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US3697192A Expired / Lapsed US ⏱️ 0.0 years remaining

Hollow turbine blade

Assignee: RTX Corp
•
Filing: 1970-05-07
•
Granted: 1972-10-10
•
Expires: 1990-05-07
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Abstract

Abstract A hollow cooled gas turbine blade is made by forming an insert with a hollow airfoil and a hollow root portion and with lateral cooling air passages extending through the wall of the airfoil and positioning the insert in a hollow main blade having an airfoil portion and a notch in the root to receive the root portion of the insert with both root portions having aligned serrations on opposite surfaces for supporting the blade and the insert in a turbine disk.

Inventors

  • 👤 Charles W Hayes

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-24 02:21
CPC Classifications
B; B23; B23P; B23P15/00; B23P15/02; F; F01; F01D; F01D5/00; F01D5/12; F01D5/14; F01D5/18; F01D5/187; F01D5/188; F01D5/189

Claims Analysis

Total Claims: 4
Claim 1
Independent Claim 131 words
A gas turbine blade construction including a main blade having a main root portion with blade attachment means on opposite sides thereof and with a transverse groove extending entirely across the root portion and an integral airfoil portion projecting from said root portion, and an insert within said main blade, said insert including an insert airfoil portion within and spaced laterally from said main blade airfoil portion and an insert root portion to which said airfoil portion is attached, said insert root portion extending transversely across said main root portion and fitting in the transverse groove therein, said insert having blade attachments means thereon in alignment with those on the main root, said insert root portion supporting the insert airfoil portion within and in spaced relation to the blade airfoil portion.
Claim 2
Dependent Claim 131 words
A gas turbine blade construction including a main blade having a main root portion with blade attachment means on opposite sides thereof and with a transverse groove extending entirely across the root portion and an integral airfoil portion projecting from said root portion, and an insert within said main blade, said insert including an insert airfoil portion within and spaced laterally from said main blade airfoil portion and an insert root portion to which said airfoil portion is attached, said insert root portion extending transversely across said main root portion and fitting in the transverse groove therein, said insert having blade attachments means thereon in alignment with those on the main root, said insert root portion supporting the insert airfoil portion within and in spaced relation to the blade airfoil portion.
Claim 3
Dependent Claim 39 words
A blade construction as in claim 1 in which the insert has a passage extending longitudinally thereof, including the insert root portion, and lateral passages positioned transversely in said insert air foil portion and communicating with the longitudinal passage.
Claim 4
Dependent Claim 40 words
A bladE construction as in claim 2 in which the airfoil portion of the insert is hollow and the passage in the insert root portion of the insert communicates from said hollow airfoil portion to the base of the root.

References Cited (Backward Citations)

US2559131A Cited
US2780435A Cited
US2848192A Cited
US2851216A Cited
GB833770A Cited
US3014270A Cited
US3057597A Cited
US3446480A Cited
US3542486A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1975-10-10 1976-04-10 1976-10-10 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1979-10-10 1980-04-10 1980-10-10 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1983-10-10 1984-04-10 1984-10-10 $7700.00 Window Closed / Lapsed

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