Gas turbine engine configured for modular assembly/disassembly and method for same
US-2015369123-A1 · Dec 24, 2015 · US
US10422225B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10422225-B2 |
| Application number | US-201515307972-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 11, 2015 |
| Priority date | May 12, 2014 |
| Publication date | Sep 24, 2019 |
| Grant date | Sep 24, 2019 |
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An annular clamping nut which is provided for being placed onto the end of a tie bar, in order to brace the latter, and which has in addition to a central recess for receiving the tie bar parallel to a longitudinal direction passages at uniform radial spacings in the ring circumferential direction which are directed parallel to the longitudinal direction of the central recess and are provided for receiving clamping screws. An external thread is provided on the outer surface of the clamping nut, which outer surface is arranged on a side which lies substantially opposite the wall of the central recess, which external thread runs substantially in the ring circumferential direction of the outer surface.
Opening claim text (preview).
The invention claimed is: 1. A tie bar system comprising: an annular clamping nut which is provided to be placed onto the end of a tie bar in order to tension said tie bar, comprising: a central recess for receiving the tie bar; passages with uniform radial spacings in a ring circumference direction which are parallel to a longitudinal direction, which passages are directed parallel to the longitudinal direction of the central recess; and on an outer surface of the clamping nut, an external thread which runs substantially in the ring circumference direction of the outer surface, clamping screws which extend through the passages of the clamping nut, and the tie bar, which is guided at the end through the central recess of the clamping nut, and a clamping device arranged in a region of the outer surface of the clamping nut, which clamping device is screwed with the external thread of the clamping nut. 2. The tie bar system as claimed in claim 1 , wherein two adjacent passages of the passages in each case are spaced apart from one another uniformly in the ring circumference direction. 3. The tie bar system as claimed in claim 1 , wherein at least part of a wall of the central recess is configured as an internal thread which runs substantially in the ring circumference direction of the wall. 4. The tie bar system as claimed in claim 1 , wherein the passages exhibit a step-wise narrowing in the longitudinal direction. 5. The tie bar system as claimed in claim 1 , wherein the external thread on the outer surface only takes up part of the outer surface of the clamping nut, and is only provided at a level in the longitudinal direction at which there is a narrowed section of the passages. 6. The tie bar system as claimed in claim 1 , wherein the clamping screws each comprise an end, and wherein each end is in contact with a single clamping ring which is not included in the clamping nut. 7. The tie bar system as claimed in claim 1 , wherein the clamping device is configured as a hydraulic lifting device. 8. The tie bar system as claimed in claim 1 , wherein the clamping device is configured as a lifting device provided with second clamping screws. 9. The tie bar system as claimed in 1 , wherein the clamping device comprises: a recess comprising an internal thread that is capable of being screwed onto the external thread of the clamping nut, and at least one lifting means which is configured, during correct operation, to apply a clamping force to the clamping device, wherein the at least one lifting means is adapted to rest against a component surface of a gas turbine including a tie bar during this operation. 10. A gas turbine comprising: the tie bar system as claimed in claim 1 . 11. A method of tensioning the tie bar system as claimed in claim 1 , the method comprising: preloading of the tie bar through actuation of the clamping device; and retensioning of the tie bar by tightening the clamping screws in the passages. 12. The method as claimed in claim 11 , further comprising: relieving of tension on the clamping device, and releasing of the clamping device from the clamping nut. 13. The tie bar system as claimed in claim 1 , wherein the external thread on the outer surface only takes up part of the outer surface of the clamping nut in the longitudinal direction with a step-wise narrowing of the passages. 14. The method as claimed in claim 11 , wherein the tie bar system is a tie bar system of a gas turbine.
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