초록 ▼

A method of producing a plurality of effusion holes in a wall of a combustor of a gas turbine engine comprises: determining a hole pattern definition which provides a functional relationship of the spacing between each adjacent hole within the row of holes; using the hole pattern definition to ident

A method of producing a plurality of effusion holes in a wall of a combustor of a gas turbine engine comprises: determining a hole pattern definition which provides a functional relationship of the spacing between each adjacent hole within the row of holes; using the hole pattern definition to identify individual positions of the effusion holes to be produced; and using a hole producing system to produce the effusion holes at the identified positions.

대표청구항 ▼

1. A method of producing a plurality of effusion holes in a wall of a combustor of a gas turbine engine, the method comprising the steps of: a) determining a hole pattern definition using: a count of the holes to be separated by first spaces in a row of holes along a first axis, positional informati

1. A method of producing a plurality of effusion holes in a wall of a combustor of a gas turbine engine, the method comprising the steps of: a) determining a hole pattern definition using: a count of the holes to be separated by first spaces in a row of holes along a first axis, positional information of a first hole in the row of holes, a first length of the row of holes, and, a first spacing ratio relating hole spacing distances between each adjacent hole within the row of holes, and further comprising determining the hole pattern definition using the geometric relation L1=aL2=a2L3=a3L4=an−1Ln=(SR)Ln,where L1 is a first hole spacing distance, a is a constant, n is the number of first spaces in the row of holes along the first axis, Ln is a hole spacing distance associated with first space number n, and, SR is the first spacing ratio which is equal to an−1;b) using the hole pattern definition to identify individual positions of the effusion holes to be produced in the wall of the combustor; andc) using a hole producing system to produce the effusion holes in the wall of the combustor at the identified positions. 2. The method as defined in claim 1, wherein the hole pattern definition of step a) is determined by further using: a count of rows of holes to be separated by second spaces along a second axis;a second length through which the rows of holes are spaced along the second axis; anda second spacing ratio relating row spacing distances between each adjacent row of holes along the second axis. 3. The method as defined in claim 2, wherein the first axis represents a circumferential direction of the combustor and the second axis represents an axial direction of the combustor. 4. The method as defined in claim 1, further comprising the step of i) designing a desired hole pattern for the effusion holes based on local hot spots within the combustor, prior to the determining step a). 5. The method as defined in claim 4, further comprising the step of ii) determining a suitable first spacing ratio based on the designed hole pattern of step i), prior to the determining step a). 6. The method as defined in claim 1, wherein the step of identifying the individual positions of the effusion holes further comprises mirroring the hole pattern. 7. A method of producing a plurality of effusion holes in a wall of a combustor of a gas turbine engine, the effusion holes being arranged in a hole pattern, the method comprising the steps of: determining individual positions of said effusion holes arranged in the hole pattern by: a) using a geometric relation that relates relative spacing distances between each of the effusion holes separated by spaces in a row of holes to each other, the geometric relation being L1=aL2=a2L3=a3L4=an−1Ln=(SR)Ln,where L1 is a first spacing distance, a is a constant, n is a count of the spaces in the row of holes, Ln is a spacing distance associated with a space number n, and, SR is a spacing ratio which is equal to an−1 and provides a functional relationship between spacing distances of any adjacent hole within the row of holes; andb) using positional information of a first hole in the row of holes, a count of the holes and a length of the row of holes to determine the position of any of the effusion holes within the row of holes in accordance with the geometric relation; andusing a hole producing system to produce the effusion holes in the wall of the combustor at the determined individual positions of said effusion holes. 8. The method as defined in claim 7, further comprising the steps of c) using the geometric relation to relate relative spacing distances between a plurality of adjacent rows of holes by defining L1 as a first row spacing, n as a count of the rows of holes and selecting SR based on a desired row spacing; andd) using the positional information of a first row of holes, a count of the rows of holes and the distance across which the rows are spaced to determine the position of any of the adjacent rows of holes in accordance with the geometric relation. 9. The method as defined in claim 8, wherein the positional information of the first row of holes is determined from the positional information of the first hole. 10. The method as defined in claim 8, wherein the holes in each row of holes are to be spaced along a circumferential direction of the combustor and the rows of holes are to be spaced along an axial direction of the combustor.