EP 1984289 A1 20081029 - LIFTING SYSTEM
Title (en)
LIFTING SYSTEM
Title (de)
HEBESYSTEM
Title (fr)
SYSTÈME DE LEVAGE
Publication
Application
Priority
- EP 2006012371 W 20061221
- DE 102006007504 A 20060216
Abstract (en)
[origin: WO2007093212A1] A lifting system (1) is used for lifting loads, for example for lifting and recovering an aircraft (2) following an accident, and has a lift (6) which can be positioned underneath a load, in particular underneath a mainplane (5) of an aircraft. The lift (6) has at least three lifting cylinders (8) or similar lifting elements and a docking head (9) for coupling to a load holding point. A measurement system is provided in order to detect the position of the docking head (9) and to measure the load vector that occurs at the docking head (9). A control device is connected to the measurement system, for mutually independent, load-controlled or movement-controlled confirmation of the individual lifting cylinder drives.
IPC 8 full level
B64F 5/00 (2006.01); B66F 3/46 (2006.01); B66F 7/20 (2006.01)
CPC (source: EP US)
B64F 5/50 (2016.12 - EP US); B66F 3/46 (2013.01 - EP US); B66F 7/20 (2013.01 - EP US)
Citation (search report)
See references of WO 2007093212A1
Designated contracting state (EPC)
AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR
DOCDB simple family (publication)
WO 2007093212 A1 20070823; AU 2006338052 A1 20070823; BR PI0621337 A2 20111206; CA 2624836 A1 20070823; CN 101309851 A 20081119; DE 102006007504 A1 20070830; EP 1984289 A1 20081029; JP 2009526722 A 20090723; RU 2008113808 A 20091210; US 2009234504 A1 20090917
DOCDB simple family (application)
EP 2006012371 W 20061221; AU 2006338052 A 20061221; BR PI0621337 A 20061221; CA 2624836 A 20061221; CN 200680042688 A 20061221; DE 102006007504 A 20060216; EP 06829806 A 20061221; JP 2008554606 A 20061221; RU 2008113808 A 20061221; US 16172306 A 20061221