Learn more

SNEKMA

Overview
  • Total Patents
    1,083
  • GoodIP Patent Rank
    21,883
About

SNEKMA has a total of 1,083 patent applications. Its first patent ever was published in 2004. It filed its patents most often in Russian Federation and Ukraine. Its main competitors in its focus markets engines, pumps and turbines, environmental technology and machines are SNECMA, SNECMA SA and ROLLS ROYCE DEUTSCHLAND.

Patent filings in countries

World map showing SNEKMAs patent filings in countries
# Country Total Patents
#1 Russian Federation 1,082
#2 Ukraine 1

Patent filings per year

Chart showing SNEKMAs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Russelehn Stefan 27
#2 Supizon Zhan-Ljuk 26
#3 Galle Fransua 22
#4 Kup Dominik 17
#5 Bel Mont Oliv E 16
#6 Sandeli Deni Zhan Moris 16
#7 Burju Mishel Andre 15
#8 Kommare Patris Andre 14
#9 Ehrnandes Did E 14
#10 Ehrnandez Did E Ippolit 13

Latest patents

Publication Filing date Title
RU2670711C1 Drained fluid evacuation stub for propulsion assembly
RU2677312C2 Turbine engine provided with means of absorbing stresses from thrust of engine thereof
RU2638883C2 Engine control device
RU2636602C2 Method for monitoring engine start cycle of gas-turbine plant
RU2646167C2 Air exhaust tube holder in turbomachine
RU2635435C2 System for equipment components assembly check
RU2642142C2 Method and system for measuring with plurality of sensors
RU2642228C2 Method for producing ceramic core for movable blade, ceramic core and movable blade
RU2617633C2 Gas turbine blades with an end section shifted towards the high pressure and cooling channels
RU2616066C2 Pressure holding device for manufacture of composite parts by resin injection and appropriate method
RU2594323C2 Turbo-machine containing film damping fluid of guide bearing shaft of turbine machine, and method of controlling thickness of said film of damping fluid
RU2599320C2 Method of drilling combustion chamber wall
RU2572731C2 Hydraulic device of control system, such as propeller pitch change device
RU2581262C2 Turbomachine
RU2564471C2 Compressor for engine, particularly, aircraft turbojet equipped with air intake system
RU2558411C2 Open air propeller for turbine machine
RU2567143C2 Method and device for electrolytic deposition of coating
RU2533384C2 Blade of propeller for aircraft
RU2559904C2 Hub for propeller with polygonal reinforced ring and turbomachine equipped by such hub
RU2548535C2 Insulation of circular protruding edge of external turbomachine casing in respect to relevant annular sector, turbomachine stage and turbomachine