Moscow, Russia

Galina Andreevna Babaeva

This inventor holds 3 USPTO granted patents. Top assignees: Oktrytoe Aktsionernoe Obschestvo 'Nauchno-Proizvodstvennoe Obiedinenie, Otkrytoe Aktsionernoe Obschestvo, Otkrytoe Aktsionernoe Obschestvo Nauchno-Proizvodstvennoe Obiedinenie. Active years: 2000-2002.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Galina Andreevna Babaeva. Retrieved from https://idiyas.com/inventor/galina-andreevna-babaeva

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


% Patents Active = 100.0

Average Co-Inventor Count = 6.4

ph-index = 3

Forward Citations = 34(Granted Patents)


Company Filing History:


Years Active: 2000-2002

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3 patents (USPTO):Explore Patents

Title: Galina Andreevna Babaeva: Innovator in Rocket Engine Technology

Introduction

Galina Andreevna Babaeva is a prominent inventor based in Moscow, Russia. She has made significant contributions to the field of rocket engine technology, holding a total of 3 patents. Her innovative designs focus on enhancing the efficiency and performance of liquid-fuel rocket engines.

Latest Patents

One of her latest patents is for a combustion chamber casing of a liquid-fuel rocket engine. This casing comprises a combustion chamber and a nozzle, which includes subsonic and supersonic sections with an external structural envelope and a fire wall featuring a ribbed external surface. The regenerative cooling passage is formed between the envelope and the fire wall, which is made from copper or a copper alloy, while the external structural envelope is constructed from steel or a nickel alloy. The fire wall has a metal coating stratified in the region of the nozzle throat, with specific thicknesses for the nickel and chromium layers.

Another notable patent is a method for producing a welded-brazed combustion chamber. This combustion chamber for a liquid-propellant rocket engine includes an injector head jointed to a combustion chamber casing with an exhaust head on the nozzle output. The casing is made of a steel jacket and a bronze-steel internal fire wall, which are joined together and contain shells connected in series. The exhaust head and shells of the casing are brazed using a solder based on nickel, chromium, and manganese, while parts of the injector head and other members are brazed using a copper-silver solder.

Career Highlights

Galina has worked with notable companies such as Otkrytoe Aktsionernoe Obschestvo and Otkrytoe Aktsionernoe Obschestvennoe Nauchno-Proizvodstvennoe Obiedinenie. Her work in these organizations has allowed her to develop and refine her innovative technologies in rocket engineering.

Collaborations

Throughout her career, Galina has collaborated with esteemed colleagues, including Alexandr Alexandrovich Vasin and Jury Alexandrovich Pestov. These partnerships have contributed to her success and the advancement of her inventions.

Conclusion

Galina Andreevna Babaeva is a trailblazer in the field of rocket engine technology, with a focus on innovative designs that enhance performance and

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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