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description=Linear Labs builds patented high-torque motor systems for wind, nuclear, pumps, actuators, and defense. Built in Fort Worth, Texas.;

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Text of the page (random words):
em event 03 efficiency 45 of global electricity powers motors 1 yet century old topologies have plateaued incremental gains can t close the gap linear labs built a new motor class from the ground up to solve all three 1 iea 4e abb 2023 electric motor systems account for over 45 of global electricity consumption our technology the het three motors working as one a patented circumferential flux architecture purpose designed for the highest torque density in any motor class delivering breakthrough efficiency and fault tolerance in a compact package 2x torque density 97 peak efficiency 50 lighter 90 patents see the full platform applications built for critical industries energy wind oil gas grid infrastructure industrial pumps actuators compressors nuclear smr coolant containment systems defense military vehicles naval systems mining haul trucks conveyors underground ready to explore what our motor architecture can do for your application schedule a technical review download pitchpro one pager the highest torque electric machine in its class purpose designed from the ground up for maximum torque density the first fundamental advancement in motor architecture in over 100 years how it works circumferential flux architecture the het hunstable electric turbine is a patented 4 rotor permanent magnet architecture purpose designed for the highest torque output in its class it combines axial and radial flux paths into a single circumferential flux tunnel extracting more torque per kilogram than any conventional motor topology unlike legacy radial flux machines limited by a single flux path the het s multi axis approach creates the equivalent of three motors working in concert maximizing flux linkage while minimizing copper losses key specifications 4 rotor shaft driven magnet architecture combined axial radial flux paths circumferential flux tunnel multi phase ride through capability built in fault tolerance graceful degradation not full shutdown not dependent on rare earth metals scalable from 10 kw to 2 2 mw 2 torque density 50 weight reduction and 97 peak efficiency based on linear labs internal testing of het prototypes vs equivalent rated radial flux motors air cooled at rated operating point performance data benchmarked against industry leaders validated performance comparisons across three power classes 1 all figures are air cooled class motor power volume l mass kg torque density nm l specific torque nm kg size weight reduction small industrial pumping het ir 19 8 kw 8 5 26 5 4 91 1 58 abb 18 6 kw 23 7 131 5 4 17 0 75 36 vol 20 mass medium large mobility het ir 90 kw 33 117 22 10 6 15 dana 100 kw 68 180 9 95 3 78 48 vol 65 mass large e frac pumping het ir 1 649 kw 972 3 700 21 60 5 68 amerimex 1 728 kw 2 024 8 164 10 87 2 69 48 vol 45 mass all figures air cooled torque density nm l volumetric specific torque nm kg gravimetric size weight reduction het ir as a percentage of competitor volume mass 1 het values from linear labs internal testing competitor values from published product datasheets abb m3bp series dana tm4 sumo amerimex pmg series small industrial pumping het ir 19 8 kw volume 8 5 l mass 26 5 kg torque density 4 91 nm l specific torque 1 58 nm kg vs abb 18 6 kw volume 23 7 l mass 131 5 kg torque density 4 17 nm l specific torque 0 75 nm kg size weight 36 vol 20 mass medium large mobility het ir 90 kw volume 33 l mass 117 kg torque density 22 10 nm l specific torque 6 15 nm kg vs dana 100 kw volume 68 l mass 180 kg torque density 9 95 nm l specific torque 3 78 nm kg size weight 48 vol 65 mass large e frac pumping het ir 1 649 kw volume 972 l mass 3 700 kg torque density 21 60 nm l specific torque 5 68 nm kg vs amerimex 1 728 kw volume 2 024 l mass 8 164 kg torque density 10 87 nm l specific torque 2 69 nm kg size weight 48 vol 45 mass all figures air cooled size weight het ir as of competitor volume mass 1 het values from linear labs internal testing competitor values from published product datasheets integrated system better motors better controllers better software better motors patented het architecture delivers 2 torque density and 50 weight reduction across all power classes from 10 kw to 2 2 mw better controllers purpose built drive electronics optimized for circumferential flux with fault tolerant multi phase ride through that keeps systems running even when phases are lost better software integrated diagnostic and control software enables predictive maintenance real time performance optimization and remote monitoring across deployed fleets scalability from 10 kw to 2 2 mw the het architecture scales across the full industrial power spectrum 10 kw built deployed 20 kw 2 2 mw modeled 10 kw 100 kw 500 kw 1 mw 2 2 mw 90 patents issued or pending worldwide het drone motor group 1 3 uas more mission less motor compact high output electric propulsion for the next generation of unmanned aircraft american engineering less mass less magnet material discuss your aircraft explore the het advantage aircraft concept illustration not a deployed het platform 25 6 lighter motor 9 44 kg vs 12 69 kg¹ 31 7 smaller envelope cylindrical volume comparison¹ 58 1 less magnet mass neodymium 0 93 kg vs 2 22 kg¹ u s built in fort worth texas based motor engineering ¹ het ir98 vs m90c60 in linear labs engineering comparison adjusted mass estimate not flight qualified specifications see comparison basis below portfolio example het ir98 a smaller core a bigger design opportunity the het ir98 is one example from the het drone motor portfolio supporting group 1 3 uas it illustrates our approach give aircraft designers more useful output from less motor with configurations matched to the aircraft and its mission less propulsion mass can free up room in the aircraft weight budget for payload battery capacity or structural margin a compact envelope gives integrators more freedom to package the propulsion system 51 4 kw reported at 100 throttle¹ 206 nm reported at 2 380 rpm¹ 243 94 mm diameter axial length ¹ engineering comparison values not continuous duty ratings motor controller propeller cooling and mission duty cycle must be validated together het ir98 24s22p het ir98 a portfolio example original engineering rendering the het advantage performance that earns its place on the aircraft start with motor level evidence then prove the advantage across the complete propulsion system and the actual mission profile 01 output 15 2 more reported power the comparison reports 51 4 kw for het ir98 versus 44 6 kw for m90c60 at the 100 throttle point more output in a lower mass package is the starting point for a stronger propulsion design 02 packaging less motor more design freedom the het ir98 model is 3 25 kg lighter and 29 mm shorter axially than the benchmark that creates potential room for payload energy storage or tighter airframe integration 03 material efficiency more output less neodymium magnet 0 93 kg of neodymium magnets versus 2 22 kg in the benchmark a 58 1 reduction in magnet mass with more reported output from less critical magnet material 04 system engineering designed around the mission propulsion is more than a motor we start with your power rpm voltage duty cycle cooling and weight targets to evaluate the right het configuration and controller pairing explore the engineering comparison assumptions metric m90c60 het ir98 het difference motor mass 12 69 kg 9 44 kg adjusted 25 6 lower diameter length 257 123 mm 243 94 mm 31 7 less envelope volume neodymium magnet mass 2 22 kg 0 93 kg 58 1 lower output 100 throttle 44 60 kw 51 40 kw 15 2 higher torque 100 throttle 178 90 nm 206 00 nm 15 1 higher basis linear labs m90c60 vs het ir98 technical performance evaluation supplied updated report pages 1 3 the report uses calculated component masses including a 0 6 winding mass adjustment for het volume reduction is derived as 1 243² 94 257² 123 using cylindrical outer envelopes not material volume figures are rounded these are model specific engineering comparisons not claims against every competing motor no flight time payload continuous power airworthiness ndaa or blue uas qualification is implied application specific bench thermal and flight validation remain required the confidential report is not available for public download supporting group 1 3 uas every group engineered for the mission the het drone motor portfolio supports group 1 group 2 and group 3 uas from compact unmanned aircraft to tactical vtol and heavy lift platforms we match the motor configuration to your aircraft s power mass speed and integration requirements group 1 compact unmanned aircraft het motor configurations for smaller platforms where low mass compact packaging and domestic sourcing matter group 1 support configured for your aircraft group 2 tactical vtol longer missions het motor configurations built around endurance propulsion efficiency compact packaging and reliable integration group 2 support configured for your mission group 3 heavy lift cargo long range het motor configurations for higher power aircraft where compact high output propulsion can create meaningful system level value group 3 support configured for your power requirements motor selection and integration are application specific performance figures shown on this page apply to the het ir98 benchmark configuration not every motor configuration across group 1 3 american engineering fort worth texas a domestic propulsion partner not just a part number bring your next aircraft program closer to the team designing its motor work with linear labs on application fit integration requirements and the path from evaluation to production start a technical review domestic content and procurement requirements are reviewed by program u s manufacturing does not by itself establish ndaa or blue uas compliance het drone motor engineering evaluation oem integration switch appearance modernize the weakest system in the ge 1 5 fleet pitchpro 2000 complete pitch system replacement without repowering the challenge aging pitch systems cost the industry billions the ge 1 5 fleet the most widely deployed turbine in north america is aging out pitch system failures are the 1 cause of unplanned downtime 7 000 1 aging turbines in the ge 1 5 fleet 20 2 of downtime caused by pitch system failures 150k 300k 3 all in cost per pitch failure crane parts labor downtime 1 ge vernova 2024 annual report awea fleet data the ge 1 5 series is the most widely deployed turbine platform in north america 2 padman pitch system reliability in wind turbines north american clean energy 2016 windurance reliability studies 3 industry estimates includes crane mobilization replacement parts labor and lost production during downtime the solution pitchpro 2000 complete system replacement a drop in replacement that modernizes every component of the pitch system motor drive plc and diagnostics in a single installation pitchpro 2000 complete pitch system assembly increased uptime eliminate the 1 cause of unplanned downtime with modern fault tolerant components decreased o m costs reduce service calls and extend maintenance intervals with built in diagnostics energy efficiency gains 97 motor efficiency captures more energy from every wind event optimized project returns 12 18 month payback extends turbine life without the cost of repowering system components het motor 97 efficiency 50 lighter ip55 rated keba pitchmaster 2 modern pitch drive with advanced control bachmann plc industrial grade programmable logic controller richardson ultracaps backup power for emergency feathering modular panel pre wired drop in design for fast installation het pitch motor integrated control panel ultracapacitor bank production hardware engineered assembled and tested at our fort worth production facility bachmann keba control stack power distribution panel energy storage rack technician control interface comparison legacy vs pitchpro 2000 component legacy system pitchpro 2000 motor brushed dc or legacy ac induction het permanent magnet 97 efficiency weight standard industrial weight 50 lighter easier nacelle handling drive aging variable frequency drive keba pitchmaster 2 with modern control plc legacy controller limited diagnostics bachmann plc with full scada integration diagnostics manual inspection reactive maintenance real time monitoring predictive alerts installation component by component replacement modular drop in panel single installation motor legacy brushed dc or legacy ac induction new het permanent magnet 97 efficiency weight legacy standard industrial weight new 50 lighter easier nacelle handling drive legacy aging variable frequency drive new keba pitchmaster 2 with modern control plc legacy legacy controller limited diagnostics new bachmann plc with full scada integration diagnostics legacy manual inspection reactive maintenance new real time monitoring predictive alerts installation legacy component by component replacement new modular drop in panel single installation return on investment the economics of modernization 12 18 mo 4 payback period 50 150 4 10 year irr 50k 100k 4 annual savings per turbine 80 4 pitch downtime reduction 4 projected estimates based on linear labs fleet modeling actual results will vary by site conditions turbine age and operating environment why modernization pays for itself 01 extend turbine life 10 15 years without repowering 02 eliminate the 1 cause of unplanned downtime pitch system failures 03 avoid costly crane mobilizations emergency truck rolls and replacement parts 04 recover lost revenue from production downtime across the fleet case study proven in the field lamar light power commercial deployment the pitchpro 2000 system was installed at lamar light power in q1 2026 replacing the legacy electric pitch system on a ge 1 5 mw turbine the drop in retrofit was completed with zero structural modifications operational data confirmed the system s performance across a full range of wind conditions validating efficiency response time and reliability targets installed q1 2026 validated performance confirmed fleet rollout scaling now download pitchpro 2000 one pager industries we serve high torque high efficiency motor systems engineered for the most demanding applications energy wind oil gas grid infrastructure from pitch systems on aging wind fleets to downhole drilling motors and grid scale energy storage the het architecture delivers the torque density and fault tolerance that energy applications demand our pitchpro 2000 is already modernizing the ge 1 5 fleet 80 pitch downtime reduction industrial pumps actuators compressors industrial motors drive 45 of global electricity consumption 1 the het s 2 torque density means smaller lighter motors that eliminate gearboxes in pump drives linear actuators and compressor systems reducing both footprint and maintenance burden 2 torque density 1 iea 4e abb 2023 electric motor systems account for over 45 of global electricity consumption nuclear smr coolant containment moto...