| 11309994 |
Highly parallel and scalable cyclic redundancy check |
— |
2022-04-19 |
| 10331601 |
Systems, apparatus, and methods for efficient space to time conversion of OTU multiplexed signal |
Vinod Narippatta, Unnikrishnan C V, Sanjay D. Kamat, Ashok Tatineni, Vishwanathan Paramasivam |
2019-06-25 |
| 10309315 |
Variable area nozzle assisted gas turbine engine restarting |
Michael Winter |
2019-06-04 |
| 9729245 |
Using artificial justifications to apply noise shaping to actual justifications associated with mapping client data |
— |
2017-08-08 |
| 9611758 |
Gas turbine engine systems involving integrated fluid conduits |
— |
2017-04-04 |
| 9479849 |
OTU4 one level de-multiplexing spatial framer for G.709 optical transport networks |
Vishwanathan Paramasivam, Ashok Tatineni |
2016-10-25 |
| 9328666 |
Variable area nozzle assisted gas turbine engine restarting |
Michael Winter |
2016-05-03 |
| 9228534 |
Variable contour nacelle assembly for a gas turbine engine |
Michael Winter |
2016-01-05 |
| 9004399 |
Nacelle flow assembly |
— |
2015-04-14 |
| 8935073 |
Reduced take-off field length using variable nozzle |
Wayne Hurwitz |
2015-01-13 |
| 8727267 |
Variable contraction ratio nacelle assembly for a gas turbine engine |
Michael Winter |
2014-05-20 |
| 8720182 |
Integrated variable area nozzle and thrust reversing mechanism |
— |
2014-05-13 |
| 8657567 |
Nacelle compartment plenum for bleed air flow delivery system |
Thomas G. Cloft |
2014-02-25 |
| 8650854 |
Bifurcation and aft vent used to vary fan nozzle exit area |
Edward F. Migliaro, Jr., Michael Winter |
2014-02-18 |
| 8596573 |
Nacelle flow assembly |
— |
2013-12-03 |
| 8408491 |
Nacelle assembly having inlet airfoil for a gas turbine engine |
Michael Winter |
2013-04-02 |
| 8402739 |
Variable shape inlet section for a nacelle assembly of a gas turbine engine |
Zaffir A. Chaudhry |
2013-03-26 |
| 8282037 |
Nacelle flow assembly |
— |
2012-10-09 |
| 8240979 |
Gas turbine engine systems involving integrated fluid conduits |
— |
2012-08-14 |
| 8209950 |
Detecting ice buildup on an aircraft engine and actuating the turbofan exit nozzle to break the ice |
Michael Winter |
2012-07-03 |
| 8209953 |
Gas turbine engine system providing simulated boundary layer thickness increase |
Michael Winter |
2012-07-03 |
| 8205430 |
Variable geometry nacelle assembly for a gas turbine engine |
— |
2012-06-26 |
| 8137060 |
Actuation of a turbofan engine bifurcation to change an effective nozzle exit area |
Michael Winter |
2012-03-20 |
| 7870721 |
Gas turbine engine providing simulated boundary layer thickness increase |
Michael Winter |
2011-01-18 |
