Inventor

JAIN NITESH

IN61 patents

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

JAIN NITESH

GEN ELECTRIC

Frangible gas turbine engine airfoil

Mechanical airfoil morphing with internal mechanical structures

Rotor blade with frangible spar for a gas turbine engine

Frangible airfoil with shape memory alloy

Containment case active clearance control structure

Noise reducing gas turbine engine airfoil

Frangible gas turbine engine airfoil including a retaining member

Method and system for separable blade platform retention clip

Metallic compliant tip fan blade

Turbine engine airfoil with a modified leading edge

Frangible gas turbine engine airfoil with layup change

Metallic compliant tip fan blade

Frangible gas turbine engine airfoil with chord reduction

Airfoil having a spar assembly for a turbine engine

Additively manufactured booster splitter with integral heating passageways

Method and device for connecting fan rotor to low pressure turbine rotor

Apparatus and system for composite fan blade with fused metal lead edge

Composite disk

System and method for HPT disk over speed prevention

Light weight fan casing configurations for energy absorption

Hybrid composite components

Airfoil for a gas turbine engine

Gas turbine engine rotor blade having a root section with composite and metallic portions

Component formed from hybrid material

Gas turbine engine rotor blade having a root section with composite and metallic portions

Variable pitch fan blade retention system

Turbine engine having a variable pitch airfoil assembly

Composite airfoil assembly for a turbine engine

Rotor blade with detachable tip

Airfoil arrangement for a gas turbine engine utilizing a shape memory alloy

Containment case active clearance control structure

Frangible gas turbine engine airfoil with fusion cavities

Composite airfoil assembly having a composite airfoil and spar

Rotating airfoil with a spring damper system

Component with spar assembly for a turbine engine

Part-span shrouds for pitch controlled aircrafts

Methods and apparatus to reduce deflection of an airfoil

Additively manufactured booster splitter with integral heating passageways

Methods and apparatus for passive fan blade tip clearance control

Airfoil assembly with tensioned blade segments

Pitch change mechanism for a fan of a gas turbine engine

Pitch change mechanism for a fan of a gas turbine engine

Additively manufactured rotating shaft

Circumferentially varying thickness composite fan casing

Fan assembly for an engine having redundant trunnion retention

Composite airfoils with frangible tips

Rotor blade with protective layer

RINGCENTRAL INC

System and method of determining an emotional state of a user

GENERAL ELECTRIC COMPANY

Methods and apparatus to reduce deflection of an airfoil

ADOBE INC

Generating digital assets utilizing a content aware machine-learning model