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In a flying-machine, the combination, with two superposed and normally parallel aeroplanes, upright standards connecting the edges of said aeroplanes to maintain their equidistance, those standards at the lateral portions of said aeroplanes being connected therewith by flexible joints, and means for simultaneously moving both lateral portions of both aeroplanes into different angular relations to the normal planes of the bodies of the respective aeroplanes, the lateral portions on one side of the machine being moved to an angle different from that to which the lateral portions on the other side of the machine are moved, so as to present different angles of incidence at the two sides of the machine, of a vertical rudder, and means whereby said rudder is caused to present to the wind that side thereof nearest the side of the aeroplanes having the smaller angle of incidence and offering the least resistance to the atmosphere, substantially as described.ORVILLE WRIGHT AND WILBUR WRIGHT, OF DAYTON, OHIO.7. 3, their downward movement being limited in any suitable manner. Moreover, although we prefer to so construct the apparatus that the movements of the lateral margins on the opposite sides of the machine are equal in extent and opposite in direction, yet our invention is not limited to a construction producing this result, since it may be desirable under certain circumstances to move the lateral margins on one side of the machine in the manner just described without moving the lateral margins on the other side of the machine to an equal extent in the opposite direction. In a flying-machine, an aeroplane normally flat and elongated transversely to the line of flight, in combination with means for imparting to said aeroplane a helicoidal warp around an axis transverse to the line of flight and extending centrally along the body of the aeroplane in the direction of the elongation of the aeroplane, substantially as described.15. It will be observed in this connection that the construction is such that the rudder will always be so turned as to present its resisting-surface on that side of the machine on which the lateral margins of the aeroplanes present the least angle of resistance. The four corners of the upper aeroplane are indicated by the reference-letters a, b, c, and d, while the corresponding corners of the lower aeroplane 2 are indicated by the reference-letters e, f, g, and h. The marginal lines a b and e f indicate the front edges of the aeroplanes, the lateral margins of the upper aeroplane are indicated, respectively, by the lines a d and b c, the lateral margins of the lower aeroplane are indicated, respectively, by the lines e h and f g, while the rear margins of the upper and lower aeroplanes are indicated, respectively, by the lines c d and g h. Before proceeding to a description of the fundamental theory of operation of the structure we will first describe the preferred mode of constructing the aeroplanes and those portions of the structure which serve to connect the two aeroplanes. or above an below the normal. B Willi ur lfrg'yif.Having thus fully described our invention, what we claim as new, anddesir to secure by Letters Patent, is-We have used the term aeroplane inthis' s ecification and the appended claims indicate the supportin -surface or supportingsurfaces by means 9 which the machine is sustained in the air, and by this term wewish to be understood as including an suitable supporting-surface which norma y is substantially flat,"although of course when constructed of cloth or other flexible fabric, asat anegative angle and employ no horizontal tail at all. It was subsequently granted as US Patent No. FLYING MACHINE.means for operatingthe rope'15, and the machineis intended to be generally used with the-operator lying face downward on the so that the operators body rests on the era- -the movements of the operators body. Said supports are free to swing upward at their free rear ends, as indicated in dotted lines in Fig. his is the final form of Wilbur and Orville Wright's patent for "new and useful improvements in Flying-Machines." Each aeroplane is of considerablygreater width from side'to side than from, frontto rear. We wishit to be understood, -however, that we do not limit ourselves to $5- the particular description of rudder setforth,The objects of our invention are to provide means for maintaining or restoring the equi-- tain novel features, which we will-now proceed to describe and will then particularly point out in the claims. Turning now to the purpose of this revision for moving the lateral margins of .t e ae planes in the manner doscribed, it should be promised that owing to various conditions of wind-pressure and other causes the body of the machine is apt to become unbalanced laterally, one side tending to sink and the otherside tending to rise, the machine turningaround its central longitudinal axis.