Inventor
Claude Marcel Mons
Inventor
Savigny le Temple, FR
Overview
Patents· 44 as inventor
Public. Assignee & technology derived from the patent record. Each patent links to its LexDana page.
F01Dprimary
F01DNon-positive displacement machines or engines, e.g. steam turbines17%
F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants13%
Y02TClimate change mitigation technologies related to transportation12%
Y10TTechnical subjects covered by former us classification9%
F04DNon-positive-displacement pumps5%
B22FWorking metallic powder4%
B23PMetal-working not otherwise provided for3%
Y02PClimate change mitigation technologies in the production or processing of goods3%
B23KSoldering or unsoldering3%
C21DModifying the physical structure of ferrous metals3%
PatentTitleYear
8,888,448'Method for the manufacture of a circular revolution thermomechanical part including a titanium-based load-bearing substrate lined with steel or superalloy, a turbomachine compressor housing which is resistant to titanium fire obtained according to this method'20148,881,395'Method for increasing the coefficient of adhesion between two parts rotating as one with a rotor'20148,839,516'Repairing titanium compressor blades by cold compacting'20148,662,838'Compressor housing resistant to titanium fire, high-pressure compressor including such a housing and aircraft engine fitted with such a compressor'20148,607,456'Method of using laser shock impacts to produce raised elements on a wall surface capable of being swept by a fluid in order to control the intensity of turbulence in a transition zone'20138,561,386'Wall cooling device'20138,448,446'Actuating device, bypass air bleed system equipped therewith, and turbojet engine comprising these'20138,322,125'Turbo-engine compressor tip comprising de-icing means'20128,256,116'Method of using laser shock impacts to produce raised elements on a wall surface capable of being swept by a fluid in order to control the intensity of turbulence in a transition zone'20128,209,834'Centering a part inside a shaft'20128,192,560'Hardened martensitic steel, method for producing a component from this steel and component obtained in this manner'20128,161,727'System providing braking in a gas turbine engine in the event of the turbine shaft breaking'20128,152,938'Hardened martensitic steel, method for producing a component from this steel and component obtained in this manner'20128,153,056'Hardened martensitic steel, method for producing a component from this steel and component obtained in this manner'20128,136,999'Turbomachine shaft guidance'20128,127,525'System for dissipating energy in the event of a turbine shaft breaking in a gas turbine engine'20127,934,367'Method and device for reducing the speed in the event of breakage of a gas turbine engine turbine shaft'20117,857,581'Annular wiper for a sealing labyrinth, and its method of manufacture'20107,836,572'Method of making a wiper for a sealing labyrinth, and a thermomechanical part and a turbomachine including such a wiper'20107,695,248'Method of making a rim situated at the free end of a blade, a blade obtained by the method, and a turbomachine fitted with the blade'20107,687,021'Method of fabricating a casing for turbine stator'20107,685,712'Method for repairing a rubbing surface of a turbomachine variable-pitch blade'20107,625,176'Plain bearing between two parts which are movable with respect to each other'20097,597,538'Thermostructural turbomachine part that is circularly symmetrical about a longitudinal axis, the part including an annular wiper, and a method of manufacture'20097,553,130'Nozzle ring adhesive bonded blading for aircraft engine compressor'20097,510,778'Part for protecting the leading edge of a blade'20097,448,280'Method for evaluating the fatigue strength of welded joints'20087,422,644'Thin parts made of β or quasi-β titanium alloys; manufacture by forging'20087,367,774'System for protecting a main shaft of an engine having a fusible bearing'20087,360,986'System for blocking a main shaft of an engine having a fusible bearing'20087,261,784'Method of making a coating on a metal substrate and/or an article, such a coating, such a metal substrate and/or an article, and a cam forming such an article'20077,234,920'Turbine casing having refractory hooks and obtained by a powder metallurgy method'20077,147,434'Nozzle ring with adhesive bonded blading for aircraft engine compressor'20067,037,389'Thin parts made of β or quasi-β titanium alloys; manufacture by forging'20066,991,433'Drum, in particular a drum forming a turbomachine rotor, a compressor, and a turboshaft engine including such a drum'20066,890,368'Dry self-lubricating dense material; a mechanical part formed from said material; a method of manufacturing said material'20056,881,029'Casing, a compressor, a turbine, and a combustion turbine engine including such a casing'20056,837,085'Transverse ultrasound peening of blades on a rotor'20056,783,642'Method of making labyrinth seal lips for the moving parts of turbomachines'20046,336,844'Method and machine for the ultrasonic peening of parts on a wheel'20026,289,705'Method for the ultrasonic peening of large sized annular surfaces of thin parts'20016,135,712'Turbomachine with mutual braking of concentric shafts'20004,423,097'Abradable seal and its method of production'19834,392,656'Air-cooled sealing rings for the wheels of gas turbines'1983Career & activity timeline
Assembled from patent assignee/location history and declaration credentials.
1983–2014Patents assigned to SNECMA (29)· patent assignee history
1983–2014Based in Savigny le Temple, FR· patent location history
2001–2012Patents assigned to SNECMA MOTEURS (14)· patent assignee history
2012–2014Patents assigned to MONS CLAUDE MARCEL (13)· patent assignee history
2012Patents assigned to ROUSSELIN STEPHANE (4)· patent assignee history
2012Patents assigned to AUBERT & DUVAL SA (3)· patent assignee history
Inventor activity
Assignee and location history derived from the patent record.
Assignees
| Assignee | Patents | Span |
|---|---|---|
| SNECMA | 29 | 1983–2014 |
| SNECMA MOTEURS | 14 | 2001–2012 |
| MONS CLAUDE MARCELself | 13 | 2012–2014 |
| ROUSSELIN STEPHANE | 4 | 2012 |
| AUBERT & DUVAL SA | 3 | 2012 |
Locations
| Location | Patents | Span |
|---|---|---|
| Savigny le Temple, FR | 44 | 1983–2014 |