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US1350211A - Sea-dirigible - Google Patents

Sea-dirigible Download PDF

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Publication number
US1350211A
US1350211A US376782A US37678220A US1350211A US 1350211 A US1350211 A US 1350211A US 376782 A US376782 A US 376782A US 37678220 A US37678220 A US 37678220A US 1350211 A US1350211 A US 1350211A
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United States
Prior art keywords
water
bag
dirigible
tank
sea
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Expired - Lifetime
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US376782A
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Jr David Corson
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Individual
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Priority to US376782A priority Critical patent/US1350211A/en
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Publication of US1350211A publication Critical patent/US1350211A/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft
    • B64B1/005Arrangements for landing or taking-off, e.g. alighting gear

Definitions

  • This invention relates to air craft, particularly to those of the dirigible type, and has for its object the provision of a dirigible which is so constructed that it may land upon and also travel-upon water, in case of necessity, without danger.
  • An important object is the provisionof a device of this character formed as a dirigible provided at its ends with pontoons which extend laterally somewhat beyond the body of the dirigible to brace the same when it is floating so as to prevent it from being blown over, the body further carrying a boat-like structure disposed beneath its central portion and adapted to travel upon the water, this boat structure being formed to provide a water chamber into which water may be admitted at the will of the operator whereby to provide ballast for holding the diriglble down, pumps being provided for forcing out the-water when desired.
  • An additional object is the provision of a device of this character which will be simple in its operation, not complex in structure; eflicient in use, and a general improvement in the art.
  • Fig. 2 is an elevation of one end
  • Fig. 3 is an elevation of the other end
  • Fig. 4 is a longitudinal sectional view throughthe central portion of the device and showing the cabin and boat structure in section,
  • Fig. 5 is a'detail cross sectional view showing the means for controlling the inlet of water to the boat structure
  • Fig. 6 is a detail view illustrating one of the pumps for forcing out the water.
  • the numeral 10 designates the gas bag which is of any ordinary or preferred construction and which is of substantially cigar or torpedo shapela nd provided withany suit- Specification of Letters Patent.
  • the bag 10 is preferably reinforced with an aluminum shield 12 serving to protect the end in case the bag should strike the water nose first.
  • the bag is of course provided with the usual rudder 13 and elevation controls 14.
  • the cabin 15 Disposed beneath the bag 10 and suspended therefrom by any suitable structure, is the cabin 15 within which the operator and passengers are intended to remain and within which are disposed the various controls, I
  • propellers 16 are provided driven by any preferred or well known high power motors, not shown.
  • brace members Disposed at the front and rear ends of the bag 10 and extending therebelow are brace members. 17 carrying pontoons 18 formed referably as hollow aluminum shields.
  • hese pontoons and their supporting braces or frames are so arranged that they will extend laterally beyond the bag so that in case the device lights upon the water the pon-- toons will not only serve to support the bag to a certain extent but also act as braces to prevent it from being blown over.
  • a boat-like structure 20 Disposed beneath the cabin 15 and held rigidly associated with the bag 10, as by means of brace bars 19, is a boat-like structure 20 formed as a tank of suitable size and any preferred shape and constructed preferably of thin sheet metal.
  • This boat structure is designed to travel upon the surface of the water in case the dirigible alights at sea, and is provided at its forward end with a wave shield 21.
  • I provide the bottom of the tank 20 with an opening 21 surrounded by an inwardly extending flange 22 and the opening is formed with a valve seat 23.
  • a piston or valve 24 Movable vertically within the tank 20 is a piston or valve 24 adapted to engage the seat 23 and this valve is moved by means of a screw 25 carried .there'by and engaged by a rotatable hand wheel 26 mounted within the cabin 15 within convenient reach of the operator.
  • the screw 25 is threaded through the worm-wheel and is provided with means whereby to prevent it from rotary movement so that when the hand wheel 26 is turned in the proper direction the unseating the valve 24: and allowing water to flow in'through the opening 21.
  • an overflow opening or hole 27 At one end of the tank 20 at the desired maximum water level therein is provided an overflow opening or hole 27 which permits the exit of air as water is admitted through the opening 21 and which also serves as a Water overflow to prevent the water from rising be 0nd the maximum predetermined level.
  • I provide one or more force pumps 28 located within the tank, driven by anysuitable means, and discharging through outlet pipe 29.
  • a dirigible comprising in combination, a gas bag provided with driving means, rigid frames extending downwardly at the end portions of the bag and carrying hollow shells serving as pontoons, a tank supported beneath the bag-,- and adapted to serve as a boat structure, and means permitting inlet of water. into the tank whereby to serve as ballast.
  • a dirigible comprising in combination, a gas bag provided with driving means, rigid frames extending downwardly at the end portions of the bag and carrying hollow shells serving as pon- I toons, a tank supported beneaththe bag and adapted to serve as a boat structure, means permitting inlet of water into the tank whereby to serve as ballast, and means for expelling water from said tank.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Description

D. CORSON, JR.
SEA DIRIGlBLE.
APPLICATION FILED APR.2(1, I920.
Patented Aug. 17, 1920.
3 SHEETS--SHEET I.
INVENTOR A Q ww w w, s
2a w'd Goran/ed ATTORN EY D. CORSON, JR.
SEA DIRIGlBLE.
APPLICATION man APR.26, 1920.
1 ,350,2 1 1 te Aug. 17, 1920.
3 SHEET S-SHEEI 2 M Q "F" INVENTOR M A 1 Q/ I ITNESSES ATTORNEY UNITED STATES PATENT OFFICE.
DAVID COBSON, JR, MOUNT UNION, PENNSYLVANIA.
SEA-DIRIGIBLE.
v To all whom it may camera.-
Be it known that I, DAVID CoRsoN, Jr., a citizen of the United States, residing at Mount Union, in the county of Huntingdon and State of Pennsylvania, have invented new and useful Improvements in Sea'Dirigi ble, of which the following is a specification.
This invention relates to air craft, particularly to those of the dirigible type, and has for its object the provision of a dirigible which is so constructed that it may land upon and also travel-upon water, in case of necessity, without danger.
An important object is the provisionof a device of this character formed as a dirigible provided at its ends with pontoons which extend laterally somewhat beyond the body of the dirigible to brace the same when it is floating so as to prevent it from being blown over, the body further carrying a boat-like structure disposed beneath its central portion and adapted to travel upon the water, this boat structure being formed to provide a water chamber into which water may be admitted at the will of the operator whereby to provide ballast for holding the diriglble down, pumps being provided for forcing out the-water when desired. An additional object is the provision of a device of this character which will be simple in its operation, not complex in structure; eflicient in use, and a general improvement in the art.
With the above and other objects and advantages in view, the invention consists in the details of construction to be hereinafter more fully described and claimed, and illustrated in the accompanying drawings in which- Figure 1 is a side elevation of the device,
Fig. 2 is an elevation of one end,
Fig. 3 is an elevation of the other end,
Fig. 4 is a longitudinal sectional view throughthe central portion of the device and showing the cabin and boat structure in section,
Fig. 5 is a'detail cross sectional view showing the means for controlling the inlet of water to the boat structure, and
Fig. 6 is a detail view illustrating one of the pumps for forcing out the water.
Referring moreparticularly to the drawings, the numeral 10 designates the gas bag which is of any ordinary or preferred construction and which is of substantially cigar or torpedo shapela nd provided withany suit- Specification of Letters Patent.
Patented Aug. 17, 1920.
1920. Serial No. 376,782.
able or necessary longitudinal and transverse reinforcing ribs or stays 11. At one end the bag 10 is preferably reinforced with an aluminum shield 12 serving to protect the end in case the bag should strike the water nose first. The bag is of course provided with the usual rudder 13 and elevation controls 14.
Disposed beneath the bag 10 and suspended therefrom by any suitable structure, is the cabin 15 within which the operator and passengers are intended to remain and within which are disposed the various controls, I
' not shown, for operating the rudder and elevation control members. It is of course evident that suitable propellers 16 are provided driven by any preferred or well known high power motors, not shown.
Disposed at the front and rear ends of the bag 10 and extending therebelow are brace members. 17 carrying pontoons 18 formed referably as hollow aluminum shields.
hese pontoons and their supporting braces or frames are so arranged that they will extend laterally beyond the bag so that in case the device lights upon the water the pon-- toons will not only serve to support the bag to a certain extent but also act as braces to prevent it from being blown over.
Disposed beneath the cabin 15 and held rigidly associated with the bag 10, as by means of brace bars 19, is a boat-like structure 20 formed as a tank of suitable size and any preferred shape and constructed preferably of thin sheet metal. This boat structure is designed to travel upon the surface of the water in case the dirigible alights at sea, and is provided at its forward end with a wave shield 21. In order to provide means whereby to weight the device to prevent undesired rising from the surface of the water, I provide the bottom of the tank 20 with an opening 21 surrounded by an inwardly extending flange 22 and the opening is formed with a valve seat 23. Movable vertically within the tank 20 is a piston or valve 24 adapted to engage the seat 23 and this valve is moved by means of a screw 25 carried .there'by and engaged by a rotatable hand wheel 26 mounted within the cabin 15 within convenient reach of the operator. The screw 25 is threaded through the worm-wheel and is provided with means whereby to prevent it from rotary movement so that when the hand wheel 26 is turned in the proper direction the unseating the valve 24: and allowing water to flow in'through the opening 21. At one end of the tank 20 at the desired maximum water level therein is provided an overflow opening or hole 27 which permits the exit of air as water is admitted through the opening 21 and which also serves as a Water overflow to prevent the water from rising be 0nd the maximum predetermined level. 11 order to provide means whereby the water within the tank 20 may be expelled when it is desired to permit the device to rise, I provide one or more force pumps 28 located within the tank, driven by anysuitable means, and discharging through outlet pipe 29. I.
From the foregoing description and a study of the drawings it will be apparent that I have thus provided a simply constructed dirigible which may safely alight upon the. water and travel thereon, if desired, especially as means is provided for properly ballasting and also for bracing the device against lateral strain caused by wind.
While I have shown and described the preferred embodiment of my invention, it is of course to be understood that I reserve the right to make such changes in the form, construction, and arrangement of parts as will not depart from the spirit of the invention or the scope of the subjoined claims.
and carrying hollow shells serving as pontoons, and a tank supported beneath the bag and adapted to serve asa boat structure. i 2. In combination, a dirigible comprising in combination, a gas bag provided with driving means, rigid frames extending downwardly at the end portions of the bag and carrying hollow shells serving as pontoons, a tank supported beneath the bag-,- and adapted to serve as a boat structure, and means permitting inlet of water. into the tank whereby to serve as ballast.
3. In combination, a dirigible comprising in combination, a gas bag provided with driving means, rigid frames extending downwardly at the end portions of the bag and carrying hollow shells serving as pon- I toons, a tank supported beneaththe bag and adapted to serve as a boat structure, means permitting inlet of water into the tank whereby to serve as ballast, and means for expelling water from said tank.
In testimony whereof ll affix my signature.
DAVID CORSON, JR.
US376782A 1920-04-26 1920-04-26 Sea-dirigible Expired - Lifetime US1350211A (en)

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2951135A1 (en) * 2009-10-14 2011-04-15 Baptiste Regas AIRSHIP.
WO2012135117A3 (en) * 2011-03-31 2013-01-03 Lta Corporation Airship including aerodynamic, floatation, and deployable structures
US8616503B2 (en) 2007-08-09 2013-12-31 Lta Corporation Lenticular airship and associated controls
US8894002B2 (en) 2010-07-20 2014-11-25 Lta Corporation System and method for solar-powered airship
US9802690B2 (en) 2013-11-04 2017-10-31 Lta Corporation Cargo airship

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9840318B2 (en) 2007-08-09 2017-12-12 Pierre Balaskovic Lenticular airship and associated controls
US8616503B2 (en) 2007-08-09 2013-12-31 Lta Corporation Lenticular airship and associated controls
US9828082B2 (en) 2007-10-18 2017-11-28 Lta Corporation Airship having a cargo compartment
WO2011045529A1 (en) * 2009-10-14 2011-04-21 Baptiste Regas Airship
US20120199693A1 (en) * 2009-10-14 2012-08-09 A-NTE(Aero-Nautic Technology & Engineering) Airship
CN102753434A (en) * 2009-10-14 2012-10-24 航空工程技术公司 Airship
FR2951135A1 (en) * 2009-10-14 2011-04-15 Baptiste Regas AIRSHIP.
JP2013507293A (en) * 2009-10-14 2013-03-04 アー−エヌテエ(エアロ−ノーティック テクノロジー アンド エンジニアリング) airship
US8783603B2 (en) * 2009-10-14 2014-07-22 A-Nte (Aero-Nautic Technology & Engineering) Airship
AU2010306461B2 (en) * 2009-10-14 2016-05-19 A-Nte (Aero-Nautic Technology & Engineering) Airship
US8894002B2 (en) 2010-07-20 2014-11-25 Lta Corporation System and method for solar-powered airship
US8899514B2 (en) 2010-07-20 2014-12-02 Lta Corporation System and method for varying airship aerostatic buoyancy
WO2012135117A3 (en) * 2011-03-31 2013-01-03 Lta Corporation Airship including aerodynamic, floatation, and deployable structures
US9745042B2 (en) 2011-03-31 2017-08-29 Lta Corporation Airship including aerodynamic, floatation, and deployable structures
US8596571B2 (en) 2011-03-31 2013-12-03 Lta Corporation Airship including aerodynamic, floatation, and deployable structures
US9802690B2 (en) 2013-11-04 2017-10-31 Lta Corporation Cargo airship

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