MRA SYSTEMS LLC has a total of 68 patent applications. It decreased the IP activity by 30.0%. Its first patent ever was published in 2009. It filed its patents most often in EPO (European Patent Office), United States and China. Its main competitors in its focus markets engines, pumps and turbines, environmental technology and transport are SAFRAN NACELLES, ROHR INC and WELCH JOHN M.
# | Country | Total Patents | |
---|---|---|---|
#1 | EPO (European Patent Office) | 21 | |
#2 | United States | 17 | |
#3 | China | 11 | |
#4 | Japan | 6 | |
#5 | Canada | 5 | |
#6 | Brazil | 4 | |
#7 | WIPO (World Intellectual Property Organization) | 4 |
# | Industry | |
---|---|---|
#1 | Engines, pumps and turbines | |
#2 | Environmental technology | |
#3 | Transport | |
#4 | Consumer goods | |
#5 | Surface technology and coating | |
#6 | Mechanical elements |
# | Technology | |
---|---|---|
#1 | Climate change mitigation in transportation | |
#2 | Special non-positive-displacement engines | |
#3 | Jet-propulsion plants | |
#4 | Gas-turbine plants | |
#5 | Parachutes | |
#6 | Steam turbines | |
#7 | Aeroplanes | |
#8 | Sound-producing devices | |
#9 | Layered products | |
#10 | Pipes |
# | Name | Total Patents |
---|---|---|
#1 | Howarth Graham Frank | 37 |
#2 | Roach Andrew Michael | 31 |
#3 | Calder David Patrick | 21 |
#4 | Beasman Timothy Robert | 11 |
#5 | Andrew Michael Roach | 10 |
#6 | Graham Frank Howarth | 6 |
#7 | Timothy Robert Beasman | 5 |
#8 | Shetty Shailesh Kumar | 4 |
#9 | Periasamy Murugesan | 4 |
#10 | David Patrick Calder | 4 |
Publication | Filing date | Title |
---|---|---|
US2020031487A1 | Nacelle inlet lip fuse structure | |
US2019285028A1 | Thrust reverser cascade | |
US2019257268A1 | Thrust reverser cascade | |
US2019063318A1 | Acoustic liner having internal structure | |
US2019048824A1 | Turbine engine thrust reverser stop | |
CN108661821A | Thrust reverser component and operating method | |
US2018245516A1 | Acoustic liner and method of forming an acoustic liner | |
US2018245515A1 | Acoustic liner having multiple layers | |
US2018142624A1 | Engine door with burst seal | |
US2017356343A1 | Thermal insulation blanket and thermal insulation blanket assembly | |
US2017321632A1 | Gas turbine engine with thrust reverser assembly and method of operating | |
US2018016987A1 | Acoustic liners for use in a turbine engine | |
EP3024729A1 | Aircraft engine pylon | |
EP2354469A2 | Turbomachine Nacelle And Anti-Icing System And Method Therefor | |
EP2370674A1 | Nacelle and method of assembling the same |