Patent US4026659A successfully refreshed from Google Patents.
US4026659A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Cooled composite vanes for turbine nozzles
Assignee: Avco Corp
•
Filing: 1975-10-16
•
Granted: 1977-05-31
•
Expires: 1995-10-16
Abstract
Abstract A turbine nozzle has inner and outer shrouds structurally connected by hollow core members which together with nose and tail inserts retained in the shrouds form airfoil-shaped vanes. Openings in one of the shrouds supply cooling air to the hollow vane cores whose walls have orifices to impinge air upon the inserts. Spent air from the nose insert film cools the core. Air directed at the tail insert divides to flow through holes in the insert and to film cool the insert. Orifices and holes are cast or readily drilled into the parts prior to their assembly. For superior resistance to high temperatures, the inserts are preferably columnar-grained or monocrystalline superalloy castings which are brazed or welded into the shrouds and are replaceable to extend nozzle service life. Alternatively, ceramic or metal inserts are mechanically retained in the shrouds.
Inventors
- 👤 William R. Freeman, Jr.
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-28 20:28
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/12; F01D5/14; F01D5/18; F01D5/186; F01D9/00; F01D9/02; F01D9/04; F01D9/041
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
195 words
A nozzle for a turbo-machine said nozzle comprising: an inner shroud; an outer shroud; and a plurality of spaced airfoils between said inner and outer shrouds, at least one of said airfoils comprising a core extending between and retaining said inner and outer shrouds, said core having an internal passage running spanwise, one of said shrouds having a cooling air inlet into said internal passage, said core having a cooling air outlet therethrough, at least one replaceable insert fabricated separately of said core and said shrouds and means for retaining said insert between said shrouds in spaced relation to and independently of said core, said insert being wedge shaped and forming a tail for said airfoil, said cooling air outlet comprising orifices through the rearward wall of said internal passage, said orifices being directed toward said tail insert, and said rearward wall and said tail insert being shaped and positioned relative to each other so as to define between them a cavity and a spanwise opening therefrom so that cooling air issuing from said orifices is dispersed in said cavity and issues through said opening to film cool an exterior surface of said tail insert.
Claim 2
Dependent Claim
195 words
A nozzle for a turbo-machine said nozzle comprising: an inner shroud; an outer shroud; and a plurality of spaced airfoils between said inner and outer shrouds, at least one of said airfoils comprising a core extending between and retaining said inner and outer shrouds, said core having an internal passage running spanwise, one of said shrouds having a cooling air inlet into said internal passage, said core having a cooling air outlet therethrough, at least one replaceable insert fabricated separately of said core and said shrouds and means for retaining said insert between said shrouds in spaced relation to and independently of said core, said insert being wedge shaped and forming a tail for said airfoil, said cooling air outlet comprising orifices through the rearward wall of said internal passage, said orifices being directed toward said tail insert, and said rearward wall and said tail insert being shaped and positioned relative to each other so as to define between them a cavity and a spanwise opening therefrom so that cooling air issuing from said orifices is dispersed in said cavity and issues through said opening to film cool an exterior surface of said tail insert.
Claim 3
Dependent Claim
22 words
The invention as in claim 1 wherein said means for retaining said insert comprises a bond between said insert and said shrouds.
Claim 4
Dependent Claim
41 words
The invention as defined in claim 1 wherein said tail insert also has cooling passages originating in the surface facing said core, said passages running rearward through said insert and carrying a portion of the cooling air issuing from said core.
Claim 5
Dependent Claim
27 words
The invention as defined in claim 1 wherein said insert additionally comprises a second insert having a generally semitubular shape and forming a nose for said airfoil.
Claim 6
Dependent Claim
127 words
The invention as defined in claim 4 wherein said cooling air outlet comprises orifices through the forward and the rearward walls of said internal passage, said forward wall orifices being directed toward said nose insert to impinge cooling air thereon, and said nose insert is shaped to direct cooling air over an exterior surface of said core, said rearward wall orifices being directed toward said tail insert, and said rearward wall and said tail insert are shaped and positioned relative to each other so as to define between them a cavity and a spanwise opening therefrom so that cooling air issuing from said rearward wall orifices is dispersed in said cavity and issues through said spanwise opening to film cool an exterior surface of said tail insert.
Claim 7
Dependent Claim
42 words
The invention as defined in claim 5 wherein said tail insert also has cooling passages originating in the surface facing said core, said passages running rearward through said insert and carrying a portion of the cooling air directed at said tail insert.
Claim 8
Dependent Claim
43 words
The invention as defined in claim 1 wherein said means for retaining said insert comprises at least one of said shrouds having a slot laterally confining at least one end of said insert and yielding means longitudinally retaining said insert within said slot.
References Cited (Backward Citations)
US2220420A
Cited
GB647143A
Cited
US2585871A
Cited
GB760734A
Cited
FR1151368A
Cited
US3166295A
Cited
US3211423A
Cited
US3533711A
Cited
DE1601563A1
Cited
US3619077A
Cited
US3430898A
Cited
US3486833A
Cited
US3600781A
Cited
US3844728A
Cited
US3650635A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1980-05-30 | 1980-11-29 | 1981-05-31 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1984-05-30 | 1984-11-29 | 1985-05-31 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1988-05-30 | 1988-11-29 | 1989-05-31 | $7700.00 | Window Closed / Lapsed |