US2407515A - Self-sealing tank - Google Patents
Self-sealing tank Download PDFInfo
- Publication number
- US2407515A US2407515A US360396A US36039640A US2407515A US 2407515 A US2407515 A US 2407515A US 360396 A US360396 A US 360396A US 36039640 A US36039640 A US 36039640A US 2407515 A US2407515 A US 2407515A
- Authority
- US
- United States
- Prior art keywords
- rubber
- closed cell
- tank
- gas
- sheet
- 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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Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
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- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/912—Puncture healing layer
-
- 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
- Y10T428/23—Sheet including cover or casing
- Y10T428/231—Filled with gas other than air; or under vacuum
-
- 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
- Y10T428/23—Sheet including cover or casing
- Y10T428/239—Complete cover or casing
-
- 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
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249953—Composite having voids in a component [e.g., porous, cellular, etc.]
- Y10T428/249976—Voids specified as closed
-
- 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
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249953—Composite having voids in a component [e.g., porous, cellular, etc.]
- Y10T428/249987—With nonvoid component of specified composition
- Y10T428/24999—Inorganic
Description
Sept. 10, 1946.
D. ROBERTS SELF-SEALING TANK Filed Oct. 9. 1940 INVENTOR "F3 a a a i M m m .N J mm, 2 M H Patented Sept. 10, 1946 SELF-SEALING TANK Dudley Roberts, deceased, late of New York, N. Y.,
. by Dudley Roberts, Jr.,
to Rubatex Products, Inc., New
N. Y., assignor executor, New York,
York, N. Y., a corporation of Delaware Application October 9, 1940, Serial No. 360,396
The invention relates to a novel construction for protecting and sealing fuel tanks against bullet or shell fire and more particularly the invention relates to a self-sealing gasoline tank to protect said tank and prevent leakage therefrom in the event of penetration by bullet or shell fragment.
In military and in naval airplanes the gasoline tank represents one of the most vulnerable points for disabling .and destroying a plane. It is preeminently'desirable that such .gasoline tanks be protected against penetration by anti-aircraft shell fragments and, if such "penetration does re sult, that the .gasoline therein be prevented from flowing .out from the pierced tank so as to prevent the possibility of fire developing.
A novel construction by means of which gasoline tanks are protected by covering the tank with closed cell gas expanded rubber of a flexible and resilient nature. It is a particular feature of the invention that such flexible and resilient closed cell gas expanded rubber be placed over the fuel tank and confined so as to be maintained under compression. The compression referred to is primarily in a direction in the plane of the resilient closed 'cell rubber but also in the direction normal thereto tending to compress the resilient closed cell rubber in the plane of its largest dimensions. By means of this covering comprising a compressed sheet of closed cell gas expanded rubber, it has been found that greatly increased protectionis afforded. In the first place, the resilient closed cell rubber is flexible and absorbent of blows and hence when surrounded by a hard and tough shell-like cover, glancing blows of shell fragments can be rendered innocuous inasmuch as closed cell rubber has a great elasticity and recedes or gives with the blow.
A further and more important feature of the invention lies in the fact that when a direct hit is scored and a bullet or shell fragment has impacted against the covering with suflicient force to penetrate the same and pierce through into the gasoline tank, because of the nature of the covering provided gasoline is prevented from flowing out in substantial quantity and accordingly the damage of fire and loss of fuel is diminished. More specifically upon the covered tank being pierced by a bullet or shell fragment, the pierced soft and. resilient closed cell gas expanded rubber, because of the inwardly directed compressive force thereupon, tends to move to fill up the space torn away by the bullet or shell fragment and cause a physical seal- 4 Claims. 7 (Cl. 154-435) ing or blocking action to take place. The slight leakage of gasoline into and through this breach exerts a sealing action thereon so that little flow of'gasoline to the outside is possible.
Accordingly, it is the object of the invention to provide a novel construction of fuel tanks.
It is a further object .of the invention to provide a novel construction whereby a self-sealing effect is obtained upon penetration of the cover and gasoline tank by a bullet or shell fragment.
It is a further object of the invention to provide novel method for resiliently resisting glancing impacts of bullets or shell fragments.
It is a further object of the invention to provide a covering for a fuel tank comprising a sheet of soft and resilient closed cell gas expanded rubber maintained under a compressive force, compression being directed inwardly in the plane of the sheet .of closed cell rubber.
These and'fnr ther objects of the invention will be apparent from a consideration of the description which follows taken in connection with the drawing, in which Figure 1 is a cross-section of the construction of the invention in which closed cell rubber is disposed over a gas tank.
Figure 2 is a cross section of a gas tank of the invention in which the closed cell rubber dis- 3 posed over the gas tank is compressed and guarded by a suitable shell-like cover.
Figure 3 is a cross section taken along line 3-3 of Figure 1.
Figure 4 is a 4-4 of Figure 2.
Figure 5 is a side elevation of the construction of the invention showing a compressing network superimposed over the closed cell rubber disposed on a gas tank.
Referring now more specifically to the ing:
In Figure 1 is shown a gasoline tank comprising a side wall, l0, and an endpiece, II, and dis posed over this gas tank is closed cell gas expanded rubber, l2 and I3. This closed cell gas expanded rubber is formed by injecting nitrogen gas under pressure in the order of three thousand pounds per square inch into rubber, and so treating the rubber as by partial vulcanization, so that the gas is entrapped in the rubber in the form of closed cells. Closed cell rubber may also be formed by mixing with the rubber suitable chemicals adapted to compose and develop nitrogen gas under heat. Methods of forming closed cell rubber are more fully set forth in Patent No.
drawfor the protection.
cross section taken along line 3 2,086,513, issued July 6, 1937, and application Serial No. 159,706, filed August 18, 1937.
The closed cell rubber, i2 and I3, is disposed over a gas tank to which it may be suitably secured as by means of adhesive areas, although to obtain free movement of the closed cell rubber, it is preferable that no adhesive be employed between the closed cell rubber and the tanks surface. Over the sheet, I2, of closed cell gas expanded rubber, there is placed a compressive spring-like member, I5, which is tightened so as to compress the closed cell rubber in a direction normal to the plane of the sheet. Over this compressing spring member is disposed a hard shell-like member, I 6, which may for example be armor plate or some suitable metal.
In order to provide desirable inward-compression an end member, I8, is found disposed over the end sheet, I3, so as to compress the same which moves against the end of the sheet, I2, causing that to be inwardly compressed. This end member, I8, is also formed of a shock-resistant hard armor plate, and hence, a full superficial protection against glancing blows of projectiles or shell fragments is aiforded. Because the closed cell rubber sheet, I 2, is compressed both downwardly and inwardly, it is well adapted to recede and give with any blows directed thereto, and in case of a direct hit secured by a projectile with sufiicient force to pass through the armor plate, I 6, the closed cell rubber, I2, and the gas tank wall, l, then the closed cell rubber, I2, under compression tends to move inwardly to close .the openings formed by the projectile. Thus a physical self-sealing action is effected. Similarly, since the gasoline exerts a solvent or flowing action on the torn portion of the closed cell rubber it tends to seal the opening formed therein.
In Figures 3 and 4 are shown cross sections based upon Figures 1 and 2, as indicated, and in these Figures 3 and 4. is indicated the relative compression and means of compression for the closed cell rubber.
Closed cell rubber contains enclosed cells of gas, homogeneously distributed throughout its mass, and when compressed, these cells are also compressed but not ruptured. Closed cell rubber is impervious to the flow of liquids, extremely resilient and. at the same time light in weight because of the presence of the gas therein.
Various modifications in the invention may be employed, but of primary importance is the fact that the closed cell gas expanded rubber is employed as a shield by the gas tank and that there may be exerted such compression on this closed cell rubber so that it has increased resilience to shock, and upon displacement of a material portion therein, will move to fill up the displaced portion. Compression of the closed cell rubber is inwardly in the plane of the rub ber, and an additional downward compression may or may not be employed.
Additionally, the armor plate to repel glancing blows is disposed as a shell-like exterior in the construction.
Althoughit' has been found that rubber is most suitable in the closed cell gas expanded material, it is in the purview of the invention to use combinations of rubber or substitute other elastic materials for the rubber base.
It is claimed:
1. A tank and a layer of closed cell gas expanded rubber positioned over said tank, means for inwardly compressing said closed cell rubber in the plane of said layer of closed cell rubber,
and a shock resistant protective layer positionedover said closed cell rubber.
2. A tank and a layer of closed cell gas expanded rubber positioned over said tank, means for inwardly and downwardly compressing said closed 'cell rubber in the plane of said layer of closed cell rubber, and a shock resistant protective layer positioned over said closed cell rubber.
3. In combination with a tank, a sealed cellular gas expanded rubber sheet covering said tank surface, said rubber being mounted to permit freedom of movement of said cellular structure, a compressive spring-like means for maintaining said rubber under compression in a direction normal to the plane of said rubber sheet, and a hard shell-like member disposed over said springlike member.
4. In combination with a tank, a sealed cellular gas expanded rubber sheet covering said tank surface, said rubber being mounted to permit freedom of movement of said cellular structure, a compressive spring-like means for maintaining said rubber under compression in a direction normal to the plane of said rub-ber sheet, a hard shell-like member disposed over said spring-like member, and end members disposed'over the ends of said sheet for pressing said rubber inwardly.
DUDLEY ROBERTS, J R.,
Executor of the Last Will and Testament of Dudley Roberts, Deceas d.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US360396A US2407515A (en) | 1940-10-09 | 1940-10-09 | Self-sealing tank |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US360396A US2407515A (en) | 1940-10-09 | 1940-10-09 | Self-sealing tank |
Publications (1)
Publication Number | Publication Date |
---|---|
US2407515A true US2407515A (en) | 1946-09-10 |
Family
ID=23417791
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US360396A Expired - Lifetime US2407515A (en) | 1940-10-09 | 1940-10-09 | Self-sealing tank |
Country Status (1)
Country | Link |
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US (1) | US2407515A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2531159A (en) * | 1948-04-15 | 1950-11-21 | William G Rowell | System for burner cutoff and signaling means upon tank leakage |
US2757242A (en) * | 1950-03-06 | 1956-07-31 | Richard H Ranger | Magnetic sound recording and reproducing apparatus |
US4216803A (en) * | 1976-06-15 | 1980-08-12 | Martin Marietta Corporation | Self-sealing fuel lines |
US4294279A (en) * | 1978-05-31 | 1981-10-13 | The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland | Fuel tanks |
US4432515A (en) * | 1981-03-12 | 1984-02-21 | Valmet Oy | Liquid fuel tank for an airplane and method and apparatus for manufacturing the same |
US4664982A (en) * | 1983-07-15 | 1987-05-12 | American Standard Inc. | Multi-layer composite structure |
US20080264951A1 (en) * | 2007-04-26 | 2008-10-30 | The Boeing Company | Sealing bladderless system and method |
WO2012166494A1 (en) | 2011-05-27 | 2012-12-06 | Hutchinson S.A. | Self-sealing liquid containment system and method of installing same |
-
1940
- 1940-10-09 US US360396A patent/US2407515A/en not_active Expired - Lifetime
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2531159A (en) * | 1948-04-15 | 1950-11-21 | William G Rowell | System for burner cutoff and signaling means upon tank leakage |
US2757242A (en) * | 1950-03-06 | 1956-07-31 | Richard H Ranger | Magnetic sound recording and reproducing apparatus |
US4216803A (en) * | 1976-06-15 | 1980-08-12 | Martin Marietta Corporation | Self-sealing fuel lines |
US4294279A (en) * | 1978-05-31 | 1981-10-13 | The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland | Fuel tanks |
US4432515A (en) * | 1981-03-12 | 1984-02-21 | Valmet Oy | Liquid fuel tank for an airplane and method and apparatus for manufacturing the same |
US4664982A (en) * | 1983-07-15 | 1987-05-12 | American Standard Inc. | Multi-layer composite structure |
US20080264951A1 (en) * | 2007-04-26 | 2008-10-30 | The Boeing Company | Sealing bladderless system and method |
WO2008134161A1 (en) * | 2007-04-26 | 2008-11-06 | The Boeing Company | Sealing bladderless system and method |
US7900333B2 (en) * | 2007-04-26 | 2011-03-08 | The Boeing Company | Sealing bladderless system and method |
US20110155741A1 (en) * | 2007-04-26 | 2011-06-30 | The Boeing Company | Sealing bladderless system and method |
US8505761B2 (en) * | 2007-04-26 | 2013-08-13 | The Boeing Company | Sealing bladderless system and method |
WO2012166494A1 (en) | 2011-05-27 | 2012-12-06 | Hutchinson S.A. | Self-sealing liquid containment system and method of installing same |
EP2715211A4 (en) * | 2011-05-27 | 2015-05-20 | Hutchinson Sa | Self-sealing liquid containment system and method of installing same |
US11168962B2 (en) | 2011-05-27 | 2021-11-09 | Hutchinson S.A. | Self-sealing liquid containment system and method of installing same |
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