US1718109A - Heavier-than-air airship - Google Patents
Heavier-than-air airship Download PDFInfo
- Publication number
- US1718109A US1718109A US277333A US27733328A US1718109A US 1718109 A US1718109 A US 1718109A US 277333 A US277333 A US 277333A US 27733328 A US27733328 A US 27733328A US 1718109 A US1718109 A US 1718109A
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- Prior art keywords
- plane
- airship
- car
- cables
- heavier
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- Expired - Lifetime
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- 241000765115 Planetes Species 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000002459 sustained effect Effects 0.000 description 1
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
Definitions
- a heavier-than-air airship comprising an elongated plane the width of which is equal to or less than one-fifth the length thereof, a car below the center of the plane, said plane being inclined downwardly and forwardly relative to the car at an angle of from iive to fifteen degrees, a central gas container separate from the plane and connected to and directly over the car, said central container being of such size as to nearly support the weight of the car and its load, end gas containers carried by and adapted to support the plane7 cables connecting the sides of the front portion of the plane to the sides of the front portion of the car, longer cables connecting the sides of the rear portion of the plane to the sides of the rear portion of the car, means for pulling the cables in predetermined succession thereby to successively pull upon rpredetermined corner portions of the planete elevate the car relative to the plane 'and for subsequently paying out the cablesin predetermined succession to allow the corresponding portions of the plane to rise under the action of the gas in the container, said relative movement of the gas sustained plane operating to fpropel the airship in a
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Description
June 18, 1929.
G. c. BROWN 1.718.109
HEAVIERTHANAIR AIRSHIP Filed May l2, 1928 @fa/P65 C. SILPa//z//V 6 WV 5 f 50:51# l 'la @Holme/14o.
Patented June 18, 1929.
1,718,1ee PATENT OFFICE.
GEORGE COLEMAN BROWN,.OF DALLAS, TEXAS. y
HEAVIER-THAN--AIR AIRSHIP.
Application filed May 12,
This invention relates to a heavier-thanair airship and to a method of operating the same, it being designed more especially as an improvement upon the structure disclosed in Patent Number 1,315,084 issued to me on September 2nd, 1919. l
One of the objects of the invention 1s to provide an airship of this type utilizing a central gas container which is connectedto the car of the airship, this container being of such size as to nearly lift the car and its load, there being a framebeneath and separate fromthe the central container provided at its ends with additional gas containers, means being employed by which the plane can be shifted relative to thesupported car so as to cause the airship to ascend, descend, go forwardly, and to be turned in any desired direction.
A further object is to provide a novel arrangement of cables or other operating connections so located and proportioned as to shift the plane properly .during the actuation of the airship.
With the foregoing and other objects in view which will appear as the description proceeds the invention resides in thek combination and arrangement of parts and in the details of construction hereinafter described and claimed it being understood that changes in the precise embodiment of the invention herein 'disclosed may be made within the scope of what is claimed without departing from the spirit of the invention.
In the accompanying drawings the preferred form of the invention has been shown.
In said drawings,
Figure 1 is a side elevation of the airship.
Figure 2 is a section on line 2-2, Figure l.
Figure 3 is a section on line 3 3, Figure 1.
Figure 4 is a section on line 4-4, Figure 1.
Referring to the figures by characters of reference A designates an elongated plane extending above the top of a car B. This plane is extended along the bottom of a central gas container C, a front gas container D, and a rear -gas container E, all of these containers being in alinement as shown and the plane being inclined upwardly and rearwardly. Relatively short cables 1 and 2 are connected to the front end of the plane the corners thereof and longer cables 3 and 4 are connected to the corner portions of the 192s. serial No. 277,333.
they are attached to operating cranks l 5 adapted to be rotated by any suitable power means located in the car. The front and back containers D and E vcarried by the plane are located beyond the front and rear Iends respectively of the car whereas the middle container C, which is connectedk to the car, is located directly over the car and is separate from the plane. This container has cables 6 which are extended downwardly and connected to the car B as shown. y The car B and the kequipment carried thereby constitute a load somewhat heavier thanthat which can be liftedby the gas contained in the containers C, D, and. E but the gas in the end containers D and E will be sufiicient'to maintain the `plane A in elevated, position` above the car. e n
In practice it has been found that best results can be obtained by using a plane A approximately five times as long as it is wide and that the plane should be inclined at from five to fifteen degrees. It has also been found desirable tohave the end cables 1,- 2, 3, and 4 extended at approximately fortyfive degrees-in the direction of the length of the airship and approximately five degrees transversely of the airship. These angles are disclosed approximately `in Figures 1 and 2.
It has also been found desirable to make the ends of the containers D and E rounded Y or pointed to facilitate forward travel while rounded to facilitate the ascent of the airship. The bottom surface of the plane A is either flat orv concaved transversely so as` to insure proper downward displacement of air during the actuation of the mechanism. Supporting wheels 7 can be connected to the bottom of the car B to aid it in leaving the ground and while making a landing. v
In practice the gas container C, which is arranged directly over and connected to the car, is inflated to sustain a part, but not all, of the weight of the car and its load. By using this container the load which can be carried by the airship is greatly increased over what would be possible should the gas container be eliminated.
The airship heretofore described is operated to ascend and to go forward through the air by pulling on and releasing the cables in proper succession, this being done by means of the motor driven'cranks 5. The
By continuing the operation ust described the airship is elevated to a desired altitude where it can be maintained by continuing the actuation of the plane at a lower speed. While the cables are operated successively during 'the ascentof the airship, as already explained, any suitable means may be employed for separately actuating the cranks So that the cables will be operated in pairs. If the front cables l and 2 are operated in unison followed by the operation of the rear cables 3 and 4 the airship can be caused to i move forwardly. The turning of the airship can be effected by operatingr the cables 1 and 4 more rapidly than the cables 2 and 3 or vice versa, thereby turning the vehicle either to the right or to the left.
It is to be understood of course that the drawing only illustrates this invention diagrammatically. Any type of car can be used and obviously the shape of the plane can be varied to produce desired results.
llVhat is claimed is:
A heavier-than-air airship comprising an elongated plane the width of which is equal to or less than one-fifth the length thereof, a car below the center of the plane, said plane being inclined downwardly and forwardly relative to the car at an angle of from iive to fifteen degrees, a central gas container separate from the plane and connected to and directly over the car, said central container being of such size as to nearly support the weight of the car and its load, end gas containers carried by and adapted to support the plane7 cables connecting the sides of the front portion of the plane to the sides of the front portion of the car, longer cables connecting the sides of the rear portion of the plane to the sides of the rear portion of the car, means for pulling the cables in predetermined succession thereby to successively pull upon rpredetermined corner portions of the planete elevate the car relative to the plane 'and for subsequently paying out the cablesin predetermined succession to allow the corresponding portions of the plane to rise under the action of the gas in the container, said relative movement of the gas sustained plane operating to fpropel the airship in a desired direction.r Y
In testimony that I claim the foregoing as my own, I have hereto aiiiXed my signature. Y
GEORGE COLEMAN BROWN.l
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US277333A US1718109A (en) | 1928-05-12 | 1928-05-12 | Heavier-than-air airship |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US277333A US1718109A (en) | 1928-05-12 | 1928-05-12 | Heavier-than-air airship |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1718109A true US1718109A (en) | 1929-06-18 |
Family
ID=23060402
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US277333A Expired - Lifetime US1718109A (en) | 1928-05-12 | 1928-05-12 | Heavier-than-air airship |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1718109A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2512824A (en) * | 1948-08-24 | 1950-06-27 | Brown George Coleman | Heavier-than-air airship |
| US5348251A (en) * | 1991-09-09 | 1994-09-20 | Ferguson F D | Dirigible airship |
| US20090045284A1 (en) * | 2007-08-17 | 2009-02-19 | Chu Adam N | Corded Orientation System For Lighter-Than-Air Aircraft |
| US20170096209A1 (en) * | 2014-06-18 | 2017-04-06 | Nikolai Borisowich SHULGIN | "vestaplan" gliding helistat |
-
1928
- 1928-05-12 US US277333A patent/US1718109A/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2512824A (en) * | 1948-08-24 | 1950-06-27 | Brown George Coleman | Heavier-than-air airship |
| US5348251A (en) * | 1991-09-09 | 1994-09-20 | Ferguson F D | Dirigible airship |
| US20090045284A1 (en) * | 2007-08-17 | 2009-02-19 | Chu Adam N | Corded Orientation System For Lighter-Than-Air Aircraft |
| US20170096209A1 (en) * | 2014-06-18 | 2017-04-06 | Nikolai Borisowich SHULGIN | "vestaplan" gliding helistat |
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