A rotating blade design uses leading edge inflection points and trailing edge grooves to alter fluid flow patterns.
A fan assembly uses a movable insert to dynamically adjust the throat gap based on rotational speed.
A fan assembly uses a threaded endcap to retain the module for quick field replacement without tools.
Movable coupling features on the fuel pump assembly shift positions along support structures to accommodate varying fuel tank depths and shapes.
Helical shaft grooves move gas from the thrust bearing to a collection chamber, preventing wear and failure caused by excess gas accumulation.
Segmenting the connection into hub and boss zones reduces press force requirements while maintaining alignment and preventing yield point exceedance.
Integrated rim fixing elements eliminate complex bolted flanges, reducing assembly cost while maintaining platform retention.
A fan securing device uses adjustable locking units and connecting arms to clamp cooling fans between holders without bolts.
Radially deflectable fingers accommodate thermal expansion of exhaust struts, reducing stress from mismatched growth between inner and outer shrouds.
Variable scroll area enlargement reduces flow resistance while recovering static pressure, resolving the trade-off between productivity and energy loss.
Segmented variable pitch inlet guide vanes adjust airflow angle to prevent surge and stall during high thrust operations.
Capillary channels in porous material return lubricant to the reservoir, eliminating gravity dependency for reliable operation in any orientation.
Profiled pylons merge structural arms with fairings to homogenize secondary air flow, minimizing angular distortion and pressure losses.
A pressure sensor between the air regulator and inlet valve measures reduced system pressure to monitor drill bit flushing air flow.
Distributed threaded connections on a turbocharger rotor shaft secure components against high-speed vibration while increasing torque transmission capacity.
Segmented inner casings with a tab and chute blocking system reduce maintenance time by eliminating complex fixing means.
Concave blade surfaces generate secondary air flow vortices to boost cross-flow fan blowing capacity while reducing power consumption and noise.
Unequal stator blade spacing disrupts wave front alignment to attenuate interference noise, avoiding engine weight increases from sound absorption materials.
Surrounding thermal transfer units expand the effective cross-sectional flow area, reducing power loss from concentrated outlet resistance.
A fan apparatus uses a hollow cylindrical housing and an axial circuit board holding structure to move air efficiently.
Transitioning from laminated layers to 3D weaving eliminates delamination under thermal gradients while preserving manufacturing feasibility.
Rerouting heat-exchanged charge air through a housing conduit convects heat from the compressor wheel, preventing premature failure of aluminum components.
A gas turbine cooling system uses a heat exchanger to transfer core airflow heat to bypass duct air via pressure differentials.
An embedded connection unites the blower volute covers, eliminating complex fasteners and lowering production costs.
Merging the impeller and rotor eliminates separate bearings, reducing volume and manufacturing costs while enhancing durability.
Segmented flexible diffusers and passive damper doors manage gas exchange in farmhouses while minimizing energy loss during non-operation.
Varying curvature radii in the scroll flow path reduce air separation along the inner wall, enhancing compressor performance.
Coolant passages with internal pins manage thermal loads and lubricant degradation to sustain high power output.
A slidingly connected passive element guides the actuating ring, preventing axial deflection and reducing assembly mass.
A vibration-absorbing boss uses integrated thermoplastic resin injection molding to couple fan components.
Segmented dampers with elastic bonding reduce vibration in rotary machines by converting energy to heat, extending service life despite wear.
An insulating fan wheel prevents electrostatic ignition in explosive gas-air mixtures, removing costly grounding mechanisms.
Fiber reinforcement underlayer secures abradable coating to turbine engine structural support without damaging sensitive anodized surfaces.
A centrifugal fan impeller uses a splitter wall to divide blade chambers and direct fluid flow efficiently.