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For the Inventor, By the Inventor

Dachau, Germany

Norbert Huebner

This inventor holds 10 USPTO granted patents and 4 published patent applications and 1 EPO patent. Top assignees: Mtu Aero Engines Ag, Mtu Aero Engines Gmbh, Mtu Motoren-Und Turbinen München Gmbh. Active years: 2003-2020.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Norbert Huebner. Retrieved from https://idiyas.com/inventor/norbert-huebner-f6rbj9ap

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

USPTO Granted Patents = 10 

% Patents Active = 80.0

 

Average Co-Inventor Count = 2.3

ph-index = 3

Forward Citations = 28(Granted Patents)


Location History:

  • Munich, DE (2017)
  • Dachau, DE (2003 - 2020)

Company Filing History:

goldMedal6 out of 505 
 
Mtu Aero Engines Ag
 patents
silverMedal3 out of 378 
 
Mtu Aero Engines Gmbh
 patents
bronzeMedal1 out of 1 
 
Mtu Motoren-Und Turbinen München Gmbh
 patent
4. 1 out of 10,655 
 
United Technologies Corporation
 patents
where one patent can have more than one assignee

Years Active: 2003-2020

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10 patents (USPTO):Explore Patents
1. 10598032 - Gas turbine guide vane element (2020-03-24),
2. 10294795 - High pitch-to-chord turbine airfoils (2019-05-21),
3. 10001083 - Turbofan aircraft engine (2018-06-19),
4. 9896940 - Blade for a gas turbomachine (2018-02-20),
5. 9869184 - Gas turbine blade (2018-01-16),
6. 9695694 - Aircraft engine blading (2017-07-04),
7. 9670783 - Blade of a turbomachine, having passive boundary layer control (2017-06-06),
8. 9617863 - Gas turbine stage (2017-04-11),
9. 9359904 - Blade for a turbomachine, blade arrangement, and turbomachine (2016-06-07),
10. 6503053 - Blade with optimized vibration behavior (2003-01-07),

Title: Biography of Inventor Norbert Huebner

Introduction: Norbert Huebner is a distinguished inventor based in Dachau, Germany. He has made significant contributions to the field of gas turbine technology, holding a total of 10 patents. His innovative designs have advanced the efficiency and performance of turbine engines.

Latest Patents: Among his latest patents is the "Gas turbine guide vane element," which features a guide vane element with a first and second guide vane, distanced by one division in the peripheral direction. This design includes at least one band joining the guide vanes, specifically a radially inner and/or outer band, with a vane-side surface that has a contouring and a groove for the uptake of a sealing element. Another notable patent is for "High pitch-to-chord turbine airfoils," which describes a low-pressure turbine engine component designed for aircraft propulsion. This component includes a disk portion and multiple low-pressure turbine blades with a pitch-to-chord ratio greater than 1.4.

Career Highlights: Norbert Huebner has worked with prominent companies in the aerospace industry, including MTU Aero Engines AG and MTU Aero Engines GmbH. His work has been pivotal in enhancing turbine engine designs and performance.

Collaborations: Throughout his career, Huebner has collaborated with notable colleagues such as Rudolf Stanka and Inga Mahle. These partnerships have contributed to

Profile summary based on public USPTO records.
Data Sources: USPTO Patent Grant XML, Patent Center, EPO & CIPO • Normalized by IDiyas Innovation Graph. Methodology & provenance architecturePlease report any incorrect information to [email protected]
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