Inventor

GROVER ERIC A

US32 patents

⚠️ This page may combine multiple inventors who share the name “GROVER ERIC A”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

GROVER ERIC A

UNITED TECHNOLOGIES CORP

Boundary layer transition model

Airfoil array with an endwall protrusion and components of the array

Gas turbine engine with non-axisymmetric surface contoured vane platform

Cantilevered hydrostatic advanced low leakage seal

Endwall contouring

Airfoil embodying mixed loading conventions

Blade or vane with a laterally enlarged base

Shaped rim cavity wing surface

Gas turbine engine airfoil

Articulating cantilevered hydrostatic seal

Endwall contouring

Variable area vane endwall treatments

Hydrostatic seal with extended housing

Hydrostatic seal with enhanced maneuver response

Airfoil contour for low-loss on-boarding of cooling air through an articulating spindle

Hydrostatic seal with aft tooth

Bearing assembly for gas turbine engines

Variable area turbine vane row assembly

Turbomachine flow path having circumferentially varying outer periphery

Non-contact seal for rotational equipment with radial through-hole

GROVER ERIC A

Endwall with leading-edge hump

Shaped rim cavity wing surface

Non-axisymmetric rim cavity features to improve sealing efficiencies

PRAISNER THOMAS J

Gas turbine engine with non-axisymmetric surface contoured rotor blade platform

Turbomachine flow path having circumferentially varying outer periphery

ALLEN-BRADLEY EUNICE

Airfoil array with an endwall depression and components of the array

Flow passage for gas turbine engine

RAYTHEON TECH CORP

Non-contact seal assembly with multiple axially spaced spring elements

Non-contact seal for rotational equipment with axially expended seal shoes

HAZZARD ROBERT L

Retrofit dirt separator for gas turbine engine

RTX CORP

Non-contact seal assembly with multiple spaced spring elements

AGGARWALA ANDREW S

Airfoil design having localized suction side curvatures