Translation of "Wing flaps" in German

The load stations 60 preferably serve the movement of the wing flaps or landing flap systems/slat flap systems.

Load stations of the wing flaps are designated by the reference numeral 60 .

Also fore flaps, slots in the wing and flaps are very effective.

He points to two wing flaps that he’s just separated from an Air-Canada jet.

Tell the pilot to keep the landing gear deployed and lower the wing flaps 15 degrees.

Tell the pilot to keep the landing gear deployed, and lower the wing flaps 15 degrees.

Furthermore, an aircraft wing comprising landing flaps is known from US 2007/0034748 A1.

As a consequence, the combination of wing and lift flaps gives rise to the outward cruising flight contour with the lift flaps retracted.

All these aircraft had enclosed crew cabins, fixed landing gear and advanced wing mechanization (flaps and slat).

In order to absorb the kinetic energy of the flue gases when the wing flaps are being closed and to move the large masses of the wing components, a drive shaft is provided for each wing component.

This air guide can be composed of swivelling wing flaps or also of Coander dishes which enable the filament sheet to be moved to and fro in the production direction.

With a view to a more rapid and more economical producability starting from the dental cap described above, and in particular to avoid excessive demands on the skill of the operating dental technician, it has elsewhere already been proposed to divide the outer region of the foil piece into at least two wing-shaped flaps, adjacent flaps being connected together at a distance from the centre of the foil piece corresponding to at least half the diameter of the cap upper side.

The latching devices 50, 51, on one hand, and 52, 53, on the other hand, respectively, for the flaps 4 and 5, should be arranged next to the indents 27, 27' and 27", for favorable accommodation, whereby the term next is seen in span direction of wing 1 or flaps 3.

In addition to these conventional uses of aircraft wing flaps, these flaps, and particularly trailing edge flaps, and in connection with the kinematics and mechanical structure controlling the movement and position as well as orientation of such flaps, German printed patent application 31 14 143 (see also U.S. patent application Ser. No. 366,250; filed: 04/02/1982) proposes to improve the aerodynamic effectiveness, particularly of transonic aircrafts during high speed/high altitude flights for purposes of changing and controlling the curvature of the camber line of a wing, in dependance upon current, updated parameters, such as altitude, weight, and speed, whereby also the effective area as well as the thickness of the wing can be modified in a controlled fashion under utilization of the existing flap systems and particularly during high speed/high altitude cruising, i.e. during those phases in which normally all flaps are well retracted.

The wing flaps and/or spoilers/airbrakes are extended during the landing approach and during low-speed flight in such a way that the above-mentioned installation space for the aircraft air-conditioning system is connected to the outside environment.

The particular advantage of the invention is to be seen in the utilization of but one linkage transmission per wing portion under utilization of elbow levers and tension rods for operating the wing flaps replacing conventional drive shafts because the conventional drive shafts do not permit synchronous movement oweing to the torsion forces.

Since the operation for landing flap 14 is coupled to the operation of the wing flap 4, a change of the position of the landing flap 14 will provide for synchronous deflection of the wing flaps 4 by either of the angles stated above covering in each instance a particular range.

In addition to these checks, Lufthansa Technik Philippines is also commissioned with modifications to doors, flaps, wing tips, fuel control systems and other structural alterations.

Such a control system can be part of a so-called avionics (flight control system) or can be connected thereto for implementing automatic pivoting in order to adjust, for example, control elements provided on the outer wing sections such as rudders (“ailerons”) or other adjustable, aerodynamically effective wing parts (e.g. flaps on the upper or lower wing side).

Wing leading-edge flaps are designed with or without a gap between the flap and the main wing, while trailing-edge flaps are usually designed as single-gap or multiple-gap trailing-edge flaps.