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This gives the machine a tendency to turn around its vertical axis, and this tendency if not properly met will not only change the direction of the front of the machine, but will ultimately permit one side thereof to drop into a position vertically below the other side with the aeroplanes in vertical position, thus causing the machine to fall. This causes the corner d to move downward and the corner e to move upward. incidence, -either y the application of mechanical power or by the uti ization of the force of gravity.and extending thencediagonally upward to the front corners a," and b of the upper aeroplane, where its ends are secured ln'anysum able manner, as indicated at 21.fipeciflcatiqn ofLettera Patent.tending from frontlto rear of the machine...The front rudder 31 is a horizontal. This construction of the aeroplanes gives a surface which has very great strength to withstand lateral and longitudinal strains, at the same time being capable of being bent or twisted in the manner hereinafter described. 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. 3, and thus preventing injury or breakage. 23, 1903.Be'it knownthat we; ORVILLE WRI HT;The'front and rear spars 3 of each .aero lan'e are connected ,by a. series of parallel ri s 5, which preferably eittend somewhat, beyond. 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. A hem is formed at the rear edge of the cloth to receive a wire 7, which is connected to the ends of the rear spar and supported by the rearwardly-extending ends of the longitudinal ribs 5, thus forming a rearwardly-extending flap or portion of the aeroplane. 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. 2. Page:Wright-Patent-US-821393.pdf/10. This results in a downward movement of the corner b and an upward movement of the corner c. Thus it results from a lateral movement of the cradle 18 to the right in Fig.
The struts 28 and 29 also serve to support the front or horizontal rudder, the construction of which we will now proceed to describe. 7. It is the chief object of our invention to provide means for remedying this difficulty, and we will now proceed to describe the construction by means of which these results are accomplished. A flying-machine comprising two superposed aeroplanes, normally flat but flexible, upright standards connecting the margins of said aeroplanes, said standards being connected to said aeroplanes by universal joints, diagonal stay-wires connecting the opposite ends of the adjacent standards, a rope extending along the front edge of the lower aeroplane, passing through guides at the front corners thereof, and having its ends secured to the rear corners of the upper aeroplane, and a rope extending along the rear edge of the lower aeroplane, passing through guides at the rear corners thereof, and having its ends secured to the front corners of the upper aeroplane, substantially as described.18. In a flying-machine, two aeroplanes, each normally flat and elongated transversely to the line of flight, and upright standards connecting the edges of said aeroplanes to maintain their equidistance, the connections between such standards and aeroplanes being by means of flexible joints, in combination with means for simultaneously imparting to each of said aeroplanes 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, 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.17.
This gives the machine a tendency to turn around its vertical axis, and this tendency if not properly met will not only change the direction of the front of the machine, but will ultimately permit one side thereof to drop into a position vertically below the other side with the aeroplanes in vertical position, thus causing the machine to fall. This causes the corner d to move downward and the corner e to move upward. incidence, -either y the application of mechanical power or by the uti ization of the force of gravity.and extending thencediagonally upward to the front corners a," and b of the upper aeroplane, where its ends are secured ln'anysum able manner, as indicated at 21.fipeciflcatiqn ofLettera Patent.tending from frontlto rear of the machine...The front rudder 31 is a horizontal. This construction of the aeroplanes gives a surface which has very great strength to withstand lateral and longitudinal strains, at the same time being capable of being bent or twisted in the manner hereinafter described. 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. 3, and thus preventing injury or breakage. 23, 1903.Be'it knownthat we; ORVILLE WRI HT;The'front and rear spars 3 of each .aero lan'e are connected ,by a. series of parallel ri s 5, which preferably eittend somewhat, beyond. 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. A hem is formed at the rear edge of the cloth to receive a wire 7, which is connected to the ends of the rear spar and supported by the rearwardly-extending ends of the longitudinal ribs 5, thus forming a rearwardly-extending flap or portion of the aeroplane. 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. 2. Page:Wright-Patent-US-821393.pdf/10. This results in a downward movement of the corner b and an upward movement of the corner c. Thus it results from a lateral movement of the cradle 18 to the right in Fig.
The struts 28 and 29 also serve to support the front or horizontal rudder, the construction of which we will now proceed to describe. 7. It is the chief object of our invention to provide means for remedying this difficulty, and we will now proceed to describe the construction by means of which these results are accomplished. A flying-machine comprising two superposed aeroplanes, normally flat but flexible, upright standards connecting the margins of said aeroplanes, said standards being connected to said aeroplanes by universal joints, diagonal stay-wires connecting the opposite ends of the adjacent standards, a rope extending along the front edge of the lower aeroplane, passing through guides at the front corners thereof, and having its ends secured to the rear corners of the upper aeroplane, and a rope extending along the rear edge of the lower aeroplane, passing through guides at the rear corners thereof, and having its ends secured to the front corners of the upper aeroplane, substantially as described.18. In a flying-machine, two aeroplanes, each normally flat and elongated transversely to the line of flight, and upright standards connecting the edges of said aeroplanes to maintain their equidistance, the connections between such standards and aeroplanes being by means of flexible joints, in combination with means for simultaneously imparting to each of said aeroplanes 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, 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.17.