Injection tube for connecting a cold plenum to a hot chamber

Information

  • Patent Grant
  • 6233915
  • Patent Number
    6,233,915
  • Date Filed
    Monday, March 23, 1998
    26 years ago
  • Date Issued
    Tuesday, May 22, 2001
    23 years ago
Abstract
An injection tube for connecting a plenum to a combustion chamber includes a first mouth having a longitudinal axis and adapted for insertion into a cold plenum port or other component and a second mouth having a longitudinal axis and adapted for insertion into a hot chamber port or other component. To accommodate flexural, axial and torsional forces caused by differential thermal expansion between the two components, the mouths of the tube are configured to have multiple degrees of freedom within each corresponding port while maintaining port-mouth seal integrity. In an illustrative embodiment, the first mouth outer surface shape allows free slip of the first mouth parallel to the first mouth longitudinal axis, as well as rotation of the first mouth about both the first mouth longitudinal axis and a first mouth outer surface transverse axis. Mounted on the outer surface of the tube is a rocker arm adapted to engage a pivot mounted on the chamber outer surface or to engage the chamber outer surface itself. The rocker engagement allows rotation of the second mouth about a second mouth transverse axis while constraining axial movement of the tube, thereby preventing the second mouth from disengaging the chamber port.
Description




FIELD OF THE INVENTION




The present invention relates to turbine engine componentry, specifically to a means for conveying a working fluid from one component to another.




BACKGROUND OF THE INVENTION




In engines of varying types, there is frequently the need for a conduit by which a gas or other fluid is conveyed from one component to another. In gas turbine engines, for example, the air exiting a compressor is collected in a plenum and mixed with fuel. This air-fuel mixture then flows through a venturi or other conduit to a combustion chamber where the mixture is ignited to form a hot gas. Because most engineering materials expand when heated, the hot gas production causes the combustion chamber to enlarge. The plenum, which is not exposed to the hot combustion gases, does not experience thermally-related growth to the extent experienced by the combustion chamber. In gas turbine engine modules such as that disclosed in U.S. Pat. No. 5,572,862 to Mowill, (“the '862 patent”) the ideal injector tube-chamber configuration is such that the tube enters the chamber in a substantially tangential manner. In addition, the tube must be substantially fixed at both the plenum and combustion chamber ends in order to effectively serve as a conduit. In such an arrangement wherein the thermal growth of the combustion chamber is substantially greater than that of the plenum, the tube will likely experience significant axial and flexural stresses and corresponding strains. In attempting to prevent tube strain induced pressure against the chamber from puncturing the chamber lining, one could theoretically provide clearance at the interfaces between the tube and chamber and the tube and plenum. However, such clearances would necessarily result in air leakage, thereby reducing the efficiency of the engine. Accordingly, what is needed is a conduit connecting one component to another component that is designed to accommodate a substantial disparity in thermal growth between those two components while simultaneously maintaining interface seal integrity.




SUMMARY OF THE INVENTION




According to the principles of the present invention, an injection tube or similar conduit includes a first mouth adapted for insertion into a plenum port or other component and a second mouth adapted for insertion into a hot chamber port or other component. To accommodate flexural, axial and torsional forces caused by the differential thermal expansion between the two components, the mouths of the tube are configured to have multiple degrees of freedom within each corresponding port while maintaining port-mouth seal integrity.




In one embodiment of the invention, the first mouth, the entry plane of which may or may not be vertically disposed, includes a fastening element such as an outer surface raised and rounded about the entire perimeter of the mouth and adapted to fit within a cylindrical sleeve incorporated into the plenum port to create what is hereinafter referred to as a spherical slip coupling. The first mouth outer surface shape allows free slip of the first mouth parallel to the first mouth longitudinal axis, as well as rotation of the first mouth about both the first mouth longitudinal axis and a first mouth outer surface transverse axis. The second tube mouth, the exit plane of which may or may not be vertically disposed, is adapted to rotatably engage the chamber port about a transverse axis to create what is hereinafter referred to as an eccentric spherical coupling. Mounted on the outer surface of the tube is a fastening element such as a rocker arm adapted to engage another fastening element such as a pivot mounted on the chamber outer surface or to engage the chamber outer surface itself. The rocker engagement allows rotation of the second mouth about a second mouth transverse axis while constraining axial movement of the tube, thereby preventing disengagement of the second mouth from the chamber port. Alternatively, the second mouth includes an outer surface with a fastening element such as contoured convex and concave portions adapted to rotatably engage a corresponding fastening element such as contoured concave and convex portions incorporated in the chamber port surface. The second mouth outer surface shape allows rotation of the second mouth about a second mouth transverse axis while constraining axial movement of the tube, thereby preventing disengagement of the second mouth from the chamber port.




It is important to note that the utility of the principles of the instant invention is not limited to the engine module disclosed in the '862 patent. The instant invention can be implemented by any combustion-type engine wherein exists differential expansion of one component relative to another.











BRIEF DESCRIPTION OF THE DRAWING




The invention will be better understood from a reading of the following detailed description taken in conjunction with the drawing figures in which like reference designators are used to designate like elements, and in which:





FIG. 1

is a side view of an injection tube connecting a plenum to an annular combustion chamber according to the prior art;





FIG. 2

is a side view of an injection tube incorporating features of the present invention;





FIG. 3

is a cross-sectional view of the interface between an injection tube and a plenum incorporating features of the present invention;





FIG. 4

is a cross-sectional view of the interface between an injection tube and an annular combustion chamber incorporating features of the present invention; and





FIG. 5

is a cross-sectional view of an alternative embodiment of an interface between an injection tube and an annular combustion chamber.











DETAILED DESCRIPTION




The drawing figures are intended to illustrate the general manner of construction and are not to scale. In the description and in the claims the terms left, right, front and back and the like are used for descriptive purposes. However, it is understood that the embodiment of the invention described herein is capable of operation in other orientations than is shown and the terms so used are only for the purpose of describing relative positions and are interchangeable under appropriate circumstances.





FIG. 1

shows, in general, a fluid injection system typical to many combustion-type engine applications and, in particular, an annular combustor system such as is contemplated by the '862 patent. In gas turbine engines implementing such an annular combustor system, the air exiting a compressor is collected in a plenum or other upstream component


10


and mixed with fuel. The resultant air-fuel mixture then flows through an injection tube


20


and into a combustion chamber


30


where the mixture is ignited to form a hot gas. The tube


20


is fixed at each end and enters the chamber


30


in a substantially tangential manner. As discussed more fully in the '862 patent, the purpose of this tangential entry is to create within the chamber


30


a radial swirl of the air-fuel mixture thereby promoting maximal residence time of the mixture within the chamber and, consequently, maximal quantitative mixture combustion and reduced emissions. The production of hot gas within chamber


30


causes chamber


30


to enlarge. The plenum


10


, which is not exposed to the hot ignition gases, does not experience thermally related growth to the extent experienced by chamber


30


. Growth-related movement of the chamber


30


relative to the plenum


10


imparts to the tube


20


significant axial and flexural stresses and strains that may in turn rupture the plenum


10


and/or chamber


30


.





FIG. 2

shows a hollow injection tube


40


incorporating features of one embodiment of the present invention. Tube


40


has an exterior surface


51


and an interior surface (not shown). Tube


40


includes a first mouth


60


and a second mouth


70


, each of which are defined by a respective perimeter formed from and part of exterior surface


51


at each end of tube


40


. First mouth


60


, the entry plane


61


of which is vertically disposed, includes a longitudinal axis


52


and an outer surface


90


raised and rounded, about the entire perimeter of first mouth


60


. Second mouth


70


includes a longitudinal axis


50


and an outer surface


100


having surface portions


100


A and


100


B. The contour of surface


100


may be ruled or curved, depending on the particular embodiment. The exit plane


71


of second mouth


70


is adapted to conform to the annular surface of a combustion chamber. Rocker tab


80


is formed upon exterior surface


51


. The function of rocker tab


80


is described in further detail hereinafter.





FIG. 3

illustrates the connection between injection tube


40


and plenum


10


wherein first mouth


60


is shown inserted into plenum port


110


to create what is referred to herein as a spherical slip joint. Outer surface


90


is adapted to slidably engage the inner surface


119


of cylindrical sleeve


120


incorporated into the plenum port


110


. To accommodate axial, flexural and torsional forces imparted to the tube


40


, outer surface


90


is so engaged with cylindrical sleeve


120


as to allow free slip of the mouth


60


parallel to longitudinal mouth axis


52


, rotation of the mouth


60


about any axis orthogonal to mouth axis


52


passing through the center of diameter


122


defined by surface


90


, and rotation of the mouth


60


about longitudinal mouth axis


52


.





FIG. 4

illustrates the connection between injection tube


40


and a combustion chamber


30


wherein second mouth


70


is shown in fluid communication with chamber port


71


. Outer second mouth surface portions


100


A,


100


B integral to tube exterior surface


51


are rotatably engaged with chamber port surface portions


130


A,


130


B which is formed from and part of chamber exterior surface


131


. The engagement of surface portions


100


A,


100


B with chamber port surface portions


130


A,


130


B causes tube


40


to be freely rotatable about an axis


200


that is eccentric to second mouth


70


. Surface portion


100


A, which is closest to axis


200


is concave to engage a correspondingly convex surface portion


130


A. Surface portion


100


B, which is distal to axis


200


is convex to engage a correspondingly concave surface portion


130


B. By forming surface portions


100


B and


130


A,


130


B to have curved profiles, tube


40


can only be engaged to chamber


30


by first engaging upper surface portions


100


A,


130


A and rotating tube


40


downward about axis


200


until surface portions


100


B and


130


B engage. Once engaged, tube


40


is constrained to rotate about axis


200


as constrained by surface portions


100


A,


100


B,


130


A,


130


B while not disengaging from port


71


. This form of coupling is hereinafter referred to as an eccentric spherical coupling.





FIG. 5

illustrates an alternative eccentric spherical coupling between injection tube


40


and a combustion chamber


30


wherein second mouth


70


is shown in fluid communication with chamber port


71


. Outer second mouth ruled surface


100


is integral to tube exterior surface


51


and is slidably engaged with chamber port ruled surface


130


which is formed from and part of chamber exterior surface


131


. Surfaces


100


and


130


do not completely constrain tube


40


axially. Accordingly, at least one rocker tab


80


is formed along the exterior surface


51


that may biasingly engage the chamber exterior surface


131


itself or, in the embodiment shown, engage a pivot tab


140


formed on the chamber exterior surface


131


. Preferably, the engaging surfaces of rocker tab


80


and pivot tab


140


are curved, but may also be square, rectangular or otherwise geometrically configured. To accommodate flexural forces imparted to the tube


40


, rocker tab


80


is so engaged by the pivot tab


140


as to prevent disengagement of the mouth


70


from the port surface


130


. The engagement of pivot tab


140


by rocker tab


80


also allows rotation of mouth


70


about an axis normal to an axis defined by the radial force vector applied to the tube


40


by the chamber


30


somewhat independent of the constraints afforded by ruled surfaces at


100


,


130


. In any embodiment of the present invention, supplementary sealing means may be used as needed to reduce leakage at the interface of second mouth


70


and chamber port


71


.




Although the invention has been described in terms of the illustrative embodiment, it will be appreciated by those skilled in the art that various changes and modifications may be made to the illustrative embodiment without departing from the spirit or scope of the invention. It is intended that the scope of the invention not be limited in any way to the illustrative embodiment shown and described but that the invention be limited only by the claims appended hereto.



Claims
  • 1. A fluid injection apparatus for connecting a plenum having a plenum port to a chamber having a chamber port, the apparatus comprising:a conduit having an exterior surface, a first mouth defined by a perimeter formed from said exterior surface and adapted for insertion into and fluid communication with the plenum port, and a second mouth defined by a perimeter formed from said exterior surface and adapted for operative connection and fluid communication with the chamber port; said first mouth having a partially spherical surface adapted to engage the plenum port; and said second mouth is configured to engage the chamber port of the chamber to permit rotation about a transverse axis eccentric of said conduit.
  • 2. The apparatus of claim 1, wherein:said first mouth comprises a spherical slip coupling configured to allow free slip within the plenum port of said first mouth parallel to a longitudinal axis of said conduit, rotation within the plenum port of said first mouth in any plane perpendicular to the plenum port and rotation within the plenum port of said first mouth about said longitudinal axis.
  • 3. The apparatus of claim 1 wherein said second mouth further comprises a rocker tab, said rocker tab being configured for biased engagement with a chamber exterior surface.
  • 4. The apparatus of claim 1 wherein said second mouth comprises a concave surface proximal said transverse eccentric axis and a convex surface distal said transverse eccentric axis.
  • 5. A fluid injection apparatus for connecting a plenum to a chamber comprising:a hollow substantially cylindrical tube having an exterior surface defining a first mouth, said first mouth adapted for insertion into and fluid communication with the plenum, said exterior surface further defining a second mouth adapted for operative connection and fluid communication with the chamber; said first mouth having a longitudinal axis and including an outer surface raised and rounded about an exterior surface of said first mouth and adapted for insertion into the plenum port, said outer surface configured to allow free slip within the plenum port of said first mouth parallel to said longitudinal axis, said outer surface configured to allow rotation within the plenum port of said first mouth in any plane perpendicular to the plenum port, said outer surface configured to allow rotation within the plenum port of said first mouth about said longitudinal axis; and a rocker tab disposed along said exterior surface proximal said second mouth, said rocker tab engaging the chamber exterior surface to prevent said second mouth from disengaging the chamber port.
  • 6. An apparatus for receiving and combusting a fluid mixture formed in a plenum having a plenum port comprising:a chamber having an exterior surface, at least one port formed from said exterior surface, and at least one first fastening element formed from said exterior surface; at least one conduit having an exterior surface, a first mouth defined by a perimeter formed from said conduit exterior surface and adapted for insertion into and fluid communication with the plenum, and a second mouth defined by a perimeter formed from said conduit exterior surface and in fluid communication with said chamber port; said first mouth having a longitudinal axis and including a second fastening element adapted for insertion into and multiple degrees of freedom within the plenum port; and a third fastening element formed from said conduit exterior surface, said third fastening element pivotally connected with said first fastening element thereby preventing disconnection of said second mouth from said chamber port.
  • 7. The apparatus of claim 6 wherein said first fastening element comprises a pivot tab.
  • 8. The apparatus of claim 6 wherein said first fastening element comprises a contoured chamber port surface.
  • 9. The apparatus of claim 6 wherein:said second fastening element is configured to allow free slip within the plenum port of said first mouth parallel to said longitudinal axis; said second fastening element is configured to allow rotation within the plenum port of said first mouth in any plane perpendicular to the plenum port; and said second fastening element is configured to allow rotation within the plenum port of said first mouth about said longitudinal axis.
  • 10. The apparatus of claim 9 wherein said second fastening element further comprises an outer surface of said first mouth, said first mouth outer surface being raised and rounded about the entirety of said first mouth perimeter.
  • 11. The apparatus of claim 6 wherein said third fastening element comprises a rocker tab.
  • 12. The apparatus of claim 6 wherein said third fastening element comprises a contoured second mouth outer surface.
  • 13. An apparatus for receiving and combusting a fluid mixture formed in a plenum having a plenum port comprising:an annular combustion chamber having an exterior surface, a port formed from said exterior surface, and a pivot tab formed from said exterior surface; a hollow substantially cylindrical tube having an exterior surface, a first mouth defined by a perimeter formed from said cylindrical tube exterior surface and adapted for insertion into and fluid communication with the plenum, and a second mouth defined by a perimeter formed from said cylindrical tube exterior surface and in fluid communication with said chamber port; said first mouth having a longitudinal axis and including an outer surface raised and rounded about the entirety of said first mouth perimeter and adapted for insertion into the plenum port, said outer surface configured to allow free slip within the plenum port of said first mouth parallel to said longitudinal axis, said outer surface configured to allow rotation within the plenum port of said first mouth in any plane perpendicular to the plenum port, said outer surface configured to allow rotation within the plenum port of said first mouth about said longitudinal axis; and a rocker tab disposed along said cylindrical tube exterior surface, said rocker tab pivotally connected with said pivot tab thereby preventing disconnection of said second mouth from said chamber port.
  • 14. A method of receiving for combustion fluid formed in a plenum having a plenum port comprising the steps of:forming a chamber having an exterior surface, a port formed from said exterior surface, and a first fastening element formed from said exterior surface; forming a conduit having an exterior surface, a first mouth having a longitudinal axis and defined by a perimeter formed from said conduit exterior surface, and a second mouth defined by a perimeter formed from said conduit exterior surface; forming a second fastening element from said first mouth, said second fastening element adapted for insertion into and multiple degrees of freedom within the plenum port; forming a third fastening element from said conduit exterior surface, said third fastening element configured to engage said first fastening element thereby preventing disconnection of said second mouth from said chamber port; inserting said first mouth into the plenum port; and placing said second mouth into fluid communication with said chamber port thereby engaging said third fastening element with said first fastening element.
  • 15. A method in accordance with claim 14 wherein said first fastening element comprises a pivot tab.
  • 16. A method in accordance with claim 14, wherein:said second fastening element is configured to allow free slip within the plenum port of said first mouth parallel to said longitudinal axis; said second fastening element is configured to allow rotation within the plenum port of said first mouth in any plane perpendicular to the plenum port; and said second fastening element is configured to allow rotation within the plenum port of said first mouth about said longitudinal axis.
  • 17. A method in accordance with claim 16, wherein said second fastening element further comprises an outer surface of said first mouth, said first mouth outer surface being raised and rounded about the entirety of said first mouth perimeter.
  • 18. A method in accordance with claim 14 wherein said third fastening element further comprises a rocker tab.
  • 19. A method of receiving for combustion fluid formed in a plenum having a plenum port comprising the steps of:forming an annular combustion chamber having an exterior surface, a port formed from said exterior surface, and a pivot tab formed along said exterior surface; forming a hollow substantially cylindrical tube having an exterior surface, a first mouth having a longitudinal axis and defined by a perimeter formed from said cylindrical tube exterior surface, and a second mouth defined by a perimeter formed from said cylindrical tube exterior surface; forming from said first mouth an outer surface raised and rounded about the entirety of said first mouth perimeter and adapted for insertion into the plenum port, said outer surface configured to allow free slip within the plenum port of said first mouth parallel to said longitudinal axis, said outer surface configured to allow rotation within the plenum port of said first mouth in any plane perpendicular to the plenum port, said outer surface configured to allow rotation within the plenum port of said first mouth about said longitudinal axis; forming a rocker tab from said tube exterior surface, said rocker tab configured to engage said pivot tab thereby preventing disconnection of said second mouth from said chamber port; inserting said first mouth into the plenum port; and placing said second mouth into fluid communication with said chamber port thereby engaging said rocker tab with said pivot tab.
Parent Case Info

This application claims the benefit of U.S. Provisional application Ser. No. 60/042,019 filed Apr. 1, 1997.

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Provisional Applications (1)
Number Date Country
60/042019 Apr 1997 US