US1054374A - Flying apparatus. - Google Patents
Flying apparatus. Download PDFInfo
- Publication number
- US1054374A US1054374A US67151312A US1912671513A US1054374A US 1054374 A US1054374 A US 1054374A US 67151312 A US67151312 A US 67151312A US 1912671513 A US1912671513 A US 1912671513A US 1054374 A US1054374 A US 1054374A
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- stretchers
- frame
- skeleton
- flying
- supporting
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/56—Folding or collapsing to reduce overall dimensions of aircraft
Definitions
- GUSTAV VOIGT OF STETTIN, GERMANY.
- My invention relates to an improved flying-apparatus, which may be employed either in the same manner as a kite, being lifted and kept floating by the resistance of the supporting current of air, and thus may serve for sporting purposes or for meteorological or aerological observations, or which may be constructed to a size which enables the apparatus to carry one or more persons, or a load, or a motor and means for propelling the apparatus.
- the principal object to be obtained by this invention is to provide a construction of parts by which the flying apparatus is maintained, while being used, in a state of equilibrium, thereby preventing the apparatus from tilting over or swerving from its true direction, the forward movement of the apparatus being steadily maintained in a straight line without deviations in the horizontal or in the vertical plane.
- the bulk of the apparatus may further be so constructed as to be collapsed at will and opened again to display its supporting surfaces, much in the same manner as an umbrella, thus 0btaining a considerable economy of space when the apparatus is out of use.
- Figure 1 represents a side elevation of the flying apparatus constructed according to this invention
- Fig. 2 is a front-elevation of the same.
- Fig. 3 is a top-plan of the same;
- Fig. 4 is a cross-section drawn on line 5-0 of the same;
- Fig. 5 is cross-section drawn on line n0 of the same;
- Fig. 6 is a perspective view of the apparatus drawn to a reduced scale.
- Fig. 7 is a cross-section of the apparatus, drawn along the line indicated by the rod RR in Fig. 6.
- Fig. 8 shows the skeleton frame of the apparatus, the supporting surfaces carried by the said skeleton frame being in place and displayed.
- Fig. 9 is a plan similar to Fig. 8, showing a modification of the skeleton frame.
- Fig. 10 is a cross-section of the apparatus ac- Specification of Letters Patent.
- FIG. 11 shows the skeleton frame according to Fig. 9 in a nearly collapsed state.
- Figs. 12 and 13 are plan views, drawn to a reduced scale and showing two other modifications of the flying apparatus, which, in these modifications, consists of two skeleton frames and supporting surfaces so combined to each other, to support a motor or other load.
- Fig. 14 shows the skeleton frame according to Fig. 8 in a nearly collapsed state, and Fig. 15 is a perspective underside View of the apparatus drawn to a reduced scale.
- the bulk or body of the flying apparatus comprises an upper or main supporting surface a, Z), c, as shown in Fig. 3, a lower surface a, f, g, as shown in Fig. 2, downwardly inclined from the point a of the apparatus toward the rear, and two side surfaces (Z, c, laterally closing the triangular or funnel-shaped space between the two diverging surfaces at, b, c, and a, f, g, the said triangular space being open at the rear.
- the said lower surface a, f, g, and sides d, e, are inferior in length to the said upper surface a, b, 0, the length of said two surfaces a, b, 0, and a, f, g, being so proportioned, that the lower surface measures about one half of the said upper surface, but the said proportion may vary within certain limits;
- Figs. 1 and 15 clearly show the relation between the upper and lower surfaces of the apparatus.
- the current of air flowing to the rear as the apparatus in its forward movement cuts through the air is directed below the rear part of the upper surface a, b, a, which extends beyond the lower surface a, f, g, and sides (Z, 6.
- the air-filled space at the front of the apparatus inclosed between the said upper surface, the lower surface and the two side-surfaces, so cooperates with the rearward extension of the said upper surface, that it will keep the apparatus at a permanent state of equilibrium, thereby preventing it from tilting in the forward as well as in the rearward or in either lateral direction.
- the downward currents of air which may bear against the upper surface of the apparatus, and the upward current, which may come to strike against the lower supporting surface are so distributed by the combination of the larger upper surface and the shorter lower surface, that all lines of resistance will meet in one point and no tendency of turning or tilting will be cccasioned.
- the apparatus will automatically take and retain its true position in the air against any varying currents of air.
- the tapering construction of the frame or skeleton to which the covering surfaces of the apparatus are secured offers the particular advantage, that the said frame or skeleton may be folded up or collapsed, much in the manner of an umbrella, thereby affording great facility and economy of space in housing and transporting theapparatus.
- the stretchers or rods of the skeleton frame, to which the supporting surfaces of the apparatus are secured, may be opened and closed by a runner to which said stretchers are hinged as usual.
- a triangular frame of rods, RR Ri and R --z' is raised upon the main or upper supporting surface a, Z), c, of the apparatus, the rod RR extending horizontally across the triangular forward portion of the said surface a. Z), 0, and the rods Ri and R z' extending to the rear in a horizontal plane.
- the covering surface of the apparatus is secured to the crossbar R-IP, and to vertical rods 1', and a, connected to said cross-bar RR the said vertical rods extending downward through the upper and lower surfaces of the apparatus and also upward beyond the horizontal rod RR
- the length of said rod R-R extends at both ends beyond the edges of the upper surface a, Z), c, which is connected to said rod.
- Two pairs of stretchers i-7c, and 2 -13, are adapted to slide upon the main or cen t-ral rod a-2 of the skeleton-frame.
- the runner to which the stretcher i in is hinged as at 2" is liable to be shifted in the forward direction, and the runner to which the stretcher i -7c is hinged as at 71 is adapted to be run downward, as shown in Fig. l t.
- the supporting surfaces of the flying apparatus are secured to the said stretchers as at 70, and A cord Z, guided by loops or eyes atthe front point a of the apparatus, and through loops or eyes at or near the ends of the rod RR serves to connect each pair of stretchers z'7c, and i 7u' as indicated by dash-and-dotted lines in Figs. 8 and 1 1.
- the frame On pulling the free inner ends of the cords downward from the position of Fig. 14 toward the hinges z, the frame will be opened to take the position of Fig. 8, and on re leasing the said inner ends of the cords Z, the stretchers z'7c, and 6 -40 may again he collapsed as indicated by Fig. 14.
- the two runners On opening the skeleton frame, the two runners will approach each other, as in Fig. 8, and on closing the frame, the said runners will move in opposite directions, as shown in Fig. 14.
- the edges of the covering fabrics, being secured to the stretchers, will be unfolded, as in Fig. 8, or folded against the main or central rod a2, as in Fig. 14L.
- the two sets of stretchers z'l:, and 5 -70 take a position opposite to each other so as to make the free ends of said stretchers cross each other
- the arrangement shown in Figs. 9 and 11 is different in that the said two sets of stretchers take a position parallel to each other and maintain their parallelism while being folded or unfolded.
- the two runners to which the two sets of stretchers are hinged are rigidly connected to each other by rods or by a tubular runner, to which both sets of stretchers are hinged. As shown on the left hand side of Figs.
- the stretchers i-lu and z' 7c may extend beyond the covering surface a, Z), 0 connected to said stretchers as at 1;, and 19.
- a cord indicated in Fig. 9 by a dash-anddot-line, is connected at or near the outer end of the stretchers z'k, said cord leading over a guide-roller or lug at the forward end a. of the apparatus, thence down along the central rod a-z to the hinged end 2'
- the runner may be locked to the central rod by a spring-clasp of the kind usually employed with umbrellas.
- the stretchers On releasing said locking clasp or catch and on sliding the two runners rigidly connected to each other toward the front end, the stretchers will be folded down as shown in Fig. 11.
- the portion lcv of the stretchers extending beyond the covering fabrics may serve for connecting to it additional or enlarging surfaces of covering fabrics by which the total area of the supporting surface is increased.
- the means for collapsing the skeleton frame of the apparatus as before described with reference to Figs. 8 to 11 of the drawings are particularly applicable with flying apparatus of the lighter kind not adapted to be motor-driven.
- a construction may be adopted as indicated by Figs. 12 and 13.
- the skeleton or collapsible frame in this case, is composed of two skeleton frames similar to either one or the other of the collapsible frames before described, the said two frames being juxtaposed and connected to each other by an intermediate frame adapted to carry the motor or load.
- Each of the two lateral collapsible frames has a main or central rod with runners and stretchers as described and adapted to be folded and unfolded independently, or means might be provided to simultaneously fold and unfold the two lateral frames.
- a flying apparatus the combination, with an upper supporting surface, of a lower supporting surface inferior in length to the said upper surface, the said lower surface having a downwardly inclined position toward the rear with relation to the upper supporting surface, side surfaces connecting the edges of the said lower surface to the said upper supporting surface, a rearward extension formed to the upper supporting surface and extending in the plane of the same, and a skeleton frame to which the said surfaces are connected, substantially as and for the purpose set forth.
- a flying apparatus the combination, with an upper supporting surface, of a lower supporting surface inferior in length to the said upper surface and having a downwardly and rearwardly inclined position with relation to the said upper surface, side surfaces connected to the said upper and lower surfaces closing the space between the said upper and lower surfaces except at the rear, a rearward extension formed to the said upper supporting surface, a skeleton frame to which said supporting surfaces are connected, and means for collapsing said frame and surfaces secured thereto, substantially as and for the purpose set forth.
- a flying apparatus the combination, with an upper supporting surface, of a lower supporting surface inferior in length to the said upper surface and having a downwardly and rearwardly inclined position with relation to the said upper surface to which said lower surface is secured in front at an acute angle, collapsible sides connecting the said upper to the said lower surfaces and forming a space between the same open only at the rear, an extension to the rear of the said upper supporting surface, a skeleton frame to which said supporting surfaces are connected, a central rod forming part of the said skeleton frame, runners slidably carried by said central rod and stretchers carried by said runners for collapsing the skeleton frame and the covering surfaces of the same, substantially as and for the purpose set forth.
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- Tents Or Canopies (AREA)
Description
G. VOIGT.
- FLYING APPARATUS.
APPLICATION FILED JAN. 16, 1912.
1,054,374, Patented Feb. 25, 1913.
Snuentor:
hiz
Witnesses:
UNITED STATES PATENT OFFICE.
GUSTAV VOIGT, OF STETTIN, GERMANY.
FLYING APPARATUS.
Application filed January 16, 1912.
To all whom it may concern:
Be it known that I, GUSTAV VOIGT, a subject of the King of Prussia, residing at No. 13 Barnimstrasse, Stettin, Germany, have invented new and useful Improvements in Flying Apparatus, of which the following is a specification.
My invention relates to an improved flying-apparatus, which may be employed either in the same manner as a kite, being lifted and kept floating by the resistance of the supporting current of air, and thus may serve for sporting purposes or for meteorological or aerological observations, or which may be constructed to a size which enables the apparatus to carry one or more persons, or a load, or a motor and means for propelling the apparatus.
The principal object to be obtained by this invention is to provide a construction of parts by which the flying apparatus is maintained, while being used, in a state of equilibrium, thereby preventing the apparatus from tilting over or swerving from its true direction, the forward movement of the apparatus being steadily maintained in a straight line without deviations in the horizontal or in the vertical plane.
The bulk of the apparatus, according to this invention, may further be so constructed as to be collapsed at will and opened again to display its supporting surfaces, much in the same manner as an umbrella, thus 0btaining a considerable economy of space when the apparatus is out of use.
To make my invention perfectly understood, I have illustrated the same in the accompanying drawings, in which:
Figure 1 represents a side elevation of the flying apparatus constructed according to this invention; Fig. 2 is a front-elevation of the same. Fig. 3 is a top-plan of the same; Fig. 4 is a cross-section drawn on line 5-0 of the same; Fig. 5 is cross-section drawn on line n0 of the same; Fig. 6 is a perspective view of the apparatus drawn to a reduced scale. Fig. 7 is a cross-section of the apparatus, drawn along the line indicated by the rod RR in Fig. 6. Fig. 8 shows the skeleton frame of the apparatus, the supporting surfaces carried by the said skeleton frame being in place and displayed. Fig. 9 is a plan similar to Fig. 8, showing a modification of the skeleton frame. Fig. 10 is a cross-section of the apparatus ac- Specification of Letters Patent.
Patented Feb. 25, 1913.
Serial No. 671,513.
cording to Fig. 9, with radially extending stretchers of the collapsible skeleton frame. Fig. 11 shows the skeleton frame according to Fig. 9 in a nearly collapsed state. Figs. 12 and 13 are plan views, drawn to a reduced scale and showing two other modifications of the flying apparatus, which, in these modifications, consists of two skeleton frames and supporting surfaces so combined to each other, to support a motor or other load. Fig. 14: shows the skeleton frame according to Fig. 8 in a nearly collapsed state, and Fig. 15 is a perspective underside View of the apparatus drawn to a reduced scale.
Referring to Figs. 1 to 8, the bulk or body of the flying apparatus comprises an upper or main supporting surface a, Z), c, as shown in Fig. 3, a lower surface a, f, g, as shown in Fig. 2, downwardly inclined from the point a of the apparatus toward the rear, and two side surfaces (Z, c, laterally closing the triangular or funnel-shaped space between the two diverging surfaces at, b, c, and a, f, g, the said triangular space being open at the rear. The said lower surface a, f, g, and sides d, e, are inferior in length to the said upper surface a, b, 0, the length of said two surfaces a, b, 0, and a, f, g, being so proportioned, that the lower surface measures about one half of the said upper surface, but the said proportion may vary within certain limits; Figs. 1 and 15 clearly show the relation between the upper and lower surfaces of the apparatus.
Owing to the peculiar arrangement of the supporting surfaces with relation to each other, the current of air flowing to the rear as the apparatus in its forward movement cuts through the air, is directed below the rear part of the upper surface a, b, a, which extends beyond the lower surface a, f, g, and sides (Z, 6. The air-filled space at the front of the apparatus, inclosed between the said upper surface, the lower surface and the two side-surfaces, so cooperates with the rearward extension of the said upper surface, that it will keep the apparatus at a permanent state of equilibrium, thereby preventing it from tilting in the forward as well as in the rearward or in either lateral direction. The downward currents of air which may bear against the upper surface of the apparatus, and the upward current, which may come to strike against the lower supporting surface are so distributed by the combination of the larger upper surface and the shorter lower surface, that all lines of resistance will meet in one point and no tendency of turning or tilting will be cccasioned. The apparatus will automatically take and retain its true position in the air against any varying currents of air.
The tapering construction of the frame or skeleton to which the covering surfaces of the apparatus are secured, offers the particular advantage, that the said frame or skeleton may be folded up or collapsed, much in the manner of an umbrella, thereby affording great facility and economy of space in housing and transporting theapparatus.
The stretchers or rods of the skeleton frame, to which the supporting surfaces of the apparatus are secured, may be opened and closed by a runner to which said stretchers are hinged as usual.
In constructing a collapsible frame of the kind, I prefer to employ a skeleton of the kind shown in Figs. 8 and 14, or of the modified kind illustrated by Figs. 9, 10 and 11.
As shown in Fig. 6, a triangular frame of rods, RR Ri and R --z' is raised upon the main or upper supporting surface a, Z), c, of the apparatus, the rod RR extending horizontally across the triangular forward portion of the said surface a. Z), 0, and the rods Ri and R z' extending to the rear in a horizontal plane. The covering surface of the apparatus is secured to the crossbar R-IP, and to vertical rods 1', and a, connected to said cross-bar RR the said vertical rods extending downward through the upper and lower surfaces of the apparatus and also upward beyond the horizontal rod RR The length of said rod R-R extends at both ends beyond the edges of the upper surface a, Z), c, which is connected to said rod.
Two pairs of stretchers i-7c, and 2 -13, are adapted to slide upon the main or cen t-ral rod a-2 of the skeleton-frame. The runner to which the stretcher i in is hinged as at 2", is liable to be shifted in the forward direction, and the runner to which the stretcher i -7c is hinged as at 71 is adapted to be run downward, as shown in Fig. l t. The supporting surfaces of the flying apparatus are secured to the said stretchers as at 70, and A cord Z, guided by loops or eyes atthe front point a of the apparatus, and through loops or eyes at or near the ends of the rod RR serves to connect each pair of stretchers z'7c, and i 7u' as indicated by dash-and-dotted lines in Figs. 8 and 1 1. On pulling the free inner ends of the cords downward from the position of Fig. 14 toward the hinges z, the frame will be opened to take the position of Fig. 8, and on re leasing the said inner ends of the cords Z, the stretchers z'7c, and 6 -40 may again he collapsed as indicated by Fig. 14. On opening the skeleton frame, the two runners will approach each other, as in Fig. 8, and on closing the frame, the said runners will move in opposite directions, as shown in Fig. 14. The edges of the covering fabrics, being secured to the stretchers, will be unfolded, as in Fig. 8, or folded against the main or central rod a2, as in Fig. 14L.
lVhile in the arrangement described with reference to Figs. 8 and 14 the two sets of stretchers z'l:, and 5 -70 take a position opposite to each other so as to make the free ends of said stretchers cross each other, the arrangement shown in Figs. 9 and 11 is different in that the said two sets of stretchers take a position parallel to each other and maintain their parallelism while being folded or unfolded. The two runners to which the two sets of stretchers are hinged are rigidly connected to each other by rods or by a tubular runner, to which both sets of stretchers are hinged. As shown on the left hand side of Figs. 9 and 11, the stretchers i-lu and z' 7c may extend beyond the covering surface a, Z), 0 connected to said stretchers as at 1;, and 19. A cord, indicated in Fig. 9 by a dash-anddot-line, is connected at or near the outer end of the stretchers z'k, said cord leading over a guide-roller or lug at the forward end a. of the apparatus, thence down along the central rod a-z to the hinged end 2' The runner may be locked to the central rod by a spring-clasp of the kind usually employed with umbrellas. On releasing said locking clasp or catch and on sliding the two runners rigidly connected to each other toward the front end, the stretchers will be folded down as shown in Fig. 11. The portion lcv of the stretchers extending beyond the covering fabrics may serve for connecting to it additional or enlarging surfaces of covering fabrics by which the total area of the supporting surface is increased.
The means for collapsing the skeleton frame of the apparatus as before described with reference to Figs. 8 to 11 of the drawings are particularly applicable with flying apparatus of the lighter kind not adapted to be motor-driven.
If a collapsible frame is desired to be employed with a motor-driven flying apparatus, a construction may be adopted as indicated by Figs. 12 and 13. The skeleton or collapsible frame, in this case, is composed of two skeleton frames similar to either one or the other of the collapsible frames before described, the said two frames being juxtaposed and connected to each other by an intermediate frame adapted to carry the motor or load. Each of the two lateral collapsible frames has a main or central rod with runners and stretchers as described and adapted to be folded and unfolded independently, or means might be provided to simultaneously fold and unfold the two lateral frames.
I claim as my invention:
1. In a flying apparatus, the combination, with an upper supporting surface, of a lower supporting surface inferior in length to the said upper surface, the said lower surface having a downwardly inclined position toward the rear with relation to the upper supporting surface, side surfaces connecting the edges of the said lower surface to the said upper supporting surface, a rearward extension formed to the upper supporting surface and extending in the plane of the same, and a skeleton frame to which the said surfaces are connected, substantially as and for the purpose set forth.
,2. In a flying apparatus, the combination, with an upper supporting surface, of a lower supporting surface inferior in length to the said upper surface and having a downwardly and rearwardly inclined position with relation to the said upper surface, side surfaces connected to the said upper and lower surfaces closing the space between the said upper and lower surfaces except at the rear, a rearward extension formed to the said upper supporting surface, a skeleton frame to which said supporting surfaces are connected, and means for collapsing said frame and surfaces secured thereto, substantially as and for the purpose set forth.
3. In a flying apparatus, the combination, with an upper supporting surface, of a lower supporting surface inferior in length to the said upper surface and having a downwardly and rearwardly inclined position with relation to the said upper surface to which said lower surface is secured in front at an acute angle, collapsible sides connecting the said upper to the said lower surfaces and forming a space between the same open only at the rear, an extension to the rear of the said upper supporting surface, a skeleton frame to which said supporting surfaces are connected, a central rod forming part of the said skeleton frame, runners slidably carried by said central rod and stretchers carried by said runners for collapsing the skeleton frame and the covering surfaces of the same, substantially as and for the purpose set forth.
In testimony whereof I have signed my name to this Specification in the presence of two subscribing witnesses.
GUSTAV VOIGT.
\Vitnesses:
K. GRZELAOHOWSKI, FRITZ LEAVY.
Copies of this patent may be obtained for five cents each, by addressing the Commissioner of Patents,
' Washington, D. G.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US67151312A US1054374A (en) | 1912-01-16 | 1912-01-16 | Flying apparatus. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US67151312A US1054374A (en) | 1912-01-16 | 1912-01-16 | Flying apparatus. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1054374A true US1054374A (en) | 1913-02-25 |
Family
ID=3122634
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US67151312A Expired - Lifetime US1054374A (en) | 1912-01-16 | 1912-01-16 | Flying apparatus. |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1054374A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3135482A (en) * | 1962-12-26 | 1964-06-02 | Ryan Aeronautical Co | Flexible wing stol assist system for aircraft |
| US3534931A (en) * | 1968-03-28 | 1970-10-20 | Rogallo Francis J | Variable area flexible wings |
| US4292757A (en) * | 1977-07-08 | 1981-10-06 | Cahen Jr George L | Collapsible wing aircraft |
| EP0075616A1 (en) * | 1981-09-28 | 1983-04-06 | Huber, Peter | Collapsible wing aircraft |
| US20120018583A1 (en) * | 2010-07-26 | 2012-01-26 | Eolo Sport Industrias, S.A. | Folding kite with a central assembly shaft |
| US20130020442A1 (en) * | 2011-07-20 | 2013-01-24 | Eolo Sport Industrias, S.A. | Static kite of seamless articulated assembly |
-
1912
- 1912-01-16 US US67151312A patent/US1054374A/en not_active Expired - Lifetime
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3135482A (en) * | 1962-12-26 | 1964-06-02 | Ryan Aeronautical Co | Flexible wing stol assist system for aircraft |
| US3534931A (en) * | 1968-03-28 | 1970-10-20 | Rogallo Francis J | Variable area flexible wings |
| US4292757A (en) * | 1977-07-08 | 1981-10-06 | Cahen Jr George L | Collapsible wing aircraft |
| EP0075616A1 (en) * | 1981-09-28 | 1983-04-06 | Huber, Peter | Collapsible wing aircraft |
| US20120018583A1 (en) * | 2010-07-26 | 2012-01-26 | Eolo Sport Industrias, S.A. | Folding kite with a central assembly shaft |
| US20130020442A1 (en) * | 2011-07-20 | 2013-01-24 | Eolo Sport Industrias, S.A. | Static kite of seamless articulated assembly |
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