US1268494A - Airship. - Google Patents
Airship. Download PDFInfo
- Publication number
- US1268494A US1268494A US18341317A US18341317A US1268494A US 1268494 A US1268494 A US 1268494A US 18341317 A US18341317 A US 18341317A US 18341317 A US18341317 A US 18341317A US 1268494 A US1268494 A US 1268494A
- Authority
- US
- United States
- Prior art keywords
- tubes
- plane
- blades
- machine
- frame
- 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
- 238000010276 construction Methods 0.000 description 2
- 101100379079 Emericella variicolor andA gene Proteins 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 210000005069 ears Anatomy 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000010006 flight Effects 0.000 description 1
- 230000033001 locomotion Effects 0.000 description 1
- 230000002085 persistent effect Effects 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
- B64C29/0025—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being fixed relative to the fuselage
Definitions
- This invention relates to air ships, constructed and adapted to operate substantially as shown and described and particu larly pointed out in the claims.
- Figure 1 is a plan view of the ship or vessel
- Fig. 2 is a cross-section on line 2,2, Fig. 1.
- Fig. 3 is a side elevation.
- Fig. 4 is a front elevation and
- Fig. 5 is a perspective view of the rudder planes or blades and the immediate means for operating the same, the said planes being partially broken off and enf larged as compared with Flg. 3.
- the primary and essential novelty resides in the Hight tube or tubes a, a set or pair of tubes being shown herein,iratherthan one or more than two, and the said tubes serve the dual purpose of buoyancy and as mediums for the effectual application of the propelling power of tlie machine.
- Both tubes are alike in.y construction and service, and are s et side by ⁇ side horizontally into a rigid skeleton frame 2, so that vsaid tubes with the frame constitute a basic unit by which all the other parts are carried.
- the basket or boat b is suspended from thel aforesaid frame by suitable stays or supports 3, as may be needed, and the main stays or supports are bent to a curvature as seen in Fig. 3, to conform to the correspondingly rounded ends of the basket or boat kand the shafts of the Wheels 4 are supported by brackets 5 formed'of rods to give the desired bracing effects and carry the wheels on a suitable level below the bottom of the basket for running'and lighting purposes as usual.
- the basket or boat is built with closed bottom and sides to ride on the waterand is adapted lto carry the engines or other source of power indicated by 6, .as well as the crew and for other purposes.
- Suitable propellers 7 are shown as mounted in the respective ends of the tubes a on a shaft 8 running lengthwise in each tube and suitably braced therein, and power is communicated to said shafts from ythe engines or motive power by bevel gmr connections 9 and lshafts 10,- and said shafts have like ears 11 at their other or inner ends meshlng with master gear 12 on en gine driven shaft-14.
- the fly wheel 'ab is driven from the opposite end of shaftlfl by shaft 15 carrying the said Wheel and gears 16.
- suitable engine control will be provided though not shown herein, andwhile internal combustion engines of the gasolene type are preferred I do not mean to exclude other power mediums available.'
- the present equlprnent comprises simply a front steering plane 20 with a hand control from the boat by; the operator through'suitable means, such as rod 21 and crank connections 22 and 23 respectively, at its ends, or l the equivalent thereof, and through .which ⁇ the position of the plane for ascent or descent is controlled. therwise the said plane is pivotally supported at 24 outside on the respective tubes a.
- An aerial machine as described havingV a rigid frame .and a pair of flight tubes side by side in the upper portion of said frame and propeller Wheels therein and a basket suspended beneath the middle of said frame andrela'tively beneath said tubes, in combination withv an engine in said basket, power connections from said engine to said propellers, a vertically disposed shaft oper-v atively'- engaged witb the engine and extending upward between said tubes, and a horizontally positioned balance wheel on the end of said shaft above said tubes.
- a machine as described having a rigid frame and a pair of Hight tubes side by side lengthwise in said frame, shafts in said tubes and propeller blades on said shafts Within said tubes, an'engine and driving tubes andpropeller blades thereon, in combination with an engine in said frame beneath said. tubes and drive connections therefrom to said shafts through said tubes, and a balance wheel horizontally disposed over the middle ofsaid'tubes and operatively connected with said engine.
- a machine as described comprising a rigid frame, peller blades therein and an engine in driving connection with said blades', in combination with a horizontally positioned balance wheel centrally over said tubes and planes at the ends of said tubes.
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Description
A. c. RUTZEN.
Amsnlr.
APPLICATION FILED JULY 30. 1917.
Patented June; 1918.
. 2SIIEETS-$HEET 2- 4 l -zr I l I I I I I l... v
VAUGUST C. BUTZEN, 0F QLE 'f ein.
recaiga.
pecication of mettere Extent.
Application med Julyo, llf eilal Ho. 183,6213.
. I To all 'whom t may concern:
Be it known that I, AUGUST C. Ro'rzEN, citizen of the United States, residing at Cleveland, in the county of Cuyahogavand State of Ohio, have invented certain new and useful Improvements in Airships, of which the following is a. specification.
This invention relates to air ships, constructed and adapted to operate substantially as shown and described and particu larly pointed out in the claims.
In the accompanyingv drawings, Figure 1 is a plan view of the ship or vessel, and Fig. 2 is a cross-section on line 2,2, Fig. 1. Fig. 3 is a side elevation. Fig. 4 is a front elevation and Fig. 5 is a perspective view of the rudder planes or blades and the immediate means for operating the same, the said planes being partially broken off and enf larged as compared with Flg. 3. p
In the construction of a ship or vessel as i thus shown and adapted to make aerial flights, the primary and essential novelty resides in the Hight tube or tubes a, a set or pair of tubes being shown herein,iratherthan one or more than two, and the said tubes serve the dual purpose of buoyancy and as mediums for the effectual application of the propelling power of tlie machine. Both tubes are alike in.y construction and service, and are s et side by `side horizontally into a rigid skeleton frame 2, so that vsaid tubes with the frame constitute a basic unit by which all the other parts are carried.
The basket or boat b is suspended from thel aforesaid frame by suitable stays or supports 3, as may be needed, and the main stays or supports are bent to a curvature as seen in Fig. 3, to conform to the correspondingly rounded ends of the basket or boat kand the shafts of the Wheels 4 are supported by brackets 5 formed'of rods to give the desired bracing effects and carry the wheels on a suitable level below the bottom of the basket for running'and lighting purposes as usual. The basket or boat is built with closed bottom and sides to ride on the waterand is adapted lto carry the engines or other source of power indicated by 6, .as well as the crew and for other purposes.
Suitable propellers 7 are shown as mounted in the respective ends of the tubes a on a shaft 8 running lengthwise in each tube and suitably braced therein, and power is communicated to said shafts from ythe engines or motive power by bevel gmr connections 9 and lshafts 10,- and said shafts have like ears 11 at their other or inner ends meshlng with master gear 12 on en gine driven shaft-14. The fly wheel 'ab is driven from the opposite end of shaftlfl by shaft 15 carrying the said Wheel and gears 16. OfA course it is to be understood that suitable engine control will be provided though not shown herein, andwhile internal combustion engines of the gasolene type are preferred I do not mean to exclude other power mediums available.'
VIn the matter of planes, it will'be seen that the present equlprnent comprises simply a front steering plane 20 with a hand control from the boat by; the operator through'suitable means, such as rod 21 and crank connections 22 and 23 respectively, at its ends, or l the equivalent thereof, and through .which `the position of the plane for ascent or descent is controlled. therwise the said plane is pivotally supported at 24 outside on the respective tubes a.
vAt the rear of the machine, I show two rudder planes 26 and 27, the plane 26 being zontal plane 27 is supported on the rear edge of plane 26 by a shackle 29 fixed on plane 26 and a cross rod 30 fixed at its ends onl plane 27 oppositelyA at the end of theslot therein astride plane 26 and rotatably pivoted in said shackle, so that the plane 27 can -be manipulated to coperate with front plane 20 in all the movements ther f and for which suitable-hand control d means are provided" through crank arms 32 fixed on' shaft 30, and operating rods 33 connected with the ends of said arms and which form a part of the manipulating mechanism comprising sprocket chain or other connections over wheel 35 and hand wheel 36 or equivalent means. No novelty is claimed for these parts 'and the details are immaterial and not of the invention.
0f course it is to be understood that the terms front and rear are relative and that the machine can bepropelled either -end forward.
,It is to be especially noticed "that the propellers in this machine are limited to two blades each, and, without thought of disparaging `other machines that employ a greater number of blades, I have to s ay that Patented June 4, i918..Y
in all my experiments with this class of machines I have found that more than two blades would not work satisfactorily lto me.
Whether there is too much displacement for the size of the tube or some other cause Ido not pretend to say, but by persistent elfort I made the discovery that the secret in such a machine seems to lie in the use of two blades on each wheel,'and no more. With two blades the work of the machine is eminently vsatisfactory andA successful.
What I claim is:
1. An aerial machine as described havingV a rigid frame .and a pair of flight tubes side by side in the upper portion of said frame and propeller Wheels therein and a basket suspended beneath the middle of said frame andrela'tively beneath said tubes, in combination withv an engine in said basket, power connections from said engine to said propellers, a vertically disposed shaft oper-v atively'- engaged witb the engine and extending upward between said tubes, and a horizontally positioned balance wheel on the end of said shaft above said tubes.-
2. A machine as described, having a rigid frame and a pair of Hight tubes side by side lengthwise in said frame, shafts in said tubes and propeller blades on said shafts Within said tubes, an'engine and driving tubes andpropeller blades thereon, in combination with an engine in said frame beneath said. tubes and drive connections therefrom to said shafts through said tubes, and a balance wheel horizontally disposed over the middle ofsaid'tubes and operatively connected with said engine.
4. A machine as described, comprising a rigid frame, peller blades therein and an engine in driving connection with said blades', in combination with a horizontally positioned balance wheel centrally over said tubes and planes at the ends of said tubes.
a setof flighttubes and pro- `Signed at Cleveland, in the county of.
Cuyahoga and State of Ohio, this 28th day of July, A. D. 1917.
AUGUST c. RUTZEN.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US18341317A US1268494A (en) | 1917-07-30 | 1917-07-30 | Airship. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US18341317A US1268494A (en) | 1917-07-30 | 1917-07-30 | Airship. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1268494A true US1268494A (en) | 1918-06-04 |
Family
ID=3336135
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US18341317A Expired - Lifetime US1268494A (en) | 1917-07-30 | 1917-07-30 | Airship. |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1268494A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2511607A (en) * | 1948-07-17 | 1950-06-13 | Alexander N Turnquist | Fluid-propelled airplane |
-
1917
- 1917-07-30 US US18341317A patent/US1268494A/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2511607A (en) * | 1948-07-17 | 1950-06-13 | Alexander N Turnquist | Fluid-propelled airplane |
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