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Trollhättan, Sweden

Volvo Aero Corporation

USPTO Granted Patents = 85

% Expired Patents = 55.3

CIPO Patents = 2

EPO Patents = 12

Forward Citations = 718

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100 inventors (with patents filed for the assignee):

Jan Lundgren (11 out of 12 patents)

Arne Boman (7 out of 7 patents)

Jan Häggander (7 out of 7 patents)

4. Bertil Jönsson (7 out of 7 patents)

5. Jan Häggander (6 out of 6 patents)

6. Hans Mårtensson (5 out of 7 patents)

7. Anders Sjunnesson (5 out of 5 patents)

8. Anders Erik Lundbladh (4 out of 5 patents)

9. Mats Hallqvist (4 out of 4 patents)

10. Bernhard Gustafsson (4 out of 4 patents)

11. Lars Sundin (3 out of 10 patents)

12. Martin Nilsson (3 out of 6 patents)

13. Per Henrikson (3 out of 3 patents)

14. Lars-Olof Pekkari (3 out of 3 patents)

15. Robert Lundberg (3 out of 4 patents)

Core Competencies:

Gas Turbine

Engine Component

Thermal Barrier

Noise Attenuation

Vane

Stator

Rocket Engine

Compressor Structure

Fuel Injector

Outlet Nozzle

Combustion Chamber

Blade

85 patents: Sort by Forward Citations

1. 8944139 - Method for manufacturing an engine component (2015-02-03),

2. 8888451 - Method for producing a vane, such a vane and a stator component comprising the vane (2014-11-18),

3. 8794912 - Strut and a gas turbine structure comprising the strut (2014-08-05),

4. 8757979 - Rotor element and method for producing the rotor element (2014-06-24),

5. 8757965 - Gas turbine compression system and compressor structure (2014-06-24),

6. 8757919 - Component and a gas turbine engine comprising the component (2014-06-24),

7. 8747066 - Gas turbine housing component (2014-06-10),

8. 8708647 - Liner for a turbine section, a turbine section, a gas turbine engine and an aeroplane provided therewith (2014-04-29),

9. 8689540 - Component configured for being subjected to high thermal load during operation (2014-04-08),

10. 8551266 - Method, alloy and component (2013-10-08),

11. 8528344 - Bleed structure for a bleed passage in a gas turbine engine (2013-09-10),

12. 8485783 - Gas turbine engine (2013-07-16),

13. 8484982 - Bleed structure for a bleed passage in a gas turbine engine (2013-07-16),

14. 8464831 - Noise attenuation panel and a gas turbine component comprising a noise attenuation panel (2013-06-18),

15. 8459942 - Gas turbine engine component, a turbojet engine provided therewith, and an aircraft provided therewith (2013-06-11),

Volvo Aero Corporation, based in Trollhättan, Sweden, specializes in advanced gas turbine technology, focusing on the development and manufacturing of critical engine components. The company is renowned for its expertise in thermal barrier coatings, noise attenuation solutions, and the design of vanes and stators for both gas turbine and rocket engines. With a commitment to innovation, Volvo Aero plays a pivotal role in enhancing the performance and efficiency of aerospace propulsion systems, contributing to the advancement of the aerospace industry.

Profile summary based on public USPTO records.

Company Badge

USPTO Data Jan 1 1976 - Sep 29 2026

85 Patents

#1 in Trollhättan

#85 in Sweden

#8,944 in the World

Trollhättan, Sweden

Volvo Aero Corporation

Forward Citations = 718

100 inventors:

Jan Lundgren (11 out of 12 patents)

Arne Boman (7 out of 7 patents)

Jan Häggander (7 out of 7 patents)

4. Bertil Jönsson (7 out of 7 patents)

5. Jan Häggander (6 out of 6 patents)

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