Gas turbine engine configured for modular assembly/disassembly and method for same
US-2015369123-A1 · Dec 24, 2015 · US
US10415624B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10415624-B2 |
| Application number | US-201715606580-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 26, 2017 |
| Priority date | May 26, 2017 |
| Publication date | Sep 17, 2019 |
| Grant date | Sep 17, 2019 |
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A bolt retention clip for a gas turbine engine rotor assembly includes a main plate section defining a central aperture, the central aperture sized to receive a bolt therethrough. Also included is a pair of bolt retention tabs extending away from a first face of the main plate section to axially retain a head of the bolt. Further included is a first clip retaining tab extending away from the first face of the main plate section for insertion into a groove of a rotor structure. Yet further included is a second clip retaining tab extending away from a second face of the main plate section for engagement with an edge of the rotor structure.
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What is claimed is: 1. A bolt retention assembly for a gas turbine engine rotor assembly comprising: a plurality of rotor stages and a rotor hub disposed in a stacked arrangement, each of the rotor stages and the rotor hub defining respective holes; a bolt extending through the holes of the rotor stages and the rotor hub; and a retention clip comprising: a main plate section defining a central aperture, the central aperture sized to receive the bolt therethrough; a pair of bolt retention tabs extending away from a first face of the main plate section to axially retain a head of the bolt; a first clip retaining tab extending away from the first face of the main plate section for insertion into a groove defined by a rotor structure that is one of the rotor stages or the rotor hub, wherein the groove is defined by a main portion of the rotor structure and a rail of the rotor structure; and a second clip retaining tab extending away from a second face of the main plate section for engagement with an edge of the rotor structure. 2. The bolt retention assembly of claim 1 , wherein the bolt retention tabs are flexibly hinged to the main plate section. 3. The bolt retention assembly of claim 1 , wherein the bolt retention tabs extend perpendicularly to the main plate section. 4. The bolt retention assembly of claim 1 , wherein the first clip retaining tab extends perpendicularly to the main plate section. 5. The bolt retention assembly of claim 1 , wherein the second clip retaining tab comprises a first segment and a second segment, the first segment extending perpendicularly from the main plate section and the second segment extending perpendicularly from the first segment to define a U-shaped slot with the main plate section. 6. The bolt retention assembly of claim 5 , wherein the edge of the rotor structure is disposed in the U-shaped groove in an assembled condition of the bolt retention clip and the rotor structure. 7. The bolt retention assembly of claim 6 , wherein the rotor structure includes a recess located adjacent the edge engaged with the second clip retaining tab. 8. The bolt retention assembly of claim 6 , wherein the edge of the rotor structure and the second clip retaining tab are sized to be in an interference fit. 9. The bolt retention assembly of claim 1 , wherein the bolt is a T-bolt. 10. The bolt retention assembly of claim 1 , further comprising a nut secured to the bolt. 11. The bolt retention assembly of claim 1 , wherein the plurality of rotor stages comprises a first rotor stage, a second rotor stage, and a third rotor stage. 12. The bolt retention assembly of claim 11 , wherein the rotor structure is part of the third rotor stage.
for surfaces not surrounding the bolt, e.g. hook adaptors for bolts · CPC title
Measures against loss of bolts, nuts or pins (devices for fastening nuts to surfaces F16B37/04) · CPC title
with snap action · CPC title
Disassembly methods · CPC title
Retaining bolts or nuts · CPC title
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