Inventor profile of:

Pascal GARDES

City:

LEVIGNAC

Country:

France

Published Applications:

12

Last publication date:

2020-11-19

Top Assignees for applications by Pascal GARDES

The entities that hold a legal rights for patent applications filed by inventor GARDES Pascal:

Recent patent applications by GARDES Pascal

Pascal GARDES from LEVIGNAC, FR has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2020-11-19
US20200362708A1
Mechanical engineering

Turbofan comprising a set of rotatable blades for blocking off the bypass flow duct

#2 | 2020-10-15
US20200325848A1
Mechanical engineering

Turbofan comprising a set of rotatable blades for blocking off the bypass flow duct

#3 | 2020-10-15
US20200325785A1
Mechanical engineering

Turbofan comprising a set of rotatable blades for blocking off the bypass flow duct

#4 | 2020-10-08
US20200318574A1
Mechanical engineering

Turbofan comprising a nacelle equipped with a reverser system and a mobile cascade grill

#5 | 2020-07-30
US20200240359A1
Mechanical engineering

Turbofan comprising a set of rotatable blades for blocking off the bypass flow duct

#6 | 2020-06-18
US20200191156A1
Mechanical engineering

Turbofan comprising a set of rotatable blades for blocking off the bypass flow duct

#7 | 2020-06-18
US20200189759A1
Performing operations; transporting

Propulsion assembly for an aircraft, comprising a load support

#8 | 2020-04-23
US20200122409A1
Performing operations; transporting

Bypass turbofan engine comprising a nacelle equipped with a translationally-mobile thrust-reversal system and with a fan case equipped with supports

#9 | 2020-03-12
US20200080513A1
Mechanical engineering

Jet engine comprising a nacelle equipped with a reverser system comprising inner doors and outer flaps

#10 | 2020-01-23
US20200025141A1
Mechanical engineering

Jet engine comprising a nacelle equipped with reverser flaps provided with vortex-generating means

#11 | 2019-09-19
US20190284952A1
Mechanical engineering

Turbofan comprising a series of rotatable blades for blocking off the bypass flow duct

#12 | 2019-09-19
US20190283892A1
Performing operations; transporting

Turbojet engine comprising a nacelle equipped with a fan case and with a fixed structure

InventorID:

2622202 ⎘