US1012559A - Aeroplane. - Google Patents
Aeroplane. Download PDFInfo
- Publication number
- US1012559A US1012559A US62745011A US1911627450A US1012559A US 1012559 A US1012559 A US 1012559A US 62745011 A US62745011 A US 62745011A US 1911627450 A US1911627450 A US 1911627450A US 1012559 A US1012559 A US 1012559A
- Authority
- US
- United States
- Prior art keywords
- bags
- aeroplane
- framework
- guides
- gas
- 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
- 239000007789 gas Substances 0.000 description 8
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- IWEDIXLBFLAXBO-UHFFFAOYSA-N dicamba Chemical compound COC1=C(Cl)C=CC(Cl)=C1C(O)=O IWEDIXLBFLAXBO-UHFFFAOYSA-N 0.000 description 3
- 238000005086 pumping Methods 0.000 description 3
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 238000009877 rendering Methods 0.000 description 1
- 230000002459 sustained effect Effects 0.000 description 1
Images
Classifications
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B2201/00—Hybrid airships, i.e. airships where lift is generated aerodynamically and statically
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
Definitions
- the object of the invention is to provide certain new and useful improvements in aeroplanes whereby the desired balance or stability is obtained, the lifting power is increased, and in case of accident to the motor or other parts the aeroplane is readily sustained in the air.
- use is made of inflatable bags mounted on the aeroplane and connected with means under the control of the aviator for inflating the bags wholly or partly according to circumstances.
- Figure 1 is a front elevation of an aeroplane provided with the improved stability devices;
- Fig. 2 is a sectional plan view of the same; and
- Fig. 3 is an enlarged sectional sideelevation of part of one of the bags.
- the aeroplane shown in the drawings is in the form of a biplane of any approved construction, having a framework A, spaced sustaining planes B, B, a propeller C, a gasolene tank E for supplying the motor with an explosive gas, and other parts and devices, such as are usually found in aeroplanes of this type, although it is expressly understood that my stability devices presently to be described in detail are applicable to other forms of aeroplanes, and hence I do not limit myself to applying my devices to any particular type of aeroplane.
- each of the bags G is made of rubber, silk orother suitable fabric in the form of bellows, inclosed in a cover or shell formed of metallic plates G, preferably aluminum, and connected with each other by hinges G the plates G overlying the corresponding folds of the bag G, and the hinges Gr at the sides being pivotally connected withrings H mounted to slide on the guide rods F.
- the bags G can be readily inflated or deflated, and at the same time are thoroughly protected by the cover made of hinged sections.
- a pipe I connects with the bottom of each bag G and leads to a pump J driven from the motor D or operated by hand, and the pump J has a pipe connection K with one or a series of tanks L filled with a light gas, such as hydrogen gas, either manufactured by suitable apparatus located on the framework A or the tanks L are filled with gas prior to using the aeroplane for an ascent.
- a light gas such as hydrogen gas
- the pump J is used for pumping gas from the tanks L into the inflatable bags G, to inflate the same to any desired extent, that is, wholly, as shown to the left of Fig. 1, or partly, as indicated on the right of Fi 2.
- the pump J may be used for pumping the gas from.the bags G back into the tanks L, it being understood that for this purpose suitable valves are arranged on the pump for the purpose mentioned. It is also understood that the pump J may be in the form of an air pump for pumping air into the bags G instead of hydrogen gas to inflate the said bags or deflate the same, as the case may be.
- An aeroplane comprising a framework, spaced planes one above the other, guides between the said planes, and inflatable and deflatable-bags mounted on the said guides and formed bellows-like for extensible and contractible movement under the effect of inflation and deflation.
- An aeroplane comprising a framework, spaced planes one above the other,.gu1des between the said planes, inflatable and deflat-able bags mounted onthe said guides and formed to increase and decrease in length in a vertical direction under the effect of inflation, and deflation, gas supply tanks. on the said framework, and a pump on the framework and connected with the said bags 1:gnd the tanks for inflating and deflating the ags. I v a 3.
- An aeroplane comprising a framework, sustaining planes one above the other and mounted on the said framework, guides on the said f amework, extensible and contractible bellows-like bags mounted on the said guides, and means under the control of the aviator for inflating or deflating the said bags, wholly or partly.; 4.
- An aeroplane comprising'a framework, sustaining planes one above the other and mounted on the said framework, guides on the said framework,inflatable bags in the form of bellows and provided with a sheet metal cover made in sections hinged together, and rings slidable on the said guides and on which the hinged cover sections are pivoted, and means under the control of the aviatorfor inflating the bags.
- An aeroplane provided with guides, and an inflatable b'agof bellows shape and .havinga cover formed of sheet metal sections hinged together, the cover sectionsoverlying the folds of the bag, and rings on able bag of bellows shape, and a metal cover for the same formed of plates overlying the folds of the bag and pivotally connected one with the other.
- An aeroplane provided with an inflat-' able bag of bellows shape and a metal cover for the same formed of plates overlying the folds of the bag and pivotally connected one with the other, and guides for the said cover.
- An aeroplane provided with sustaining planes, a framework, guides, extensible and contractible bellows-like bags mounted on the said guides, and means under the control of the aviator for filling-the said bags with a gas to extend the same or for discharging the gas from the bags to deflate thesame.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Bedding Items (AREA)
Description
MORRIS KALABA, OF NEW ROCHELLE, NEW YORK.
AEROPLANE.
Specification of Letters'l atent.
Patented Dec. 19, 1911.
Application filed May 16, 1911. Serial No. 627,450.
citizen of the United States, and a resident of New Rochelle, in the county of Vestchester and State of New York, have invented new and useful Improvements in Aeroplanes, of which the following is a full, clear, and exact description.
The object of the invention is to provide certain new and useful improvements in aeroplanes whereby the desired balance or stability is obtained, the lifting power is increased, and in case of accident to the motor or other parts the aeroplane is readily sustained in the air. For the purpose mentioned use is made of inflatable bags mounted on the aeroplane and connected with means under the control of the aviator for inflating the bags wholly or partly according to circumstances.
A practical embodimentof the invention is represented in the accompanying drawings forming a part of this specification, in which similar characters of reference indicate corresponding parts in allthe views.
Figure 1 is a front elevation of an aeroplane provided with the improved stability devices; Fig. 2 is a sectional plan view of the same; and Fig. 3 is an enlarged sectional sideelevation of part of one of the bags.
I The aeroplane shown in the drawings is in the form of a biplane of any approved construction, having a framework A, spaced sustaining planes B, B, a propeller C, a gasolene tank E for supplying the motor with an explosive gas, and other parts and devices, such as are usually found in aeroplanes of this type, although it is expressly understood that my stability devices presently to be described in detail are applicable to other forms of aeroplanes, and hence I do not limit myself to applying my devices to any particular type of aeroplane.
On the sides of the aeroplane, and preferably between the sustaining planes B and B, are arranged guide rods F for guiding inflatable bags G on inflating and deflating the same. Each of the bags G is made of rubber, silk orother suitable fabric in the form of bellows, inclosed in a cover or shell formed of metallic plates G, preferably aluminum, and connected with each other by hinges G the plates G overlying the corresponding folds of the bag G, and the hinges Gr at the sides being pivotally connected withrings H mounted to slide on the guide rods F. -Thus by the arrangement described the bags G can be readily inflated or deflated, and at the same time are thoroughly protected by the cover made of hinged sections. A pipe I connects with the bottom of each bag G and leads to a pump J driven from the motor D or operated by hand, and the pump J has a pipe connection K with one or a series of tanks L filled with a light gas, such as hydrogen gas, either manufactured by suitable apparatus located on the framework A or the tanks L are filled with gas prior to using the aeroplane for an ascent. By the arrangement described the pump J is used for pumping gas from the tanks L into the inflatable bags G, to inflate the same to any desired extent, that is, wholly, as shown to the left of Fig. 1, or partly, as indicated on the right of Fi 2. If it is desired to deflate the bags G, the pump J may be used for pumping the gas from.the bags G back into the tanks L, it being understood that for this purpose suitable valves are arranged on the pump for the purpose mentioned. It is also understood that the pump J may be in the form of an air pump for pumping air into the bags G instead of hydrogen gas to inflate the said bags or deflate the same, as the case may be.
By making the inflated bags in the form of bellows, a large sustaining surface is obtained, so as to insure stability of the aeroplane, and in case of accident to the motor to present sufficient resistance to the air to prevent rapid falling of the aeroplane, thus rendering the aeroplane exceed ngly safe.
Having thus described my invention, I claim as new and desire to secure by Letters Patent 1. An aeroplane, comprising a framework, spaced planes one above the other, guides between the said planes, and inflatable and deflatable-bags mounted on the said guides and formed bellows-like for extensible and contractible movement under the effect of inflation and deflation.
2. An aeroplane, comprising a framework, spaced planes one above the other,.gu1des between the said planes, inflatable and deflat-able bags mounted onthe said guides and formed to increase and decrease in length in a vertical direction under the effect of inflation, and deflation, gas supply tanks. on the said framework, and a pump on the framework and connected with the said bags 1:gnd the tanks for inflating and deflating the ags. I v a 3. An aeroplane, comprising a framework, sustaining planes one above the other and mounted on the said framework, guides on the said f amework, extensible and contractible bellows-like bags mounted on the said guides, and means under the control of the aviator for inflating or deflating the said bags, wholly or partly.; 4. An aeroplane, comprising'a framework, sustaining planes one above the other and mounted on the said framework, guides on the said framework,inflatable bags in the form of bellows and provided with a sheet metal cover made in sections hinged together, and rings slidable on the said guides and on which the hinged cover sections are pivoted, and means under the control of the aviatorfor inflating the bags.
5. An aeroplane provided with guides, and an inflatable b'agof bellows shape and .havinga cover formed of sheet metal sections hinged together, the cover sectionsoverlying the folds of the bag, and rings on able bag of bellows shape, and a metal cover for the same formed of plates overlying the folds of the bag and pivotally connected one with the other.
7. An aeroplane provided with an inflat-' able bag of bellows shape and a metal cover for the same formed of plates overlying the folds of the bag and pivotally connected one with the other, and guides for the said cover. 1
8. An aeroplane provided with sustaining planes, a framework, guides, extensible and contractible bellows-like bags mounted on the said guides, and means under the control of the aviator for filling-the said bags with a gas to extend the same or for discharging the gas from the bags to deflate thesame.
In testimony whereof I have signed my name to this specification in the presence of two subscribing witnesses.
MORRIS KALABA. Witnesses: f u
JAMES D. FERRIs,
THOMAS E. SHEEHAN'.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US62745011A US1012559A (en) | 1911-05-16 | 1911-05-16 | Aeroplane. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US62745011A US1012559A (en) | 1911-05-16 | 1911-05-16 | Aeroplane. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1012559A true US1012559A (en) | 1911-12-19 |
Family
ID=3080867
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US62745011A Expired - Lifetime US1012559A (en) | 1911-05-16 | 1911-05-16 | Aeroplane. |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1012559A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20060000945A1 (en) * | 2003-09-09 | 2006-01-05 | Voss Paul B | System and method for altitude control |
| US9540091B1 (en) | 2016-02-11 | 2017-01-10 | World View Enterprises Inc. | High altitude balloon systems and methods |
| US9561858B2 (en) | 2015-03-09 | 2017-02-07 | World View Enterprises Inc. | Rigidized assisted opening system for high altitude parafoils |
| US9694910B2 (en) | 2013-02-22 | 2017-07-04 | World View Enterprises Inc. | Near-space operation systems |
| US10124875B1 (en) | 2017-01-09 | 2018-11-13 | World View Enterprises Inc. | Continuous multi-chamber super pressure balloon |
| US10336432B1 (en) | 2017-01-09 | 2019-07-02 | World View Enterprises Inc. | Lighter than air balloon systems and methods |
| US20240217642A1 (en) * | 2021-04-08 | 2024-07-04 | Space Balloon Technologies Corp. | Apparatus, Method And System For Balloon Altitude Control By In-Situ Characterization And Active Energy Management |
| US12325504B2 (en) | 2022-11-07 | 2025-06-10 | World View Enterprises Inc. | Magnetic ballast dispenser |
-
1911
- 1911-05-16 US US62745011A patent/US1012559A/en not_active Expired - Lifetime
Cited By (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7469857B2 (en) * | 2003-09-09 | 2008-12-30 | University Of Massachusetts | System and method for altitude control |
| US20060000945A1 (en) * | 2003-09-09 | 2006-01-05 | Voss Paul B | System and method for altitude control |
| US9694910B2 (en) | 2013-02-22 | 2017-07-04 | World View Enterprises Inc. | Near-space operation systems |
| US12195189B2 (en) | 2013-02-22 | 2025-01-14 | World View Enterprises Inc. | Near-space operation systems |
| US11613364B2 (en) | 2013-02-22 | 2023-03-28 | World View Enterprises Inc. | Near-space operation systems |
| US10829229B2 (en) | 2013-02-22 | 2020-11-10 | World View Enterprises Inc. | Near-space operation systems |
| US11608181B2 (en) | 2015-03-09 | 2023-03-21 | World View Enterprises Inc. | Rigidized assisted opening system for high altitude parafoils |
| US9561858B2 (en) | 2015-03-09 | 2017-02-07 | World View Enterprises Inc. | Rigidized assisted opening system for high altitude parafoils |
| US10787268B2 (en) | 2015-03-09 | 2020-09-29 | World View Enterprises Inc. | Rigidized assisted opening system for high altitude parafoils |
| US9540091B1 (en) | 2016-02-11 | 2017-01-10 | World View Enterprises Inc. | High altitude balloon systems and methods |
| US12151800B2 (en) | 2016-02-11 | 2024-11-26 | World View Enterprises Inc. | High altitude balloon systems and methods |
| US10988227B2 (en) | 2016-02-11 | 2021-04-27 | World View Enterprises Inc. | High altitude balloon systems and methods using continuous multi-compartment super pressure balloon |
| US10336432B1 (en) | 2017-01-09 | 2019-07-02 | World View Enterprises Inc. | Lighter than air balloon systems and methods |
| US10124875B1 (en) | 2017-01-09 | 2018-11-13 | World View Enterprises Inc. | Continuous multi-chamber super pressure balloon |
| US11447226B1 (en) | 2017-01-09 | 2022-09-20 | World View Enterprises Inc. | Lighter than air balloon systems and methods |
| US10829192B1 (en) | 2017-01-09 | 2020-11-10 | World View Enterprises Inc. | Lighter than air balloon systems and methods |
| US11904999B2 (en) | 2017-01-09 | 2024-02-20 | World View Enterprises Inc. | Lighter than air balloon systems and methods |
| US12570389B2 (en) | 2017-01-09 | 2026-03-10 | World View Enterprises Inc. | Lighter than air balloon systems and methods |
| US10737754B1 (en) | 2017-01-09 | 2020-08-11 | World View Enterprises Inc. | Continuous multi-chamber super pressure balloon |
| US11511843B2 (en) | 2017-01-09 | 2022-11-29 | World View Enterprises Inc. | Lighter than air balloon systems and methods |
| US12214855B2 (en) | 2017-01-09 | 2025-02-04 | World View Enterprises Inc. | Lighter than air balloon systems and methods |
| US12312063B2 (en) * | 2021-04-08 | 2025-05-27 | Space Balloon Technologies Corp. | Apparatus, method and system for balloon altitude control by in-situ characterization and active energy management |
| US20250249997A1 (en) * | 2021-04-08 | 2025-08-07 | Space Balloon Technologies Corp. | Apparatus, Method And System For Balloon Altitude Control By In-Situ Characterization And Active Energy Management |
| US12559219B2 (en) * | 2021-04-08 | 2026-02-24 | Space Balloon Technologies Corp. | Apparatus, method and system for balloon altitude control by in-situ characterization and active energy management |
| US20240217642A1 (en) * | 2021-04-08 | 2024-07-04 | Space Balloon Technologies Corp. | Apparatus, Method And System For Balloon Altitude Control By In-Situ Characterization And Active Energy Management |
| US12325504B2 (en) | 2022-11-07 | 2025-06-10 | World View Enterprises Inc. | Magnetic ballast dispenser |
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