Inventor

SCHMALING DAVID N

US42 patents

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

SCHMALING DAVID N

SIKORSKY AIRCRAFT CORP

Snubber

Optimized composite flexbeam for helicopter tail rotors

Rotor system with pitch flap coupling

Upper rotor control system for a counter-rotating rotor system

Rotor blade folding system

Snubber-vibration damper system for a bearingless main rotor

Inertial vibration isolator spring for helicopter

Optimized composite flexbeam for helicopter rotors

Structural bushing application for highly loaded composites lugs

Vibration isolator for rotorcraft

Helicopter rotor blade mounting assembly

Elastomeric bearing with heatable shims

Strain isolated trim tab

Stiff inplane elastomeric rotorhead

Inertial mass for vibration isolators

Abrasion resistant pivot bearing

Rotor assemblies having automatic blade folding systems

Rotor blade snubber retainer for a rotary wing aircraft

Trim tab retention system, an aircraft employing same and a method of retaining a trim tab within a blade housing

Rotary wing aircraft pitch beam attachment with anti-rotation plate design

UNITED TECHNOLOGIES CORP

Fiber reinforced composite spar for a rotary wing aircraft

Snubber bearing mounting assembly for bearingless rotors

Pitch adjustment assembly for bearingless main rotors

Hybrid composite flexbeam for a helicopter bearingless main rotor assembly

Flexbeam for a helicopter bearingless main rotor assembly

Spar-to-hub joint for a flexbeam helicopter rotor

Hybrid helicopter rotor hub retention plate

Two-step composite joint

Propeller blade pin attachment

LOCKHEED CORP

Hingeless helicopter rotor with high stiffness and low drag configuration

Folding horn concept for rigid rotor blade fold

Rotor blade non-counterbored retention assembly via a sliding clamped bushing

Main rotor blade using integral metallic center block strap assembly

Rotor system

Rotor assembly connectable to rotor hub and having pitch control

Low drag high capacity pitch bearing for rigid rotor aircraft

Rotor blade folding system

SCHMALING DAVID N

Clevis joint capable of accommodating substantial pivotal motion between its joined members and loading along its axis

Compact load path swashplate assembly

Lead stop for rotor system with fluid-elastomeric lead/lag damper

Impact test fixture with simulated centrifugal force

MEYER LEON M

Elastomeric bearing system motion limiter