AIRCRAFT WITH ENGINE PODS TILTABLE ABOUT A TRANSVERSE AXIS
摘要
The invention concerns an aircraft with engine pods located outboard on the wings and tiltable about a transverse axis. A fixed wing centerpiece is provided which terminates at the outside in each spanwise direction in a separation location. A through tubular spar is rotatably supported in the wing centerpiece. This tubular spar serves as a support for the outer wings which continue beyond the separation locations and which, together with the engine pods located there, form a unit which can be jointly swivelled or tilted.
申请公布号
US5096140(A)
申请公布日期
1992.03.17
申请号
US19900578037
申请日期
1990.09.05
申请人
DORNIER, JR., DECEASED, CLAUDIUS;DORNIER-TIEFENTHALER, LEGAL REPRESENTATIVE, BY MARTINE;WINDISCHBAUER, FLORIAN
发明人
DORNIER, JR., DECEASED, CLAUDIUS;DORNIER-TIEFENTHALER, LEGAL REPRESENTATIVE, BY MARTINE;WINDISCHBAUER, FLORIAN