Power Plant Construction TRIZ Cases
- Aircraft Engine Mount Bearing Washer Rotation Control
Clamped bearing washers rotate freely to prevent deformation, eliminating heavy arms and reducing weight while maintaining structural integrity.
- Non-axisymmetric Gas Turbine Intake Angular Offset
A non-axisymmetric gas turbine intake features an angularly offset medial plane relative to the engine central axis.
- Integrally Formed Pylon Mount Beam for Gas Turbine Engine
Unitarily forming engine mount beams with pylon structures eliminates separate bolted joints, reducing assembly labor and component weight.
- Turbine Engine Mounting Beam With Shear Fasteners
A mounting beam assembly uses radial shear fasteners to distribute loads across a webbed structure.
- Aircraft Engine Suspension Arch with Pivot Link
A suspension arch links to a beam via a pivot link parallel to the engine axis.
- Turbomachine Upstream Suspension System for Dilution Ratio
Segmented connecting rods reduce radial footprint to expand secondary flow vein cross-section and enhance dilution ratio.
- Gas Turbine Engine Mounting System with Mid-Turbine Frame
A gas turbine engine mounting system uses a mid-turbine frame to connect the rear mount and support bearing loads.
- Aircraft Engine Mount Rear-Facing Shear Pin Installation
Rear-mounted shear pins and tension bolts secure the aircraft engine mount, eliminating front face access requirements for fitting fasteners.
- Aircraft Engine Mounting System Backbone Bending Reduction
Angular mounting components create focal points that minimize backbone deflection, improving fuel efficiency.
- Jet Engine Mounting Pylon with Segmented Lateral Flank Joists
Segmented lateral flank joists in a jet engine mounting pylon distribute loads along specific paths, reducing weight while maintaining structural rigidity.