Modularity of an aircraft turbomachine
US-2024003303-A1 · Jan 4, 2024 · US
US9869198B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9869198-B2 |
| Application number | US-201514710742-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 13, 2015 |
| Priority date | May 13, 2015 |
| Publication date | Jan 16, 2018 |
| Grant date | Jan 16, 2018 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
An intershaft integrated seal and lock-nut assembly includes spaced apart forward and aft shafts, forward lock-nut threaded onto aft end of forward shaft, aft lock-nut threaded onto a forward end of aft shaft, and seal ring sealingly engaging and disposed between forward and aft lock-nuts operable to seal annular gap between forward and aft shafts. Seal ring may be disposed in annular ring groove extending radially inwardly into one of forward and aft lock-nuts and annular cylindrical inner surface on other one of lock-nuts operable to seal against seal ring. Seal ring may be carbon seal ring and split. Aft lock-nut may include forwardly extending annular arm having annular cylindrical inner surface. Retention tabbed rings may engage lock-nuts and shafts and snap rings may engage retention tabbed rings and lock-nuts. Seal ring may be in ring groove in aft lock-nut.
Opening claim text (preview).
What is claimed: 1. An intershaft integrated seal and lock-nut assembly comprising: axially spaced apart forward and aft shafts, a forward lock-nut threaded onto an aft end of the forward shaft, an aft lock-nut threaded onto a forward end of the aft shaft, and a seal ring sealingly engaging and disposed between the forward and aft lock-nuts and operable to seal an annular gap between forward and aft shafts, further comprising: the seal ring disposed in an annular ring groove extending radially inwardly into one of the forward and aft lock-nuts, the seal ring operable to seal against the one of the forward and aft lock-nuts within the annular ring groove, an annular cylindrical inner surface on another one of the forward and aft lock-nuts, and the annular cylindrical inner surface operable to seal against the seal ring. 2. The assembly as claimed in claim 1 , further comprising the seal ring being a carbon seal ring. 3. The assembly as claimed in claim 2 , further comprising the carbon seal ring being split. 4. An intershaft integrated seal and lock-nut assembly comprising: axially spaced apart forward and aft shafts, a forward lock-nut threaded onto an aft end of the forward shaft, an aft lock-nut threaded onto a forward end of the aft shaft, and a seal ring sealingly engaging and disposed between the forward and aft lock-nuts and operable to seal an annular gap between forward and aft shafts, further comprising: the seal ring disposed in the annular ring groove extending radially inwardly into the forward lock-nut, the aft lock-nut including a forwardly extending annular arm having an annular cylindrical inner surface surrounding the annular ring groove, and the annular cylindrical inner surface being operable to seal against the seal ring. 5. The assembly as claimed in claim 4 , further comprising the seal ring being a carbon seal ring. 6. The assembly as claimed in claim 5 , further comprising the carbon seal ring being split. 7. An intershaft integrated seal and lock-nut assembly comprising: axially spaced apart forward and aft shafts, a forward lock-nut threaded onto an aft end of the forward shaft, an aft lock-nut threaded onto a forward end of the aft shaft, and a seal ring sealingly engaging and disposed between the forward and aft lock-nuts and operable to seal an annular gap between forward and aft shafts, further comprising: forward and aft retention tabbed rings engaging the forward and aft lock-nuts and the forward and aft shafts respectively, forward and aft snap rings disposed in radially inwardly open annular forward and aft grooves in the lock-nuts respectively, and the forward and aft snap rings engaging the forward and aft retention tabbed rings and the forward and aft lock-nuts respectively. 8. The assembly as claimed in claim 7 , further comprising: the seal ring disposed in the annular ring groove extending radially inwardly into the forward lock-nut, the aft lock-nut including a forwardly extending annular arm having an annular cylindrical inner surface surrounding the annular ring groove, and the annular cylindrical inner surface being operable to seal against the seal ring. 9. The assembly as claimed in claim 8 , further comprising the seal ring being a carbon seal ring and/or split. 10. An intershaft integrated seal and lock-nut assembly comprising: axially spaced apart forward and aft shafts, a forward lock-nut threaded onto an aft end of the forward shaft, an aft lock-nut threaded onto a forward end of the aft shaft, and a seal ring sealingly engaging and disposed between the forward and aft lock-nuts and operable to seal an annular gap between forward and aft shafts, further comprising: the seal ring disposed in the annular ring groove extending radially inwardly into the aft lock-nut, the forward lock-nut including an aftwardly extending annular arm having an annular cylindrical inner surface surrounding the annular ring groove, and the annular cylindrical inner surface operable to seal against the seal ring. 11. A gas turbine engine assembly comprising: axially spaced apart power output and stub shafts, the power output connected to a low pressure drive shaft connected to a low pressure turbine, the stub shaft connected to a high pressure rotor including a high pressure turbine and rotatably supported by a first bearing, a horizontal bevel gear and a ball bearing inner race of the a first bearing mounted on the stub shaft, a high pressure lock-nut threaded on forward threads on a forward end of the stub shaft, the high pressure lock-nut axially securing the horizontal bevel gear and the ball bearing inner race on the stub shaft, an aft power shaft lock-nut threaded on aft threads on an aft end of the power output shaft axially securing a roller bearing inner race of the output shaft bearing to the power output shaft, and a seal ring sealingly engaging and disposed between the aft power shaft lock-nut and the high pressure lock-nut and operable to seal an annular gap between the power output shaft and the stub shaft. 12. The assembly as claimed in claim 11 , further comprising: the seal ring disposed in an annular ring groove extending radially inwardly into the aft power shaft lock-nut, the seal ring operable to seal against the aft power shaft lock-nut within the annular ring groove, the high pressure lock-nut including an annular cylindrical inner surface surrounding the annular ring groove, and the annular cylindrical inner surface being operable to seal against the seal ring. 13. The assembly as claimed in claim 12 , further comprising the seal ring being a carbon seal ring. 14. The assembly as claimed in claim 13 , further comprising the carbon seal ring being split. 15. The assembly as claimed in claim 11 , further comprising: the seal ring disposed in an annular ring groove extending radially inwardly into the aft power shaft lock-nut, the high pressure lock-nut including a forwardly extending annular arm having an annular cylindrical inner surface surrounding the annular ring groove, and the annular cylindrical inner surface being operable to seal against the seal ring. 16. The assembly as claimed in claim 15 , further comprising the seal ring being a carbon seal ring. 17. The assembly as claimed in claim 16 , further comprising the carbon seal ring being split. 18. The assembly as claimed in claim 15 , further comprising: forward and aft retention tabbed rings engaging the aft power shaft lock-nut the high pressure lock-nut and the power output shaft and the stub shaft respectively, forward and aft snap rings disposed in radially inwardly open annular forward and aft grooves in the aft power shaft lock-nut the high pressure lock-nut respectively, and the forward and aft snap rings engaging the forward and aft retention tabbed rings and the high pressure lock-nut and the power output shaft and the stub shaft respectively. 19. The assembly as claimed in claim 18 , further comprising the seal ring being a split carbon seal ring.
for turbines · CPC title
Radial bearings · CPC title
Blade-carrying members, e.g. rotors (rotors of non-bladed type F01D1/34; stators F01D9/00 {; selecting particular materials F01D5/28}) · CPC title
Arrangement of bearings; Supporting or mounting bearings in casings (bearings per se F16C) · CPC title
Retaining bolts or nuts · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.