US1364786A - Tank or receptacle for holding liquid fuel or other combustible liquids - Google Patents
Tank or receptacle for holding liquid fuel or other combustible liquids Download PDFInfo
- Publication number
- US1364786A US1364786A US306479A US30647919A US1364786A US 1364786 A US1364786 A US 1364786A US 306479 A US306479 A US 306479A US 30647919 A US30647919 A US 30647919A US 1364786 A US1364786 A US 1364786A
- Authority
- US
- United States
- Prior art keywords
- tank
- layers
- receptacle
- liquid fuel
- holding liquid
- 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
- 239000007788 liquid Substances 0.000 title description 7
- 239000000446 fuel Substances 0.000 title description 2
- 229920001971 elastomer Polymers 0.000 description 11
- 239000002184 metal Substances 0.000 description 11
- 239000004744 fabric Substances 0.000 description 9
- 238000010276 construction Methods 0.000 description 8
- 239000000463 material Substances 0.000 description 7
- PEDCQBHIVMGVHV-UHFFFAOYSA-N Glycerine Chemical compound OCC(O)CO PEDCQBHIVMGVHV-UHFFFAOYSA-N 0.000 description 4
- 239000011345 viscous material Substances 0.000 description 4
- 241000322338 Loeseliastrum Species 0.000 description 3
- 239000011120 plywood Substances 0.000 description 3
- 239000002131 composite material Substances 0.000 description 2
- 239000000945 filler Substances 0.000 description 2
- 235000011187 glycerol Nutrition 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 239000000344 soap Substances 0.000 description 2
- 240000008564 Boehmeria nivea Species 0.000 description 1
- 244000286663 Ficus elastica Species 0.000 description 1
- RRHGJUQNOFWUDK-UHFFFAOYSA-N Isoprene Chemical compound CC(=C)C=C RRHGJUQNOFWUDK-UHFFFAOYSA-N 0.000 description 1
- 238000007747 plating Methods 0.000 description 1
- 229920001195 polyisoprene Polymers 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
- B64D37/06—Constructional adaptations thereof
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S220/00—Receptacles
- Y10S220/90—Rupture proof
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/31504—Composite [nonstructural laminate]
- Y10T428/31678—Of metal
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/31504—Composite [nonstructural laminate]
- Y10T428/31678—Of metal
- Y10T428/31703—Next to cellulosic
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/31504—Composite [nonstructural laminate]
- Y10T428/31826—Of natural rubber
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T442/00—Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
- Y10T442/20—Coated or impregnated woven, knit, or nonwoven fabric which is not [a] associated with another preformed layer or fiber layer or, [b] with respect to woven and knit, characterized, respectively, by a particular or differential weave or knit, wherein the coating or impregnation is neither a foamed material nor a free metal or alloy layer
- Y10T442/2041—Two or more non-extruded coatings or impregnations
Definitions
- the object of the present invention is to improve the construction of such tanks orreceptacles in order to reduce to a minimum the liability for the tank to be completely pierced by a bullet or other projectile, to prevent the escape of liquid should the tank be pierced and to limit the size of opening pierced inthe tank by preventing the latter from being burst or seriously damaged by the pressure which is ordinarily set up when the tank is suddenly pierced.
- the invention consists in a tank or receptacle. for holding combustible or other liquids, the walls of which are formed from a combination of an inner metal lining and one or more layers of rubber or like material separated by or combined with one or more layers of fabric and inclosed between two or more layers of ply-wood, calico, canvas, felt, baize or the like.
- the invention also consists in an inner lining of the above character which is made of corrugated metal or material and has its corners rounded off, so as to allow for the ezrpansion which may take place owing to the pressure which is ordinarily set up when a tank or receptacle holding a liquid is suddenly pierced.
- the invention also consists in a tank or receptacle of the above character in which the rubber and fabric layers are covered or coated with soft soap, glycerin or any of the so-called anti-puncture compositions or tire fillers of commerce or other like viscous material.
- the invention also consists in a tank or receptacle .of the above kind in which the composite wall is completed by an outer layer of metal gauze, net or mesh, strong canvas, or
- Figure 1 is a perspective View of atank partly broken away and embodying the improved, wall construction.
- Fig. 2 is an enlarged section view taken through the wall
- Fig 3 is a similar view of a slightly modified orm of a wall construction.
- a petrol tank for use upon aeroplanes wherein the walls of the tank comprise an inner lining 1 ofsuitable metal of any convenient thickness; a layer 2 of canvas or 3-ply wood, felt, baize or the like adjacent to the inner lining, one or more layers 3 of india-rubber or similar sheet material arranged next to' the layer 2.
- these layers 3 there is arranged another layer 4 of canvas or 3-ply wood, calico, felt, baize or like material, and the whole is completed by an outer layer or'lining 5 of metal plating, open wire mesh, net gauze, strong canvas treated, if necessary, with rubber or a perforated metal plate, the layers being held in position by fianging the outer edge portions of the metal as shown at 6; by providing covering strips or the like, or by interlacing the gauze at'the meeting edges.
- rubber strips 7 for reinforcing purposes.
- the layers 3 are separated by or combined with layers 8 of soft calico, ramie cloth, or other similar fabric, and the rubber layers or the fabric layers are coated as at 9 with soft soap, glycerin orany of the so-called anti-puncture compositions ortire fillers of commerce, such as have been proposed in connection with pneumatic tires, or other similar viscous substance or material.
- a tank or receptacle constructed in. the manner above indicated possesses the very great r'actical advantages that it is much more di cult to pierce w1th a projectile than tanks or. receptacles of ordinary construction, while if itis pierced the inner linin oflers a minimum of resistance to the pro ectile andthe composite wall tends toclose up after piercing in order to prevent the escape of the liquid from the receptacle and, moreover, the material employed in the construction of the layers 3 will result in a considerable decrease in the area of the aperture made and the outer layer orlining will be found to prevent the tank, if pierced, from being seriously damaged by the pressure set up when a liquidcontaining receptacle is suddenly pierced.
- This latter feature constitutes an important advantage when a construction in accordance with my invention is employed for petrol tanks that may be released from an aeroplane, since owing to the absence of any tendency for the wall to spread upon being pierced it is possible to reduce very considerably the amount of inclination that must ordinarily be given to such releasable tanks, whereby the capacity of the tank may be very considerably increased.
- I may use fabric coated on one or both sides with rubber of any desired thickness.
- a tank for combustible or other liquids wherein the walls are composed of an inner metal lining, an outer metal covering, a plu-- rality of layers of rubber between the lining and covering, inner and outer fabric layers intimately contacting with the outer surface of the rubber layers and contacted by' the metal lining and covering, a plurality' of fabric layers separating the rubber layers, and thefabric layers and the rubber layers being coated with a viscous material.
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Processing Of Solid Wastes (AREA)
Description
S E. NEAL. TANK 0R RECEPTACLE FOR HOLDING LIQUID FUEL OR OTHER COMBUSTIBLE LIQUIDS.
APPLICATION FILED JUNE 24,19I9.
Patented Jan. 4, 1921.
at touwg UNITED STATES PATENT OFFICE.
SAMUEL ERIC NEAL, OF LONDON, ENGLAND.
TANK OR REGEPTACLE'FOR HOLDING LIQUID FUEL OR OTHER COMBUSTIBLE LIQUIDS.
Patented Jan. 4, 1921.
Application filed June 24, 1919. Serial No. 306,479.
To all whom it may concern:
Be it known that I, SAMUEL ERIC NEAL, a
subject of the King of Great Britain and. at 34: Homefield road,- 4., England, have intacles for holdin -li uid fuel or other combustible or other iquids and especially designed for use in the construction of petrol tanks that are to be carried upon aeroplanes or which are located in other situations Where they are liable to be pierced by bullets or incendiary or-other projectiles.
The object of the present invention is to improve the construction of such tanks orreceptacles in order to reduce to a minimum the liability for the tank to be completely pierced by a bullet or other projectile, to prevent the escape of liquid should the tank be pierced and to limit the size of opening pierced inthe tank by preventing the latter from being burst or seriously damaged by the pressure which is ordinarily set up when the tank is suddenly pierced.
The invention consists in a tank or receptacle. for holding combustible or other liquids, the walls of which are formed from a combination of an inner metal lining and one or more layers of rubber or like material separated by or combined with one or more layers of fabric and inclosed between two or more layers of ply-wood, calico, canvas, felt, baize or the like.
The invention also consists in an inner lining of the above character which is made of corrugated metal or material and has its corners rounded off, so as to allow for the ezrpansion which may take place owing to the pressure which is ordinarily set up when a tank or receptacle holding a liquid is suddenly pierced.
The invention also consists in a tank or receptacle of the above character in which the rubber and fabric layers are covered or coated with soft soap, glycerin or any of the so-called anti-puncture compositions or tire fillers of commerce or other like viscous material.
The invention also consists in a tank or receptacle .of the above kind in which the composite wall is completed by an outer layer of metal gauze, net or mesh, strong canvas, or
by an outer'perforated or corrugated metal plate.-
The accompanying drawings illustrate various improvements in accordance withthe invention.
Figure 1 is a perspective View of atank partly broken away and embodying the improved, wall construction.
Fig. 2 is an enlarged section view taken through the wall, and
Fig 3 is a similar view of a slightly modified orm of a wall construction.
Referring now more particularly to the drawing there is provided a petrol tank for use upon aeroplanes wherein the walls of the tank comprise an inner lining 1 ofsuitable metal of any convenient thickness; a layer 2 of canvas or 3-ply wood, felt, baize or the like adjacent to the inner lining, one or more layers 3 of india-rubber or similar sheet material arranged next to' the layer 2. On the other side of these layers 3 there is arranged another layer 4 of canvas or 3-ply wood, calico, felt, baize or like material, and the whole is completed by an outer layer or'lining 5 of metal plating, open wire mesh, net gauze, strong canvas treated, if necessary, with rubber or a perforated metal plate, the layers being held in position by fianging the outer edge portions of the metal as shown at 6; by providing covering strips or the like, or by interlacing the gauze at'the meeting edges. At the corners of the tank and between the outer layers 3are arranged rubber strips 7 for reinforcing purposes.
As shown in Fi 3, the layers 3 are separated by or combined with layers 8 of soft calico, ramie cloth, or other similar fabric, and the rubber layers or the fabric layers are coated as at 9 with soft soap, glycerin orany of the so-called anti-puncture compositions ortire fillers of commerce, such as have been proposed in connection with pneumatic tires, or other similar viscous substance or material.
It-will be found that a tank or receptacle constructed in. the manner above indicated possesses the very great r'actical advantages that it is much more di cult to pierce w1th a projectile than tanks or. receptacles of ordinary construction, while if itis pierced the inner linin oflers a minimum of resistance to the pro ectile andthe composite wall tends toclose up after piercing in order to prevent the escape of the liquid from the receptacle and, moreover, the material employed in the construction of the layers 3 will result in a considerable decrease in the area of the aperture made and the outer layer orlining will be found to prevent the tank, if pierced, from being seriously damaged by the pressure set up when a liquidcontaining receptacle is suddenly pierced.
This latter feature constitutes an important advantage when a construction in accordance with my invention is employed for petrol tanks that may be released from an aeroplane, since owing to the absence of any tendency for the wall to spread upon being pierced it is possible to reduce very considerably the amount of inclination that must ordinarily be given to such releasable tanks, whereby the capacity of the tank may be very considerably increased.
In place of using the fabric and rubber as separate layers, I may use fabric coated on one or both sides with rubber of any desired thickness.
It is to be understood that the foregoing details of construction are given by way of example only, as I may modify the number of layers of the various materials employed, the quality and texture of the materials and the manner in which the layers are arranged relatively -to one another, in any manner that may" be found to give most satisfactory results in practice.
Having now described my invention, what I claim as new and desire to secure by Letters Patent is A tank for combustible or other liquids wherein the walls are composed of an inner metal lining, an outer metal covering, a plu-- rality of layers of rubber between the lining and covering, inner and outer fabric layers intimately contacting with the outer surface of the rubber layers and contacted by' the metal lining and covering, a plurality' of fabric layers separating the rubber layers, and thefabric layers and the rubber layers being coated with a viscous material.
In testimony whereof I have signed my name to this specification.
SAMUEL ERIC NEAL.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US306479A US1364786A (en) | 1919-06-24 | 1919-06-24 | Tank or receptacle for holding liquid fuel or other combustible liquids |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US306479A US1364786A (en) | 1919-06-24 | 1919-06-24 | Tank or receptacle for holding liquid fuel or other combustible liquids |
Publications (1)
Publication Number | Publication Date |
---|---|
US1364786A true US1364786A (en) | 1921-01-04 |
Family
ID=23185487
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US306479A Expired - Lifetime US1364786A (en) | 1919-06-24 | 1919-06-24 | Tank or receptacle for holding liquid fuel or other combustible liquids |
Country Status (1)
Country | Link |
---|---|
US (1) | US1364786A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2442983A (en) * | 1942-08-14 | 1948-06-08 | Baxter Laboratories Inc | Closure |
FR2459956A1 (en) * | 1979-06-26 | 1981-01-16 | Cristiani Jacques | Ballistic screens partic. for bulletproof sheeting for car body mfr. - incorporates laminate of fibrous materials combined with metal sheet, light in wt. and thin |
US20060186129A1 (en) * | 2005-02-23 | 2006-08-24 | Allnutt Elena G | Reusable sleeve for a beverage container |
US8561829B1 (en) * | 2009-10-23 | 2013-10-22 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Composite pressure vessel including crack arresting barrier |
-
1919
- 1919-06-24 US US306479A patent/US1364786A/en not_active Expired - Lifetime
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2442983A (en) * | 1942-08-14 | 1948-06-08 | Baxter Laboratories Inc | Closure |
FR2459956A1 (en) * | 1979-06-26 | 1981-01-16 | Cristiani Jacques | Ballistic screens partic. for bulletproof sheeting for car body mfr. - incorporates laminate of fibrous materials combined with metal sheet, light in wt. and thin |
US20060186129A1 (en) * | 2005-02-23 | 2006-08-24 | Allnutt Elena G | Reusable sleeve for a beverage container |
US8561829B1 (en) * | 2009-10-23 | 2013-10-22 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Composite pressure vessel including crack arresting barrier |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4336291A (en) | Flexible self-sealing wall member | |
US2421613A (en) | Plastic liner for containers | |
US1364786A (en) | Tank or receptacle for holding liquid fuel or other combustible liquids | |
DE1101463B (en) | Large capacity container for storing or transporting liquefied hydrocarbon gases at around atmospheric pressure | |
US2438965A (en) | Self-sealing fuel tank | |
US2446815A (en) | Self-sealing fuel tank construction | |
US2461096A (en) | Self-sealing gasoline tank | |
US1381175A (en) | Antiexplosive and non-inflammable gasolene-tank | |
US2657884A (en) | Fuel cell | |
ES2680350T3 (en) | Wheel made of cardboard | |
US4401140A (en) | Filler valve for valve bag | |
US2401627A (en) | Puncture sealing gas tank | |
US2381739A (en) | Hidden barrier | |
US2933214A (en) | Pressure vessel | |
US2381402A (en) | Droppable fuel tank | |
US2547146A (en) | Hollow pontoon structure and method of making the same | |
US1392892A (en) | Tank or receptacle for combustible or other liquids | |
US1448180A (en) | Composite laminated structure | |
US5031558A (en) | Liquid cargo tanker | |
USRE19494E (en) | Compound ventilated fabric and method of making same | |
US2278733A (en) | Sound deadener | |
US2381400A (en) | Fuel tank | |
US3304900A (en) | Aircraft float | |
US1510133A (en) | Protecting device for fuel tanks | |
US2415032A (en) | Manufacture of fuel tanks |