Light weight and highly cooled turbine blade
US8057183B1 · kind B1 · utility
Assignee
Inventor
Key dates
| Filing date | Dec 16, 2008 |
| Grant date | Nov 15, 2011 |
| Priority date | — |
| Expiry date | May 19, 2030 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2260/2214
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A turbine rotor blade formed from a main support spar and having a thin thermal skin bonded or formed to the support spar to form the outer airfoil surface of the blade. The main support spar is formed from a plurality of ribs arranged to form a cooling air supply cavity near the leading edge region, a plurality of impingement chambers and a plurality of spent air collector chambers arranged along the pressure side and suction side of the airfoil to form a series of impingement chambers and collector chambers to provide near wall cooling for the thermal skin. A row of exit cooling holes located along the trailing edge discharges the cooling air from the last collector chamber. In another embodiment, some of the collector chambers are connected to rows of film cooling air to discharge film cooling onto the outer airfoil surface. The thermal skin includes micro pin fins on the inner wall to enhance the cooling effect of the impinging cooling air. The entire blade comprises a spar support structure, a thin thermal skin, external coating formed using a metal molecular depositing process to build up the blade as a single piece but with multiple material.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.