Active stator field control and damping components keep rotor alignment stable in VTOL maglev flight while reducing noise and inefficiency.
A nickel-iron-titanium aluminum alloy balances yield strength, electrical conductivity, flowability, and hot-tear resistance in die casting.
Heating the outer ring and using radial jaws plus axial pressing speeds turbine vane ring assembly while reducing damage risk.
Heating the outer ring and using expandable jaws plus a press speeds vane ring assembly while reducing damage to press-fitted turbine parts.
A tensile preloading tool elastically offsets weld-induced flange retraction in bladed stators, reducing post-weld machining and vane replacement issues.
A metal repair preform replaces damaged CMC sections to cut repair cost and reduce brittle failure in turbine engine components.
Roll-welded sheet channels enable branched cooling paths in cast motor and battery housings while avoiding welding deformation.
Variable-pitch stator blades correct sector misalignment to homogenize turbine passage sections and improve turbomachine efficiency over engine life.
Different tongue-to-impeller radial distances in a twin-scroll turbine cut excitation force and blade vibration without sacrificing aerodynamic performance.
An integrated annular baffle guides hot air to the splitter, cutting heat loss and deicing demand without hurting turbomachine performance.
A multi-material exhaust flange with ring and tubular sections accommodates thermal expansion and lowers stress at the strut junction.
Radial support ribs stiffen gas turbine guide vane support sections, improving force distribution and reducing machining cracks.
Non-uniform stator blade pitch matches circumferential pressure distortion to balance rotor flow and reduce stability margin loss.
Scroll stator vanes and an annular collection region smooth rotary-engine exhaust pulsation for more uniform turbine inlet flow and lower stress.
Replaceable pads between the nozzle ring root and clamp absorb friction and contact corrosion, cutting turbine maintenance cost and downtime.
A segmented outer flange in a different material absorbs turbine case thermal deflection and lowers stress concentrations during transients.
Vane passages steer combustion gas inward and tangentially, reducing flow pulsations and nonuniformity at the axial turbine inlet.
Independent tip and hub vane segments adjust fan exit flow to improve operability, stall margin, and incidence control.
A machined relief feature creates a collapse path, removing an interference-fit strut without damaging the bearing structure.
Matched nickel-alloy expansion and brazing join the tierod to the bearing ring while enlarging space for cooling and oil routing.
Additive manufacturing integrates vanes, mounts, and deformable baffles to simplify assembly and reduce gas turbine engine mass.