M
Mark Joseph Mielke
Researcher at General Electric
Publications - 24
Citations - 442
Mark Joseph Mielke is an academic researcher from General Electric. The author has contributed to research in topics: Trailing edge & Casing. The author has an hindex of 10, co-authored 24 publications receiving 442 citations.
Papers
More filters
Patent
Method and apparatus for reducing rotor assembly circumferential rim stress
TL;DR: A rotor assembly for a gas turbine engine (12) operates with reduced circumferential rim stress as discussed by the authors, which includes a rotor (14) including a plurality of rotor blades (26) extending radially outward from an annular rim (20).
Patent
Self bleeding rotor blade
TL;DR: In this paper, a self bleeding rotor blade and method of operation for reducing boundary layer thickness for improved performance was disclosed for improving aerodynamic performance of the rotor blade, which includes an outer surface configured for pressurizing air flowable thereover with bleed apertures being disposed therein.
Patent
Turbofan gas turbine engine with variable fan outlet guide vanes
TL;DR: A turbofan gas turbine engine (10) as mentioned in this paper includes a forward fan section (33) with a row of fan rotor blades (32), a core engine (18), and a fan bypass duct (40) downstream of the forward fan and radially outwardly of the core engine.
Patent
Reduced-stress compressor blisk flowpath
Mark Joseph Mielke,James Edwin Rhoda,David Edward Bulman,Craig Patrick Burns,Paul Smith,Daniel Gerard Suffoletta,Steven Mark Ballman,Richard Patrick Zylka,Lawrence J. Egan +8 more
TL;DR: In this paper, the outer surface of the rotor has a concave shape between adjacent blades with apexes located at interfaces between the blades and the rim, which directs air flow away from an interface between a blade and the rotor to reduce aerodynamic performance losses between the rim and blades.
Patent
Bowed compressor airfoil
TL;DR: A compressor airfoil (12) includes pressure and suction sides (18,20) extending from root (22) to tip (24) and between leading and trailing edges (26,28) as mentioned in this paper.