Inventor

SURACE RAYMOND

US73 patents

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

SURACE RAYMOND

UNITED TECHNOLOGIES CORP

Thin seal for an engine

Thin seal for an engine

Enhanced serpentine cooling with U-shaped divider rib

Blade damper

Variable area turbine arrangement with secondary flow modulation

Systems and methods for providing vane platform cooling

Gas turbine engine component cooling scheme

Airfoil with ceramic airfoil piece having internal cooling circuit

Airfoil having panels

Multi-segment adjustable stator vane for a variable area vane arrangement

Variable area gas turbine engine component having movable spar and shell

Cooled cooling air for blade air seal through outer chamber

Variable area vane endwall treatments

Vane support systems

Multi-flow cooling circuit for gas turbine engine flowpath component

Vane cooling structures

Airfoil pieces secured with endwall section

Variable area vane arrangement for a turbine engine

Turbine component with a thin interior partition

Wire mesh brush seal windage cover

Variable area turbine arrangement for a gas turbine engine

Multi-walled airfoil core

Method for providing coolant to a movable airfoil

RAYTHEON TECH CORP

Thin seal for an engine

Airfoil with sandwich composite

Airfoil anti-rotation ring and assembly

Ceramic component having silicon layer and barrier layer

Ceramic component having silicon layer and barrier layer

Vane arc segment with thermal insulation element

Gas turbine engine airfoil with variable pitch cooling holes

Engine with cooling passage circuit for air prior to ceramic component

Airfoil with sandwich composite flange

Vane arc segment with thermal insulation element

Diffused cooling arrangement for gas turbine engine components

Needled ceramic matrix composite cooling passages

Seal slot with coating

Vane multiplet with conjoined singlet vanes

Airfoil with wishbone fiber structure

Seal system having silicon layer and barrier layer

Cooling arrangement for gas turbine engine component

Multi-walled airfoil core

Ceramic matrix composite part release from chemical vapor infiltration tooling

RTX CORP

Turbine component with a thin interior partition

Repair of ceramic vane using over-wrap fiber ply and re-stagger

Dovetail features on panel rails or impingement sheet to hold panels

Airfoil anti-rotation ring and assembly

Cooling arrangement for gas turbine engine component

SURACE RAYMOND

Castings, casting cores, and methods

Gas turbine engine component cooling scheme

Gas turbine engine component cooling scheme