US1043079A - Flying-machine. - Google Patents
Flying-machine. Download PDFInfo
- Publication number
- US1043079A US1043079A US62373811A US1911623738A US1043079A US 1043079 A US1043079 A US 1043079A US 62373811 A US62373811 A US 62373811A US 1911623738 A US1911623738 A US 1911623738A US 1043079 A US1043079 A US 1043079A
- Authority
- US
- United States
- Prior art keywords
- flying
- machine
- web
- covering
- ribs
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 240000008564 Boehmeria nivea Species 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 239000004744 fabric Substances 0.000 description 2
- 239000004753 textile Substances 0.000 description 2
- 241000206672 Gelidium Species 0.000 description 1
- 230000004308 accommodation Effects 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 238000004079 fireproofing Methods 0.000 description 1
- 108010059642 isinglass Proteins 0.000 description 1
- 229910052627 muscovite Inorganic materials 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
Definitions
- the machine is made of elongated form with a pointed bow and is propelled in the line of its major axis, while a longitudinal fin and web extending along the top and bottom of the plane respectively serve to counterbalance lateral air pressure.
- the invention also comprises various other features of novelty hereinaftermore' fully pointed out;
- Figure 1 is a plan partly broken away and partly in section of a flying. machine embodying our invention
- Fig. 2 a sectional side elevation thereof
- Fig. 3 an enlarged vertical cross section on line 3-3, Fig. 1
- Fig. 4 a cross section through the covering
- Fig. 5 a cross section through a connection between frame and covering.
- the frame of the flying machine comprises essentially an upper longitudinal rod 10 from each side of which extend laterally a plurality of arched ribs 11. These ribs constitute the supports for the carrying planes 12 which thus form a pair of wings having the configuration more fully shown in Fig. 1. That is to say the covering has parallel sides 13, slightly converging rear edges 14, a square back 15, a curved prow 16 and a sharp bow 17. By this peculiar form the flying machine cuts readily through the air while at the same time objectionable back suction is prevented.
- the covering 12 is composed of a textile fabric woven with threads spun from the ramie'fiber and possessing marked advantages over the canvas or similar coverings hitherto generally used. Itdoes not absorb water, but readily sheds the-same, does not shrink and being very smooth passes freely through theair similar to a birds wing. It is preferred to reinforce the covering by interwoven. strengthening threads.or wires 18 interposed between groups of warp threads and also between groups of weft tor driving motor 24:, etc.
- each rib is secured to ribs 11 by a plurality of bottom strips 19 also made of ramie and secured to the main body of the covering at the right and left of each rib in such a way that each strip slopes uniformly from the center of the rib toward both edges, as more fully shown in Fig. 5. In this way each rib is pocketed while the sloping sides of the strips decrease the resistance against air pressure during flying, and at the same time prevent objectionable back suction.
- a web A which is also made of ramie and is of the peculiar form shown in Figs. 1 and 2.
- This web is composed of a pointed front section 20, a pair of bulged central sections 21, and a tapering rear section 22.
- the bulged central sections 21 are so spaced as to form a cage 23 for the accommodation of the avia-
- the converging front portions of central sections 21 are provided with windows 25 made of isinglass.
- the front and rear propellers 26, 27 are mounted on a shaft 28 and are operated from motor 24 by a suitable chain drive 29.
- the rear propeller 27 is accommodated within a corresponding opening of covering 12 and web A.
- Back of propeller 27 there is hinged at 30 to the frame of square back 15 a horizontal rudder 31, while a vertical rudder 32 1s hinged at 33 at the rear of .web A.
- nal fin. 34 having a pointed front end. This fin serves to counteract the pressure of side winds against web A, so that tilting of the air-ship is prevented.
- runners or wheels 35 As usual.
- the air ship constructed as described is ofsimple construction, offers a minimum resistance to the air and is not liable to tilt or get out of order. Furthermore the peculiar construction of the carrying plane materially increases the serviceability of the flying machine, as it is not liable to sag, rip, shrink or become wa ter soaked.
- a flying machine comprising a frame, an oblong carrying plane supported thereby and having an arched pointed bow and a contracted squared stern, and a web depending from said plane, said web' being composed of a single front section, a pair of spaced central sections forming an interveningcabin, and a single rear section.
- a flying machine comprising a frame, an oblong carrying plane supported thereby and having an arched pointed bow and a contracted apertured stern, a fin extending longitudinally over said plane, a web depending from the plane and formed of a pointed single front section, a pair of spaced central sections, and an apertured rear section, and a propeller accommodated within the apertures of the carrying plane and web.
- a flying machine provided with a frame having a plurality of transverse ribs, a textile carrying plane extending over the same, and a plurality of transverse strips extendingbeneath the ribs from end to end and secured to the plane at a substantial distance from the ribs to form sides that slope uniformly from the center of the ribs to the outer edges of the strips, whereby the air is evenly deflected from the ribs during action.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Treatment Of Fiber Materials (AREA)
Description
g: 2 MM v E. F. VON DREDBN & H. R. HOFMANN.
FLYING MACHINE.
LPILIOATION' nun APR. 27, 1911.
1,043,079. Patented Not-5,1912.
w/msssss: mvmrdns UNITED STATES PATENT OFFICE.
ERNEST F. von DREDEN Ann HERBERT re. rrornmrm, or new YORK, N. Y.
' FLYING-MACHINE.
Specification of Letters Patent.
Patented Nov. 5, 1912.
Application filed April 27, 1911. Serial No. 623,738.
of the monoplane type which is adapted to readily cut through the air and is effectively protected against tilting. For this purpose the machine is made of elongated form with a pointed bow and is propelled in the line of its major axis, while a longitudinal fin and web extending along the top and bottom of the plane respectively serve to counterbalance lateral air pressure.
The invention also comprises various other features of novelty hereinaftermore' fully pointed out;
In the accompanying drawing: Figure 1 is a plan partly broken away and partly in section of a flying. machine embodying our invention; Fig. 2a sectional side elevation thereof; Fig. 3 an enlarged vertical cross section on line 3-3, Fig. 1; Fig. 4 a cross section through the covering, and Fig. 5 a cross section through a connection between frame and covering.
The frame of the flying machine comprises essentially an upper longitudinal rod 10 from each side of which extend laterally a plurality of arched ribs 11. These ribs constitute the supports for the carrying planes 12 which thus form a pair of wings having the configuration more fully shown in Fig. 1. That is to say the covering has parallel sides 13, slightly converging rear edges 14, a square back 15, a curved prow 16 and a sharp bow 17. By this peculiar form the flying machine cuts readily through the air while at the same time objectionable back suction is prevented.
The covering 12 is composed of a textile fabric woven with threads spun from the ramie'fiber and possessing marked advantages over the canvas or similar coverings hitherto generally used. Itdoes not absorb water, but readily sheds the-same, does not shrink and being very smooth passes freely through theair similar to a birds wing. It is preferred to reinforce the covering by interwoven. strengthening threads.or wires 18 interposed between groups of warp threads and also between groups of weft tor driving motor 24:, etc.
threads. .So also the fabric may be impregnated by a suitable fire proofing solution if desired. The covering 12 is secured to ribs 11 by a plurality of bottom strips 19 also made of ramie and secured to the main body of the covering at the right and left of each rib in such a way that each strip slopes uniformly from the center of the rib toward both edges, as more fully shown in Fig. 5. In this way each rib is pocketed while the sloping sides of the strips decrease the resistance against air pressure during flying, and at the same time prevent objectionable back suction.
From rod 10 depends a web A which is also made of ramie and is of the peculiar form shown in Figs. 1 and 2. This web is composed of a pointed front section 20, a pair of bulged central sections 21, and a tapering rear section 22. The bulged central sections 21 are so spaced as to form a cage 23 for the accommodation of the avia- The converging front portions of central sections 21 are provided with windows 25 made of isinglass. The front and rear propellers 26, 27 are mounted on a shaft 28 and are operated from motor 24 by a suitable chain drive 29. The rear propeller 27 is accommodated within a corresponding opening of covering 12 and web A. Back of propeller 27 there is hinged at 30 to the frame of square back 15 a horizontal rudder 31, while a vertical rudder 32 1s hinged at 33 at the rear of .web A.
For steadying. purposes, there extends centrally over the covering 12, a longitudi= nal fin. 34 having a pointed front end. This fin serves to counteract the pressure of side winds against web A, so that tilting of the air-ship is prevented.
For starting and launching the flying machine, it is provided with runners or wheels 35 as usual.
It will beseenthat the air ship constructed as described is ofsimple construction, offers a minimum resistance to the air and is not liable to tilt or get out of order. Furthermore the peculiar construction of the carrying plane materially increases the serviceability of the flying machine, as it is not liable to sag, rip, shrink or become wa ter soaked.
We claim:
1. A flying machine comprising a frame, an oblong carrying plane supported thereby and having an arched pointed bow and a contracted squared stern, and a web depending from said plane, said web' being composed of a single front section, a pair of spaced central sections forming an interveningcabin, and a single rear section.
2. A flying machine comprising a frame, an oblong carrying plane supported thereby and having an arched pointed bow and a contracted apertured stern, a fin extending longitudinally over said plane, a web depending from the plane and formed of a pointed single front section, a pair of spaced central sections, and an apertured rear section, and a propeller accommodated within the apertures of the carrying plane and web.
means 3. A flying machine provided with a frame having a plurality of transverse ribs, a textile carrying plane extending over the same, and a plurality of transverse strips extendingbeneath the ribs from end to end and secured to the plane at a substantial distance from the ribs to form sides that slope uniformly from the center of the ribs to the outer edges of the strips, whereby the air is evenly deflected from the ribs during action.
ERNEST F. VON DREDEN. HERBERT R. HOFMANN. Witnesses:
ARTHUR E. ZUNYER, KATHERYNE K0011.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US62373811A US1043079A (en) | 1911-04-27 | 1911-04-27 | Flying-machine. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US62373811A US1043079A (en) | 1911-04-27 | 1911-04-27 | Flying-machine. |
Publications (1)
Publication Number | Publication Date |
---|---|
US1043079A true US1043079A (en) | 1912-11-05 |
Family
ID=3111353
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US62373811A Expired - Lifetime US1043079A (en) | 1911-04-27 | 1911-04-27 | Flying-machine. |
Country Status (1)
Country | Link |
---|---|
US (1) | US1043079A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2472763A (en) * | 1946-08-05 | 1949-06-07 | Jack F Rodeck | Airplane |
US20090039207A1 (en) * | 2007-08-09 | 2009-02-12 | Silverlit Toys Manufactory, Ltd. | Flying object |
CN101433765B (en) * | 2007-11-13 | 2011-11-16 | 银辉玩具制品厂有限公司 | Flight object |
-
1911
- 1911-04-27 US US62373811A patent/US1043079A/en not_active Expired - Lifetime
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2472763A (en) * | 1946-08-05 | 1949-06-07 | Jack F Rodeck | Airplane |
US20090039207A1 (en) * | 2007-08-09 | 2009-02-12 | Silverlit Toys Manufactory, Ltd. | Flying object |
US7971824B2 (en) * | 2007-08-09 | 2011-07-05 | Silverlit Limited | Flying object |
CN101433765B (en) * | 2007-11-13 | 2011-11-16 | 银辉玩具制品厂有限公司 | Flight object |
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