US1577756A - Balloon - Google Patents
Balloon Download PDFInfo
- Publication number
- US1577756A US1577756A US755001A US75500124A US1577756A US 1577756 A US1577756 A US 1577756A US 755001 A US755001 A US 755001A US 75500124 A US75500124 A US 75500124A US 1577756 A US1577756 A US 1577756A
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- US
- United States
- Prior art keywords
- balloon
- air
- gas
- bags
- envelope
- 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
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/58—Arrangements or construction of gas-bags; Filling arrangements
- B64B1/62—Controlling gas pressure, heating, cooling, or discharging gas
Definitions
- This invention relates to improvements in lighter-thanair crafts, and has for its principal object to provide a balloon wherein means is associated therewith for facilitating the ascension and descension in a simple and'efiicient manner.
- One of the importantobjeets of the present invention is to provide a balloon which includes a plurality of gas bags which are inflated with an expansible gas, air bags being positioned below the gas bags for com pressing the gas bags when inflated with air to facilitate the 'descension of the balloon withoutthe loss of the expansible gas within the gas bags, the air bags being deflated to permit the expansion of the gas in the gas bags during the ascension of the balloon.
- a further object of the invention is to provide a balloon of the above mentioned character wherein means is associated for cooperation with the propeller of the balloon for collecting air and discharging the same into the air bags, additional means being provided for controlling the supply of air to each of the air bags thus enabling the I balloon to be easilystabilized.
- a further object of the invention is to provide aballoon of the above mentioned character, which is simple in construction, inexpensive, strong and durable and furthermore adapted for the purposes for which it is designated.
- the figure represents a view'partly in section, and partly diagrammatic.
- the numeral 1 designates the envelope balloon, the same being preferably in the shape of a cigar.
- the usual earriage whieh is supported and suspended below the en of my improved velope is not shown in the drawing, but the propeller of the engine is illustrated at.2,
- Suitable vertically extending partitions 3 are arranged within'the envelope 1 whereby the compartments d are formed in the enthe compartments is a gas bag 5 whichis. adapted to be inflated with expansible gas in any well known manner. so arranged in each of the compartments 4 below the inflated gas bag therein is the air bag 6.
- Air is supplied to the air bags through the several distributor pipe lines 7 which are connectedatoneend to the respective air bags and at their opposite ends to a'main feed line 8.
- the latter in turn is associated, with? a suitable air receiving and discharging member designated generally by the numeral 9, which may comprise either an air compressonblower fan or air collector, the same being disposed rearwardly of the propeller 2 and furthermore provided with the funnel shaped air receiver 10.
- Suitable cut off valves 11 are associated with the independent distributor pipes 7 and for cutting off the supplyof air from the main feed line 8 to the distributor pipe 7, I provide a valve 12 in the main feed line as clearly illustrated in the drawing.
- the air is released from the air bags 6 so that the gas in the gas bags 5 will expand, thus permitting the balloon to rise to the desired altitude.
- the air is released from the air bags so that the gas in the gas bags will expand nearly to the atmospheric pressure.
- air is charged into the air bags, causing the same to become inflated and furthermore causing the compression ofthe gas bags without increasing the pressure in the envelope. This will decrease the lifting power, relieving the upward pressure of the gas on the upper half of the; balloon and distributing a like pressure on the lower half of the balloon.
- velopea Adapted to be'disposed in each of pern'iitting the efficient descen-sion of the balloon.
- the provision of thecontrol valves 11 in the independent distributor pipes .7 will enable the balloon to be maintained in a stabilized position whil in the air, and the valves are so arranged as to enable theoperator within the carriage to have ready access thereto.
- a balloon of the above mentioned charac' ter may be constructed at a very low cost and will further be strong and durable, and the operation thereof will at all times .be positive and etlicient.
- a balloon including in combination with the usual propeller associated therewith, an 'lD'lPGlfOlEI'EGCl envelope, partitions .in the envelopedividing the same into a pin rality of compartments, an inflated gas bag separate from and independent of the en velope 1n each compartment, an an bag separate from .and independent of the ensaid lI ⁇ O.l11l)Q1,'il.HCl distributor pipes connecting said air bags with the said feed pipe.
- a balloon including in combination the usual propeller, an in'lperforated envelope, partitions in the envelope dividing the same into In plurality of compartments, an inflated gas bag separate from and independentof the envelope beneath the compartment, an air bag iin each compartn'icnt separate from and independent of the gas bag and the :envelope and disposed below said gas bags therein, means for inflating the air bags consisting of an air receiving and discharging member disposed rearwardly of sald propeller and 1110011111111111C21fi1011 therewith, a feed.pipeextending from said member, distributor pipes connectingsaid air bags with said teed pipe -valves in saiddistributor pipes, and valves in said feed pipes.
Description
March as 1926.
7 I. W. REAGAN BALLOON Filed Dec. 10, 1924 J. WF
Patented Mar. 23, 1926.
* UNITED STATES IRVIN W REAGAN, or ELFERS, FLORIDA.
BALLOON,
Application filed December 10, 1924. Serial No. 755,001.
1 '0 all whom it may concern I Be it known that I, IRVIN W. REAGAN, a citizen of the United States, lGSKllllg. at Eliers, in the county of Pasco and State: Florida, have invented certamnew and'usc-' ful Innarovements in a Balloon, of which the following is a specification.
This invention relates to improvements in lighter-thanair crafts, and has for its principal object to provide a balloon wherein means is associated therewith for facilitating the ascension and descension in a simple and'efiicient manner. I
One of the importantobjeets of the present invention is to provide a balloon which includes a plurality of gas bags which are inflated with an expansible gas, air bags being positioned below the gas bags for com pressing the gas bags when inflated with air to facilitate the 'descension of the balloon withoutthe loss of the expansible gas within the gas bags, the air bags being deflated to permit the expansion of the gas in the gas bags during the ascension of the balloon. A further object of the invention is to provide a balloon of the above mentioned character wherein means is associated for cooperation with the propeller of the balloon for collecting air and discharging the same into the air bags, additional means being provided for controlling the supply of air to each of the air bags thus enabling the I balloon to be easilystabilized.
A further object of the invention is to provide aballoon of the above mentioned character, which is simple in construction, inexpensive, strong and durable and furthermore adapted for the purposes for which it is designated.
Other objects and advantages of this invention will become apparent during the course of thefollowing description.
Inthe accompanying drawing forming a part of this specification and in which like numerals designate like parts throughout the same: 7
The figure represents a view'partly in section, and partly diagrammatic.
In the drawing, wherein for the purpose of, illustration is shown the preferred. em bodiment of my invention, the numeral 1 designates the envelope balloon, the same being preferably in the shape of a cigar. The usual earriage whieh is supported and suspended below the en of my improved velope is not shown in the drawing, but the propeller of the engine is illustrated at.2,
the engine being also i. not shown for the reason that the same forms no important part of the present invention. 7
Suitable vertically extending partitions 3 are arranged within'the envelope 1 whereby the compartments d are formed in the enthe compartments is a gas bag 5 whichis. adapted to be inflated with expansible gas in any well known manner. so arranged in each of the compartments 4 below the inflated gas bag therein is the air bag 6.
. Air is supplied to the air bags through the several distributor pipe lines 7 which are connectedatoneend to the respective air bags and at their opposite ends to a'main feed line 8. The latter in turn is associated, with? a suitable air receiving and discharging member designated generally by the numeral 9, which may comprise either an air compressonblower fan or air collector, the same being disposed rearwardly of the propeller 2 and furthermore provided with the funnel shaped air receiver 10. Suitable cut off valves 11 are associated with the independent distributor pipes 7 and for cutting off the supplyof air from the main feed line 8 to the distributor pipe 7, I provide a valve 12 in the main feed line as clearly illustrated in the drawing. a
When the balloon is about to ascend, the air is released from the air bags 6 so that the gas in the gas bags 5 will expand, thus permitting the balloon to rise to the desired altitude. The air is released from the air bags so that the gas in the gas bags will expand nearly to the atmospheric pressure. When it is desired to descend, air is charged into the air bags, causing the same to become inflated and furthermore causing the compression ofthe gas bags without increasing the pressure in the envelope. This will decrease the lifting power, relieving the upward pressure of the gas on the upper half of the; balloon and distributing a like pressure on the lower half of the balloon. By permitting the air bags to become inflated, thus compressing the gas bags within the compartments of the envelope, when descending, it will not be necessary to discharge any of the gas from the-gas bags as is now usually done, thus preventing any unneces sary waste of the gas from the gas bags; yet
velopea. Adapted to be'disposed in each of pern'iitting the efficient descen-sion of the balloon. The provision of thecontrol valves 11 in the independent distributor pipes .7 will enable the balloon to be maintained in a stabilized position whil in the air, and the valves are so arranged as to enable theoperator within the carriage to have ready access thereto.
A balloon of the above mentioned charac' ter, may be constructed at a very low cost and will further be strong and durable, and the operation thereof will at all times .be positive and etlicient.
While I have shown the preferred embodiment of my invention, it is to be understood that various changes in the size, shapeand arrangement of parts may be resorted to without departing from the spiritof the invention and the scope of the appended claims. 7
Having thus described the invention, what I claim is 1. A balloon including in combination with the usual propeller associated therewith, an 'lD'lPGlfOlEI'EGCl envelope, partitions .in the envelopedividing the same into a pin rality of compartments, an inflated gas bag separate from and independent of the en velope 1n each compartment, an an bag separate from .and independent of the ensaid lI\O.l11l)Q1,'il.HCl distributor pipes connecting said air bags with the said feed pipe.
2. A balloon including in combination the usual propeller, an in'lperforated envelope, partitions in the envelope dividing the same into In plurality of compartments, an inflated gas bag separate from and independentof the envelope beneath the compartment, an air bag iin each compartn'icnt separate from and independent of the gas bag and the :envelope and disposed below said gas bags therein, means for inflating the air bags consisting of an air receiving and discharging member disposed rearwardly of sald propeller and 1110011111111111C21fi1011 therewith, a feed.pipeextending from said member, distributor pipes connectingsaid air bags with said teed pipe -valves in saiddistributor pipes, and valves in said feed pipes.
In testlnony whereof Iafiix my signature.
lnviu w. nnaeiin.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US755001A US1577756A (en) | 1924-12-10 | 1924-12-10 | Balloon |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US755001A US1577756A (en) | 1924-12-10 | 1924-12-10 | Balloon |
Publications (1)
Publication Number | Publication Date |
---|---|
US1577756A true US1577756A (en) | 1926-03-23 |
Family
ID=25037287
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US755001A Expired - Lifetime US1577756A (en) | 1924-12-10 | 1924-12-10 | Balloon |
Country Status (1)
Country | Link |
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US (1) | US1577756A (en) |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4773617A (en) * | 1987-03-05 | 1988-09-27 | Mccampbell Burton L | Lighter-than-air craft |
WO1990009312A1 (en) * | 1987-08-20 | 1990-08-23 | Wintzell, Bruno | Device for adjustment of the height of an airship |
US5143322A (en) * | 1989-04-03 | 1992-09-01 | Mason Earl W | Ground handling, altitude control and longitudinal stability of airships |
EP1394038A1 (en) * | 2001-05-11 | 2004-03-03 | Kawasaki Jukogyo Kabushiki Kaisha | Airship |
US20060065777A1 (en) * | 2004-09-27 | 2006-03-30 | Walden Michael K | Systems for actively controlling the aerostatic lift of an airship |
US20060266886A1 (en) * | 2005-05-24 | 2006-11-30 | Nachbar Daniel W | Hoop stress reduction in a buoyant airship |
US20080135678A1 (en) * | 2006-10-23 | 2008-06-12 | Heaven George H | Buoyancy control system for an airship |
US20080265086A1 (en) * | 2007-04-27 | 2008-10-30 | Yee-Chun Lee | Long mission tethered aerostat and method of accomplishing |
US20090114768A1 (en) * | 2007-04-24 | 2009-05-07 | Michael Todd Voorhees | Aerostatic Buoyancy Control System |
US20110062289A1 (en) * | 2009-09-14 | 2011-03-17 | Chu Adam N | Envelope With Gas Management System For Lighter-Than-Air Aircraft |
JP2011093422A (en) * | 2009-10-29 | 2011-05-12 | Kawasaki Heavy Ind Ltd | Airship and attitude control method of the same |
US20120223181A1 (en) * | 2011-03-01 | 2012-09-06 | John Ciampa | Lighter-Than-Air Systems, Methods, and Kits for Obtaining Aerial Images |
EP2514666A1 (en) * | 2011-04-20 | 2012-10-24 | Lockheed Martin Corporation | Vehicle comprising heavier than air internal ballast |
US8505847B2 (en) | 2011-03-01 | 2013-08-13 | John Ciampa | Lighter-than-air systems, methods, and kits for obtaining aerial images |
US9211942B1 (en) * | 2013-07-01 | 2015-12-15 | Google Inc. | Controlled balloon descent using straws |
-
1924
- 1924-12-10 US US755001A patent/US1577756A/en not_active Expired - Lifetime
Cited By (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4773617A (en) * | 1987-03-05 | 1988-09-27 | Mccampbell Burton L | Lighter-than-air craft |
WO1990009312A1 (en) * | 1987-08-20 | 1990-08-23 | Wintzell, Bruno | Device for adjustment of the height of an airship |
US5251850A (en) * | 1987-08-20 | 1993-10-12 | Bruno Wintzell | Device for adjustment of the height of an airship |
AU650613B2 (en) * | 1987-08-20 | 1994-06-30 | Torsten Anders Bertil Noren | Device for adjustment of the height of an airship |
US5143322A (en) * | 1989-04-03 | 1992-09-01 | Mason Earl W | Ground handling, altitude control and longitudinal stability of airships |
EP1394038A4 (en) * | 2001-05-11 | 2009-05-13 | Kawasaki Heavy Ind Ltd | Airship |
EP1394038A1 (en) * | 2001-05-11 | 2004-03-03 | Kawasaki Jukogyo Kabushiki Kaisha | Airship |
US20060065777A1 (en) * | 2004-09-27 | 2006-03-30 | Walden Michael K | Systems for actively controlling the aerostatic lift of an airship |
US7156342B2 (en) * | 2004-09-27 | 2007-01-02 | Ltas Holdings, Llc | Systems for actively controlling the aerostatic lift of an airship |
US7669796B2 (en) * | 2005-05-24 | 2010-03-02 | Daniel Nachbar | Hoop stress reduction in a buoyant airship |
US20060266886A1 (en) * | 2005-05-24 | 2006-11-30 | Nachbar Daniel W | Hoop stress reduction in a buoyant airship |
US7487936B2 (en) | 2006-10-23 | 2009-02-10 | Ltas Holdings, Llc | Buoyancy control system for an airship |
US20080135678A1 (en) * | 2006-10-23 | 2008-06-12 | Heaven George H | Buoyancy control system for an airship |
US8091826B2 (en) | 2007-04-24 | 2012-01-10 | Michael Todd Voorhees | Aerostatic buoyancy control system |
US20090114768A1 (en) * | 2007-04-24 | 2009-05-07 | Michael Todd Voorhees | Aerostatic Buoyancy Control System |
US8083174B2 (en) | 2007-04-27 | 2011-12-27 | Stratocomm Corporation | Long mission tethered aerostat and method of accomplishing |
US20080265086A1 (en) * | 2007-04-27 | 2008-10-30 | Yee-Chun Lee | Long mission tethered aerostat and method of accomplishing |
US7708222B2 (en) * | 2007-04-27 | 2010-05-04 | Stratocomm Corporation | Long mission tethered aerostat and method of accomplishing |
US8485465B2 (en) | 2007-04-27 | 2013-07-16 | Stratocomm Corporation | Long mission tethered aerostat and method of accomplishing |
US20110062289A1 (en) * | 2009-09-14 | 2011-03-17 | Chu Adam N | Envelope With Gas Management System For Lighter-Than-Air Aircraft |
JP2011093422A (en) * | 2009-10-29 | 2011-05-12 | Kawasaki Heavy Ind Ltd | Airship and attitude control method of the same |
US20120223181A1 (en) * | 2011-03-01 | 2012-09-06 | John Ciampa | Lighter-Than-Air Systems, Methods, and Kits for Obtaining Aerial Images |
US8505847B2 (en) | 2011-03-01 | 2013-08-13 | John Ciampa | Lighter-than-air systems, methods, and kits for obtaining aerial images |
US8622338B2 (en) | 2011-03-01 | 2014-01-07 | John Ciampa | Lighter-than-air systems, methods, and kits for obtaining aerial images |
US9126669B2 (en) | 2011-03-01 | 2015-09-08 | John Ciampa | Lighter-than-air systems, methods, and kits for obtaining aerial images |
EP2514666A1 (en) * | 2011-04-20 | 2012-10-24 | Lockheed Martin Corporation | Vehicle comprising heavier than air internal ballast |
US8777156B2 (en) | 2011-04-20 | 2014-07-15 | Lockheed Martin Corporation | Heavier than air internal ballast |
US9211942B1 (en) * | 2013-07-01 | 2015-12-15 | Google Inc. | Controlled balloon descent using straws |
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