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name:-0.0096790790557861
name:-0.010175943374634
name:-0.0062739849090576
Scharl; Richard Patent Filings

Scharl; Richard

Patent Applications and Registrations

Patent applications and USPTO patent grants for Scharl; Richard.The latest application filed is for "blade of a turbomachine, including a cooling channel and a displacement body situated therein, as well as a method for manufacturing".

Company Profile
5.7.9
  • Scharl; Richard - Karlsfeld DE
*profile and listings may contain filings by different individuals or companies with the same name. Review application materials to confirm ownership/assignment.
Patent Activity
PatentDate
Gas turbine component
Grant 11,248,484 - Schlothauer , et al. February 15, 2
2022-02-15
Seal carrier, guide vane ring and turbomachine
Grant 10,533,569 - Jakimov , et al. Ja
2020-01-14
Method for additive manufacturing of a gas turbine casing part
Grant 10,443,445 - Liebl , et al. Oc
2019-10-15
Guide vane ring for a turbomachine
Grant 10,280,775 - Liebl , et al.
2019-05-07
Blade Of A Turbomachine, Including A Cooling Channel And A Displacement Body Situated Therein, As Well As A Method For Manufacturing
App 20190078446 - Scharl; Richard ;   et al.
2019-03-14
Turbomachine Sealing Element
App 20190010819 - Ladewig; Alexander ;   et al.
2019-01-10
Shaft seal system and a compressor having a corresponding shaft seal system
Grant 10,030,585 - Flouros , et al. July 24, 2
2018-07-24
Turbomachine Blade System
App 20180142558 - Scharl; Richard
2018-05-24
Seal Carrier, Guide Vane Ring And Turbomachine
App 20160377087 - Jakimov; Andreas ;   et al.
2016-12-29
Method For Additive Manufacturing Of A Gas Turbine Casing Part
App 20160290164 - Liebl; Christian ;   et al.
2016-10-06
Gas turbine component
App 20160230582 - Schlothauer; Steffen ;   et al.
2016-08-11
Guide Vane Ring For A Turbomachine
App 20160222807 - Liebl; Christian ;   et al.
2016-08-04
Shaft Seal System And A Compressor Having A Corresponding Shaft Seal System
App 20160061116 - FLOUROS; Michael ;   et al.
2016-03-03
Turbine engine and bladed rotor for a compression stage of a turbine engine
Grant 7,399,164 - Scharl July 15, 2
2008-07-15
Turbine engine and bladed rotor for a compression stage of a turbine engine
App 20070134100 - Scharl; Richard
2007-06-14
Nozzle ring for an aircraft engine gas turbine
Grant 6,543,998 - Scharl April 8, 2
2003-04-08

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