Turbine blade for a gas turbine engine

KR301364526SActive Publication Date: 2026-09-16SIEMENS ENERGY GLOBAL GMBH & CO KG
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Patent Information

Application Number
KR3020250042662
Authority / Receiving Office
KR · KR
Patent Type
Designs
Current Assignee / Owner
Filing Date
2025-10-22
Publication Date
2026-09-16
Estimated Expiration
2045-10-22

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    Figure 112025117909930-DES00003
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Description

Draw 15 The item that is the subject of the design Turbine blade for a gas turbine engine Description of the design 1. This design is a partial design, and the part expressed in solid lines is the part for which design registration is sought, while the part expressed in dashed lines is excluded from the scope of design rights. 2. Broken dashed lines shown in the drawing are shading lines to indicate curved or flat surfaces and do not constitute the shape of the design. 3. [Drawing 1] shows the overall shape of the design. 4. [Drawing 2] shows the front view of the design. 5. [Drawing 3] shows the rear view of the design. 6. [Drawing 4] shows the left side of the design. 7. [Drawing 5] shows the right side of the design. 8. [Drawing 6] shows the plan view of the design. 9. [Drawing 7] shows the bottom portion of the design. 10. [Figure 8] is an enlarged view of a part of [Figure 1]. 11. [Figure 9] is an enlarged view of a part of [Figure 2]. 12. [Figure 10] is an enlarged view of a part of [Figure 3]. 13. [Figure 11] is an enlarged view of a part of [Figure 4]. 14. [Figure 12] is an enlarged view of a part of [Figure 5]. 15. [Figure 13] is an enlarged view of a part of [Figure 6]. 16. [Reference Drawing 1] is an enlarged view of the shape of a part obscured by the dashed line in [Drawing 7]. Key points of the design creation The combination of the shape and form of the "turbine blade for a gas turbine engine" design is the key point of the design creation content.