Inventor profile of:

Markus GIBBERT

City:

Hamburg

Country:

Germany

Published Applications:

10

Last publication date:

2026-05-14

Top Assignees for applications by Markus GIBBERT

The entities that hold a legal rights for patent applications filed by inventor GIBBERT Markus:

Recent patent applications by GIBBERT Markus

Markus GIBBERT from Hamburg, DE has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2026-05-14
US20260131886A1
Performing operations; transporting

ACTUATION MECHANISM FOR A HIGH LIFT SYSTEM, ASSOCIATED HIGH LIFT SYSTEM, AIRCRAFT AND METHOD OF ACTUATING A HIGH LIFT SYSTEM

#2 | 2023-11-02
US20230348039A1
Performing operations; transporting

FAIRING ATTACHMENT SYSTEM FOR A WING OF AN AIRCRAFT, AIRCRAFT WING AND METHOD FOR MOUNTING A FAIRING DEVICE

#3 | 2021-10-28
US20210331782A1
Performing operations; transporting

System for driving a flap arrangement between a retracted position and an extended position

#4 | 2021-09-02
US20210269142A1
Performing operations; transporting

Support stay and support arrangement for supporting a movable part of an aircraft

#5 | 2020-03-05
US20200070954A1
Performing operations; transporting

Wing system for an aircraft with a flow body and a cover panel

#6 | 2020-01-16
US20200017193A1
Performing operations; transporting

System for driving a flap arrangement between a retracted position and an extended position

#7 | 2020-01-16
US20200017192A1
Performing operations; transporting

System for driving a flap arrangement between a retracted position and an extended position

#8 | 2019-12-05
US20190367158A1
Performing operations; transporting

SYSTEM FOR DRIVING A FLAP ARRANGEMENT BETWEEN A RETRACTED POSITION AND AN EXTENDED POSITION

#9 | 2019-12-05
US20190367157A1
Performing operations; transporting

SYSTEM FOR DRIVING A FLAP ARRANGEMENT BETWEEN A RETRACTED POSITION AND AN EXTENDED POSITION

#10 | 2019-08-08
US20190241250A1
Performing operations; transporting

Linkage mechanism for linking a flaperon to a droop panel of an aircraft

InventorID:

2579390 ⎘