US516581A - wellne r - Google Patents
wellne r Download PDFInfo
- Publication number
- US516581A US516581A US516581DA US516581A US 516581 A US516581 A US 516581A US 516581D A US516581D A US 516581DA US 516581 A US516581 A US 516581A
- Authority
- US
- United States
- Prior art keywords
- ribs
- eccentric
- rotary
- lifting surfaces
- axle
- 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
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 1
- 239000013013 elastic material Substances 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 239000007779 soft material Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 239000002023 wood Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/006—Paddle wheels
Definitions
- the rotary sail for flying machines which forms the subject of this invention consists of an axle provided with arms and around them are arranged lifting surfaces, which are turned at slight angles during the revolution by a fixed eccentric with eccentric strap and rods.
- the rotation of the rotary sail when the axle is in the horizontal position produces the lifting power for rising and soaring in the air and in addition hereto under certain circumstances the production of powerfor driving in a horizontal direction for the purpose of producing forward motion in the direction of the axle.
- Figure 1 of the accompanying drawings is an end view of the rotary sail and Fig. 2 a part longitudinal section.
- A is the axis of rotation, which is mounted in bearings in the standards 0 and in the journals B connected to the said bearings.
- the shaft A has keyed thereon or otherwise fixed thereto the arms D forming a sort of star wheel.
- Either made in one with or fixedly connected to the journals B are the eccentric disks E, the eccentric straps 1 of which each have a rigid rod H while the others (seven in the present case) have jointed connecting rods G.
- the lifting surfaces F of which there are eight, are arranged drum-fashion around the axle and have stiffening ribs J each of which has two bolts or studs through which they are movably connected to the star wheel D and to the eccentric by the rods H and G.
- the front edge of the lifting surfaces in the uppermost position (No. 3) is raised or is further from the center and in the lowest position (No. 7) is nearer the center at every revolution while it'gradually takes up intermediate position at. other periods, so that in the horizontal positions as shown at No. 1 to the right and No. 5 to the left, the lifting surfaces come near to the dotted circle of revolution.
- the ribs of the lifting surfaces and also the arms D, G and H may be made in the form of a screw so that when revolving they may work to propel in the direction of the axle in the same way as the propeller of a steam ship works in the water. If the ribs and arms are not made in this manner then the rotary sail merely has a lifting but no propelling power.
- lifting surfaces are shown of an oval form and partly circular in section with decreasing thickness from front to back, other forms may however if considered advisable be utilized such as for instance, rightangled elliptic, egg shaped, pointed wingshaped and the like and other sections employed such for instance rectilinear tapering, parabolically curved or with sharper or easier curves.
- a hard substance with stiff ribs may be used such as for instance wood, tinned iron, vulcanite and the like or instead thereof flexible elastic and soft material may be employed such as silk, linen, sail, cloth or the like with stiff or flexible ribs.
- the number of the arms of the wheels, of the star wheel systems and of the lifting surfaces depends upon the size of the rotary sail.
- Motion is communicated to the axle of the rotary sails from a'motor by means of cranks K as shown in Fig. 2 or by tooth wheels, pulley wheels, or in any other well known manner.
- the rotary sail mechanism with regard to the connection of the movable surfaces with the fixed eccentric, slightly resembles Morgans paddle wheel mechanism for steamships but the action and arrangement of the lifting surfaces in the rotary sail is quite difierent.
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Moulding By Coating Moulds (AREA)
Description
(No Model.) 2 Sheets-:Sheet 1. G. WELLNER.
FLYING APPARATUS.
N0.516,581. I Patented Mar. 13, 1894.
2 Sheets-Sheet 2.
(No Model.)
G WBLLNER FLYING APPARATUS. N0. 516,581.
Patented Mar. 13, 1894.
renzo aezzwn UNITED STATES PATENT OFFIQE.
GEORG WELLNER, or BRUNN, AUSTRIA-HUNGARY.
FLYING APPARATUS.
SPECIFICATION forming part of Letters Patent No. 516,581, dated March 13, 1894.
Application filed June 17, 1893. Serial No. 478,183. (No model.) Patented in Germany April 22, 1893, No. 71,903 in France May 2, 1293,11). 229,796, andin England May 26,1893,N0.10,4=05.
To all whom it may concern.-
Be it known thatI, GEORG WELLNER, a subject of theEmperor of Austria-Hungary, residingatBriinn,l\/Ioravia,Austria-Hungary,have invented certain new and useful Improvements in Propeller-Wheels for Flying-Machines, (for which I have secured patents in Germany, No. 71,903, dated April 22,1893; in England, No. 10,405, dated May 26, 1893, and in France, No. 229,796, dated May 2, 1893,) of which the following is a specification.
The rotary sail for flying machines which forms the subject of this invention consists of an axle provided with arms and around them are arranged lifting surfaces, which are turned at slight angles during the revolution by a fixed eccentric with eccentric strap and rods. The rotation of the rotary sail when the axle is in the horizontal position produces the lifting power for rising and soaring in the air and in addition hereto under certain circumstances the production of powerfor driving in a horizontal direction for the purpose of producing forward motion in the direction of the axle.
Figure 1 of the accompanying drawings is an end view of the rotary sail and Fig. 2 a part longitudinal section.
. A is the axis of rotation, which is mounted in bearings in the standards 0 and in the journals B connected to the said bearings. The shaft A has keyed thereon or otherwise fixed thereto the arms D forming a sort of star wheel. Either made in one with or fixedly connected to the journals B are the eccentric disks E, the eccentric straps 1 of which each have a rigid rod H while the others (seven in the present case) have jointed connecting rods G. The lifting surfaces F, of which there are eight, are arranged drum-fashion around the axle and have stiffening ribs J each of which has two bolts or studs through which they are movably connected to the star wheel D and to the eccentric by the rods H and G. In consequence of this movable connection with the eccentric, the front edge of the lifting surfaces (see direction of the arrow in Fig. 1) in the uppermost position (No. 3) is raised or is further from the center and in the lowest position (No. 7) is nearer the center at every revolution while it'gradually takes up intermediate position at. other periods, so that in the horizontal positions as shown at No. 1 to the right and No. 5 to the left, the lifting surfaces come near to the dotted circle of revolution. In addition, the ribs of the lifting surfaces and also the arms D, G and H may be made in the form of a screw so that when revolving they may work to propel in the direction of the axle in the same way as the propeller of a steam ship works in the water. If the ribs and arms are not made in this manner then the rotary sail merely has a lifting but no propelling power.
On the drawings the lifting surfaces are shown of an oval form and partly circular in section with decreasing thickness from front to back, other forms may however if considered advisable be utilized such as for instance, rightangled elliptic, egg shaped, pointed wingshaped and the like and other sections employed such for instance rectilinear tapering, parabolically curved or with sharper or easier curves.
With regard to the material of which the lifting surfaces are to be made, a hard substance with stiff ribs may be used such as for instance wood, tinned iron, vulcanite and the like or instead thereof flexible elastic and soft material may be employed such as silk, linen, sail, cloth or the like with stiff or flexible ribs.
The number of the arms of the wheels, of the star wheel systems and of the lifting surfaces depends upon the size of the rotary sail.
Motion is communicated to the axle of the rotary sails from a'motor by means of cranks K as shown in Fig. 2 or by tooth wheels, pulley wheels, or in any other well known manner.
The rotary sail mechanism with regard to the connection of the movable surfaces with the fixed eccentric, slightly resembles Morgans paddle wheel mechanism for steamships but the action and arrangement of the lifting surfaces in the rotary sail is quite difierent.
With reference to the disposition of the rotary sails for flying machines it should be observed, that they may either be used singly or two or more close to each other (and in that ner faces, the eccentrics on said shaft having the rods pivotally joined to said ribs, said radial supports also being joined to said ribs so that the Wheel operates in the manner and for the purpose set forth.
In testimony whereof I have signed my I name to this specification in the presence of two subscribing witnesses.
GEORG WELLNER. Witnesses:
J on. E. BRUK, RUDOLF v. LIOHTENFELS.
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US516581A true US516581A (en) | 1894-03-13 |
Family
ID=2585386
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US516581D Expired - Lifetime US516581A (en) | wellne r |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US516581A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20060199514A1 (en) * | 2004-11-29 | 2006-09-07 | Sony Corporation | Cooling fan and image display apparatus |
| US20180044012A1 (en) * | 2016-08-10 | 2018-02-15 | Bell Helicopter Textron Inc. | Aircraft with tilting cross-flow fan wings |
| US20180044010A1 (en) * | 2016-08-10 | 2018-02-15 | Bell Helicopter Textron Inc. | Aircraft tail with cross-flow fan systems |
| US10377480B2 (en) * | 2016-08-10 | 2019-08-13 | Bell Helicopter Textron Inc. | Apparatus and method for directing thrust from tilting cross-flow fan wings on an aircraft |
-
0
- US US516581D patent/US516581A/en not_active Expired - Lifetime
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20060199514A1 (en) * | 2004-11-29 | 2006-09-07 | Sony Corporation | Cooling fan and image display apparatus |
| US7518864B2 (en) * | 2004-11-29 | 2009-04-14 | Sony Corporation | Cooling fan and image display apparatus |
| US20180044012A1 (en) * | 2016-08-10 | 2018-02-15 | Bell Helicopter Textron Inc. | Aircraft with tilting cross-flow fan wings |
| US20180044010A1 (en) * | 2016-08-10 | 2018-02-15 | Bell Helicopter Textron Inc. | Aircraft tail with cross-flow fan systems |
| US10377480B2 (en) * | 2016-08-10 | 2019-08-13 | Bell Helicopter Textron Inc. | Apparatus and method for directing thrust from tilting cross-flow fan wings on an aircraft |
| US10421541B2 (en) * | 2016-08-10 | 2019-09-24 | Bell Helicopter Textron Inc. | Aircraft with tilting cross-flow fan wings |
| US10479495B2 (en) * | 2016-08-10 | 2019-11-19 | Bell Helicopter Textron Inc. | Aircraft tail with cross-flow fan systems |
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