1
Schievelbusch Bernd: Device for detecting the asymmetric deflection of aircraft high lift surfaces. Liebherr Aerospace, March 22, 2006: EP1637453-A2 (2 worldwide citation)

An assembly checks the geometric alignment of leading edge and trailing edge lift devices e.g. slats and flaps on the wing of an aircraft. The assembly has a light source (6) at the wing tip linked by a fibre optic cable (5) to a photodiode light sensor (7) at the wing root. The signal received at t ...


2
Schievelbusch Bernd: Device for monitoring the synchronism of flaps of an airplane wing. Liebherr Aerospace, October 22, 2008: EP1982916-A2 (2 worldwide citation)

The device has a Bowden cable staying in connection with flaps in such a manner that the Bowden cable follows flap movement. A shift path of the Bowden cable extends from one point to another point, where one or both the points are arranged at non movable structural components of an airplane wing. T ...


3
SCHIEVELBUSCH BERND, HAUBER BERNHARD: [fr] Système dhypersustentation daéronef et procédé de détermination de son état de fonctionnement, [de] Flugzeughochauftriebssystem sowie Verfahren zur Ermittlung eines Betriebszustandes eines Flugzeughochauftriebssystems, [en] Aircraft high-lift system and method for determining the operational state of same. LIEBHERR AEROSPACE, November 17, 2010: EP2251258-A2 (1 worldwide citation)

[en] The airplane high lift system (10) comprises a loading station (22,24,32,34) for activation of a butterfly valve (20,30) of an airfoil, particularly a landing flap or a fore flap. A transmission (17) is provided with the transmission sections (42,44,46). An operating mode of the transmission or ...


4
Schievelbusch Bernd: A drive system for slats / flaps of an aircraft wing. Liebherr Aerospace, November 12, 2008: GB2449172-A (1 worldwide citation)

A drive system for the flaps / slats of an aircraft wing comprises drive shafts which are connected to the flaps, and comprises one or more servo motor units 30 connected to the drive shafts, wherein the drive shafts can be selectively coupled with one another. Ideally, a first drive shaft 12 is con ...


5
Schievelbusch Bernd: Aircraft high-lift device system with overload protection. Liebherr Aerospace, March 25, 2009: EP2039605-A2 (1 worldwide citation)

Die vorliegende Erfindung betrifft ein Flugzeughochauftriebsystem mit wenigstens einer Antriebseinheit (1) zum Betrieb der Hochauftriebssysteme (10) der Halbflügel (Halbflügelsysteme) sowie mit wenigstens einer Überlastsicherung zur Vermeidung unerwünscht hoher Betriebsmomente in den Halbflügelsyste ...


6
Schievelbusch Bernd: Aircraft lift augmentation system with overload protection. Liebherr Aerospace, September 1, 2004: EP1452442-A1

The operating drive has a central drive system, coupled to elements for transmission of the drive energy over the full width of the wing to individual drive stations (10) for the different landing flaps. Overload protection is provided by a number of electrical load sensors, associated with the poin ...


7
KLEINHANS REINHOLD DIPL ING, HUTH STEFAN DIPL ING, WEISS WERNER DIPL ING, SCHIEVELBUSCH BERND: High-lift system for an aircraft, Hochauftriebssystem eines Luftfahrzeuges, Système de portance élevée dun aéronef. LIEBHERR AEROSPACE, April 4, 2012: EP2436597-A2

Die vorliegende Erfindung betrifft ein Hochauftriebssystem eines Luftfahrzeuges mit wenigstens einer Antriebseinheit, mit wenigstens einer Laststation sowie mit einer oder mehreren Transmissionen zur Übertragung der Antriebsenergie der Antriebseinheit an die wenigstens eine Laststation, wobei eine o ...


8
SCHIEVELBUSCH BERND: DISPOSITIF DE DETECTION DERREURS SYNCHRONES DE SURFACES A PORTANCE ELEVEE SUR UN AERONEF, DEVICE FOR DETECTING SYNCHRONOUS ERRORS OF HIGH-LIFT SURFACES ON AIRCRAFT. LIEBHERR AEROSPACE LINDENBERG, LIEBHERR AEROSPACE LINDENBERG, SHAPIRO COHEN, April 16, 2013: CA2520064

A device for detecting synchronous errors of high-lift surfaces, having an optical conductor laid over at least two adjacent high-lift surfaces, a light source and an optical receiver which are allocated to different ends of the optical conductor, as well as an evaluation unit for determining a sync ...


9
SCHIEVELBUSCH BERND: [fr] SYSTEME DENTRAINEMENT POUR VOLETS ET/OU BECS MOBILES DUN AVION ET AERONEF MUNI DUN TEL SYSTEME. LIEBHERR AEROSPACE, May 10, 2013: FR2982238-A1

[fr] La présente invention concerne un système d'entraînement pour volets, en particulier volets d'atterrissage et volets hypersustentateurs , et/ou pour becs mobiles d'un aéronef ou d'un avion. Le système comprend au moins une unité d'entraînement (20) qui est reliée à au moins un mécanisme de déri ...


10
Kleinhans Reinhold Dipl ing, Huth Stefan Dipl ing, Weiss Werner Dipl ing, Schievelbusch Bernd: High-lift system for aircraft. Liebherr Aerospace, hu qiang, May 9, 2012: CN201110299632

The present invention relates to a high-lift system of an aircraft having at least one drive unit, having at least one load station as well as having one or more transmissions for transmitting the drive energy of the drive unit to the at least one load station, wherein one or more of the transmissio ...