Turbine blade for a gas turbine engine
Patent Information
- Application Number
- US29/999996
- Authority / Receiving Office
- US · United States
- Patent Type
- Designs(United States)
- Current Assignee / Owner
- Filing Date
- 2025-04-18
- Publication Date
- 2026-09-15
- Estimated Expiration
- 2041-09-15
Smart Images

Figure USD1148007-D00000_ABST
Description
[0001] FIG. 1 is a perspective view of a turbine blade for a gas turbine engine showing the new design.
[0002] FIG. 2 is a left side view of the turbine blade for a gas turbine engine of FIG. 1.
[0003] FIG. 3 is a right side view of the turbine blade for a gas turbine engine of FIG. 1
[0004] FIG. 4 is a front view of the turbine blade for a gas turbine engine of FIG. 1.
[0005] FIG. 5 is a rear view of the turbine blade for a gas turbine engine of FIG. 1.
[0006] FIG. 6 is a top view of the turbine blade for a gas turbine engine of FIG. 1.
[0007] FIG. 7 is a bottom view of the turbine blade for a gas turbine engine of FIG. 1.
[0008] FIG. 8 is an enlarged perspective view of a portion of the turbine blade for a gas turbine engine of FIG. 1.
[0009] FIG. 9 is a left side view of the portion of the turbine blade for a gas turbine engine of FIG. 8.
[0010] FIG. 10 is a right side view of the portion of the turbine blade for a gas turbine engine of FIG. 8
[0011] FIG. 11 is a front view of the portion of the turbine blade for a gas turbine engine of FIG. 8.
[0012] FIG. 12 is a rear view of the portion of the turbine blade for a gas turbine engine of FIG. 8.
[0013] FIG. 13 is a top view of the portion of the turbine blade for a gas turbine engine of FIG. 8; and,
[0014] FIG. 14 is a bottom view of the portion of the turbine blade for a gas turbine engine of FIG. 8.
[0015] The elements shown in broken lines are included for the purpose of illustrating environment and form no part of the claimed design.
Claims
The ornamental design for a turbine blade for a gas turbine engine as shown and described.
Citation Information
Patent Citations
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