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For the Inventor, By the Inventor

Trollhättan, Sweden

Volvo Aero Corporation


USPTO Granted Patents = 85



Forward Citations = 697

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115 inventors (with patents filed for the assignee):

goldMedal Jan Lundgren (11 out of 12 patents)

silverMedal Arne Boman (7 out of 7 patents)

bronzeMedal 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 3 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
Engine Component Manufacturing
Vane Production
Compressor Structure
Noise Attenuation Panel
Stator for Jet Engine
Propulsion System
Thermal Load Components
Welding Area Monitoring
Rocket Engine Manufacturing
Flow Machine Blade
Afterburner Fuel-Feed Arrangement

85 patents:

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 is a aerospace engineering company specializing in the design, manufacturing and maintenance of aircraft engines. With a history dating back over 80 years, Volvo Aero has established itself as a leading provider of innovative solutions for the global aviation industry. The company offers a wide range of products and services, including engine components, maintenance and overhaul services, as well as aftermarket support. Volvo Aero is committed to delivering cutting-edge technology and performance to ensure the safety and efficiency of aircraft worldwide.
This text is generated by artificial intelligence and may not be accurate.

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USPTO Data Jan 1 1976 - Dec 9 2025

85 Patents

#1 in Trollhättan

#86 in Sweden

#8,664 in the World

...
Trollhättan, Sweden

Volvo Aero Corporation

Forward Citations = 697

115 inventors:

goldMedal Jan Lundgren (11 out of 12 patents)

silverMedal Arne Boman (7 out of 7 patents)

bronzeMedal 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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