Blade for a gas turbine engine

• US 4,260,326 A
• Filed: 07/18/1974
• Issued: 04/07/1981
• Est. Priority Date: 07/26/1973
• Status: Expired due to Term

• Current Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Inventors: Simmons, Roy, Scott, Alexander
• Primary Examiner(s): Bentley, Stephen C.
• Application Number:
  US05/489,151
• Time in Patent Office: 2,455 Days
• Field of Search: 416/232, 416/97 RA, 416/132 R, 416/225, 416/95, 415/115
• US Class Current: 415/115
• CPC Class Codes: F01D 9/023 Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings

Abstract

A stator blade for a gas turbine engine comprises a stack of laminar sections and means adapted to resiliently hold the sections together in compression to allow for differential expansion between the stack and supporting structure.

Claims

1. A stator blade for a gas turbine engine, comprising laminar sections arranged in abutting relationship and defining a stack having opposite ends, fixed structure confronting one end of the stack, and a piston and cylinder device connected between the fixed structure and the other end of the stack for compression thereof under air pressure supplied to said piston and cylinder device.

2. A stator blade as claimed in claim 1 in which said sections are hollow and define an opening extending through the stack between the ends thereof, and including a pressure member situated at said other end of the stack, said piston and cylinder device having a cylinder situated adjacent said one end of the stack and containing a piston, and a tension member connected between the pressure member and the piston.

3. A stator blade as claimed in claim 2 in which said fixed structure includes means defining an inlet for pressurized cooling air adjacent said other end of said stack and connected to the opening in said stack for the supply of cooling air thereto, and means provided adjacent the other end of said stack for ducting the cooling air from the opening in said stack into said cylinder for actuation of said piston.

4. A stator blade as claimed in claim 2 comprising a core extending within said opening and having exterior surfaces for the support of the sections in their stacked relationship, an enlarged portion of the core extending beyond said one end of the stack and including the said cylinder, means defining an opening within the core in the direction of the length of the stack, and said tension member extending through the opening in the core.

5. A stator blade as claimed in claim 4 comprising means defining ducts in the core between the interior thereof and the opening in the stack for the supply of cooling air from the interior of the core to the sections.

6. A stator blade according to claim 1 in which adjacent sections define two abutting surfaces, at least one groove in one of the abutting surfaces extending between the interior and exterior of the hollow section defining together with the other abutting surface at least one channel for the supply of cooling air from the opening in the stack to the exterior thereof.

7. A stator blade as claimed in claim 1 and in which said sections are made of a ceramic material.

8. A stator blade as claimed in claim 7 and in which there is a structural core which is made of metal.