes 46, 48. Bolt holes on one of the flanges may be threaded as shown in FIG. 4, or the bolt holes on both flanges may be unthreaded as in FIG. 5. Axes 50, 52 of each respective primary contact surface 29C, 31C are shown. These axes may coincide with an axis of each respective component 54, 56 if the component is a solid of revolution.
FIG. 6 shows exemplary geometry of a flange embodiment 30D on a component 58 that is not a solid of revolution. Whether or not a component is a solid of revolution, the flange extends around a perimeter of the component, and the primary contact surface 31D of the flange is defined by a curve C in a section plane P transverse to a direction of the flange along the perimeter. The perimeter 60 may be at an end of a component as shown or it may be intermediate the ends as later shown. The curve C may have a maximum departure, from a straight line drawn between the ends of the curve, of at least 5% of the length of the line, or at least 10% in some embodiments. In some embodiments, the curve may be a circular arc with a span angle of at least 40 degrees, or at least 50 degrees in some embodiments.
FIG. 7 is a sectional side view of a pilot fuel nozzle 36 bolted by a toric flange 28E to a combustor head 38. The toric interface 32E providing precise centering and alignment of the pilot fuel nozzle extending into the combustor. Any flange embodiment herein may extend around a component intermediate the ends of the component as shown here. It is not limited to extending from an end of a component.
While various embodiments of the present invention have been shown and described herein, it will be obvious that such embodiments are provided by way of example only. Numerous variations, changes and substitutions may be made without departing from the invention herein. Accordingly, it is intended that the invention be limited only by the spirit and scope of the appended claims.
Patent Application
20160123231
