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We wish it to be understood, however, that our invention is not limited to this particular construction, since-any construction whereby the angular relations of the lateral margins of the aeroplanes may be varied in op site directions withirespeet to the "normal planes of said aeroplanes comeswithinthe sco of our invention. 4 and 5 are detail views, of one form of flexible joint for connecting the upright standards with the aeroplanes. It was subsequently granted as US Patent No. Orville would file additional patents of his own in 1921 and 1923. This greatly increases the efficiency of the rudder as compared with a plane surface of equal area. These standards are substantially rigid, being preferably constructed of wood and of equal length, equally spaced along the front and rear edges of the aeroplane, to which they are connected at their top and bottom ends by hinged joints or universal joints of any suitable description. 821393 issued to Orville Wright and Wilbur Wright of Dayton, Ohio, May 26, 1906, for "new and useful improvement in Flying Machines. 1 and 5 are detailviews, of one formof flexible j oin't'forconnectn" the upright standards with the aeroplanes.extendin from side to'sidc of the machine,thereby moving the lateral margins on, the' opposite sides of the machine into different angular relations-to the normal planes of' the same side of the machine moving to the same angle, and the nmrgins on one side of the ma- ,rhmo moving to an angle different from the angle to whichthemargins on the other side of the machine mo\'e,:snbstantiallv as (lescribed.19.indicates a second rope extending tra'ns-.versely of'themachine along the rear edge of the body portion .of the lower aeroplane, passing under suitable pulleys'or guides 20 at the rear corners g .and h of the lower aeroplane,6; In a flying-machine the combination, with two super osod'and'norlnally arallel aeroplanes, ear-1 having substantialy the; form of a normally fiat rectangle elongated transversely to tho line of flight, of upright standards gunner-ring the edges ot'said acroplanes to maintain their equidistancc, those standards at the lateral portions'ol said aoroplanes being connected therewith by flexible punts, and means for simultaneously impartmg to both lateral margins of both aeroplanes a moymuenl about axes which are perpen lic ular to. The movement of the rudder hereinbefore described prevents this action, since it exerts a retarding influence on that side of the machine which tends to move forward too rapidly and keeps the machine with its front properly presented to the direction of flight and with its body properly balanced around its central longitudinal axis. The front and rear spars 3 of each aeroplane are connected by a series of parallel ribs 5, which preferably extend somewhat beyond the rear spar, as shown. Patented May 22, 1906. (:1,'1- if may concern; Irope extending along the front edge of the lower aeroplane,atmosphere that $1 angle of incidence, alt ou'gh bem lifte or movedupward in the manner a ready described, at the same time meets with an increased resistance to its forward motion, and is therefore retarded in'its forward motion, while at the same time the other side of the machine, presentin a smaller angle of. 1 of the drawings. In either case owing to the varying conditions to be met there are numerous disturbing forces which tend to shift the machine from the position which it should occupy to obtain the desired results. As the corner e moves upward it carries the corner a upward with it, since the intermediate standard 8 is substantially rigid and maintains an equal distance between the corners a and e at all times. The objects of our invention are to provide means for maintaining or restoring the equilibrium or lateral balance of the apparatus, to provide means for guiding the machine both vertically and horizontally, and to provide a structure combining lightness, strength, convenience of construction, and certain other advantages which will hereinafter appear.11. a fixed distance between .the portions of the aeroplanes which theyconnect, and means for imparting such movement to the lateral m a] portions of the aeroplanes, substantial] as described;1 and WILBUR Wmen'r, citizens of-the United n of Montgomery, and State of .0mal plane at its rear end, said later'al margins being thus inclined upward and forward.