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List of MTU Aero Engines patents

List of MTU Aero Engines patents
List of EchoNous patents
List of Pharmajet patents
List of CrowdComfort (software company) patents
List of SBIR/STTR awards granted to Intraband Llc
List of SBIR/STTR awards granted to PARABON NANOLABS, INC.
Patents where
Current Assignee
Name
is
MTU Aero EnginesMTU Aero Engines
Name
Description
Patent Applicant
Current Assignee
Inventor
Patent Jurisdiction
Patent Number
Date of Patent
‌
US Patent 8341841 Method for machining components of a gas turbine and composite material

Patent 8341841 was granted and assigned to MTU Aero Engines on January, 2013 by the United States Patent and Trademark Office.

MTU Aero Engines
MTU Aero Engines
United States Patent and Trademark Office
United States Patent and Trademark Office
8341841
January 1, 2013
‌
US Patent 7806651 Method for designing a low-pressure turbine of an aircraft engine, and low-pressure turbine

Patent 7806651 was granted and assigned to MTU Aero Engines on October, 2010 by the United States Patent and Trademark Office.

MTU Aero Engines
MTU Aero Engines
United States Patent and Trademark Office
United States Patent and Trademark Office
7806651
October 5, 2010
‌
US Patent 7108477 Warning before pump limit or in case of blade failure on a turbomachine

Patent 7108477 was granted and assigned to MTU Aero Engines on September, 2006 by the United States Patent and Trademark Office.

MTU Aero Engines
MTU Aero Engines
United States Patent and Trademark Office
United States Patent and Trademark Office
7108477
September 19, 2006
‌
US Patent 11519296 Bearing chamber housing for a turbomachine

Patent 11519296 was granted and assigned to MTU Aero Engines on December, 2022 by the United States Patent and Trademark Office.

MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
United States Patent and Trademark Office
United States Patent and Trademark Office
11519296
December 6, 2022
‌
US Patent 10112236 Device and method for the manufacture or repair of a three-dimensional object

Patent 10112236 was granted and assigned to MTU Aero Engines on October, 2018 by the United States Patent and Trademark Office.

MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
United States Patent and Trademark Office
United States Patent and Trademark Office
10112236
October 30, 2018
‌
US Patent 11306596 Gas turbine blade impulse body module

MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
United States Patent and Trademark Office
United States Patent and Trademark Office
11306596
April 19, 2022
‌
US Patent 11566524 Method and device for repairing a damaged blade tip of a turbine blade which is armor-plated and provided with a blade coating

Patent 11566524 was granted and assigned to MTU Aero Engines on January, 2023 by the United States Patent and Trademark Office.

MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
United States Patent and Trademark Office
United States Patent and Trademark Office
11566524
January 31, 2023
‌
US Patent 11434785 Jacket ring assembly for a turbomachine

Patent 11434785 was granted and assigned to MTU Aero Engines on September, 2022 by the United States Patent and Trademark Office.

MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
United States Patent and Trademark Office
United States Patent and Trademark Office
11434785
September 6, 2022
‌
US Patent 11371370 Flow arrangement for placing in a hot gas duct of a turbomachine

Patent 11371370 was granted and assigned to MTU Aero Engines on June, 2022 by the United States Patent and Trademark Office.

MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
United States Patent and Trademark Office
United States Patent and Trademark Office
11371370
June 28, 2022
‌
US Patent 7495354 Gas turbine, particularly an aircraft engine

Patent 7495354 was granted and assigned to MTU Aero Engines on February, 2009 by the United States Patent and Trademark Office.

MTU Aero Engines
MTU Aero Engines
United States Patent and Trademark Office
United States Patent and Trademark Office
7495354
February 24, 2009
‌
US Patent 9587499 Inner ring of a fluid flow machine and stator vane array

Patent 9587499 was granted and assigned to MTU Aero Engines on March, 2017 by the United States Patent and Trademark Office.

MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
United States Patent and Trademark Office
United States Patent and Trademark Office
9587499
March 7, 2017
‌
US Patent 10174628 Axially divided inner ring for a turbomachine and guide vane ring

Patent 10174628 was granted and assigned to MTU Aero Engines on January, 2019 by the United States Patent and Trademark Office.

MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
United States Patent and Trademark Office
United States Patent and Trademark Office
10174628
January 8, 2019
‌
US Patent 10982558 Guide vane connection

Patent 10982558 was granted and assigned to MTU Aero Engines on April, 2021 by the United States Patent and Trademark Office.

MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
United States Patent and Trademark Office
United States Patent and Trademark Office
10982558
April 20, 2021
‌
US Patent 11499437 Sealing apparatus for a turbomachine, seal-carrier ring element for a sealing apparatus, and turbomachine

Patent 11499437 was granted and assigned to MTU Aero Engines on November, 2022 by the United States Patent and Trademark Office.

MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
United States Patent and Trademark Office
United States Patent and Trademark Office
11499437
November 15, 2022
‌
US Patent 7575412 Anti-stall casing treatment for turbo compressors

Patent 7575412 was granted and assigned to MTU Aero Engines on August, 2009 by the United States Patent and Trademark Office.

MTU Aero Engines
MTU Aero Engines
United States Patent and Trademark Office
United States Patent and Trademark Office
7575412
August 18, 2009
‌
US Patent 8678742 Clearance control system, turbomachine and method for adjusting a running clearance between a rotor and a casing of a turbomachine

Patent 8678742 was granted and assigned to MTU Aero Engines on March, 2014 by the United States Patent and Trademark Office.

MTU Aero Engines
MTU Aero Engines
United States Patent and Trademark Office
United States Patent and Trademark Office
8678742
March 25, 2014
‌
US Patent 10035223 Repair method for the additive repair of a component

Patent 10035223 was granted and assigned to MTU Aero Engines on July, 2018 by the United States Patent and Trademark Office.

MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
United States Patent and Trademark Office
United States Patent and Trademark Office
10035223
July 31, 2018
‌
US Patent 11319820 Blade or guide vane with raised areas

Patent 11319820 was granted and assigned to MTU Aero Engines on May, 2022 by the United States Patent and Trademark Office.

MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
United States Patent and Trademark Office
United States Patent and Trademark Office
11319820
May 3, 2022
‌
US Patent 9068471 Clearance control system, turbomachine and method for adjusting a running clearance between a rotor and a casing of a turbomachine

Patent 9068471 was granted and assigned to MTU Aero Engines on June, 2015 by the United States Patent and Trademark Office.

MTU Aero Engines
MTU Aero Engines
United States Patent and Trademark Office
United States Patent and Trademark Office
9068471
June 30, 2015
‌
US Patent 7294361 Method and device for gas phase diffusion coating of metal components

Patent 7294361 was granted and assigned to MTU Aero Engines on November, 2007 by the United States Patent and Trademark Office.

MTU Aero Engines
MTU Aero Engines
United States Patent and Trademark Office
United States Patent and Trademark Office
7294361
November 13, 2007
‌
US Patent 9696142 Method and apparatus for determining residual stresses of a component

Patent 9696142 was granted and assigned to MTU Aero Engines on July, 2017 by the United States Patent and Trademark Office.

MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
United States Patent and Trademark Office
United States Patent and Trademark Office
9696142
July 4, 2017
‌
US Patent 10428668 Vane segment with peripheral securing

Patent 10428668 was granted and assigned to MTU Aero Engines on October, 2019 by the United States Patent and Trademark Office.

MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
MTU Aero Engines
United States Patent and Trademark Office
United States Patent and Trademark Office
10428668
October 1, 2019
‌
US Patent 7637719 Sealing arrangement

Patent 7637719 was granted and assigned to MTU Aero Engines on December, 2009 by the United States Patent and Trademark Office.

MTU Aero Engines
MTU Aero Engines
United States Patent and Trademark Office
United States Patent and Trademark Office
7637719
December 29, 2009
‌
US Patent 6935833 Recirculation structure for turbo chargers

Patent 6935833 was granted and assigned to MTU Aero Engines on August, 2005 by the United States Patent and Trademark Office.

MTU Aero Engines
MTU Aero Engines
United States Patent and Trademark Office
United States Patent and Trademark Office
6935833
August 30, 2005
‌
US Patent 8992172 Turbo engine

Patent 8992172 was granted and assigned to MTU Aero Engines on March, 2015 by the United States Patent and Trademark Office.

MTU Aero Engines
MTU Aero Engines
United States Patent and Trademark Office
United States Patent and Trademark Office
8992172
March 31, 2015
...
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