US1591618A - Crashproof fuel tank - Google Patents
Crashproof fuel tank Download PDFInfo
- Publication number
- US1591618A US1591618A US606872A US60687222A US1591618A US 1591618 A US1591618 A US 1591618A US 606872 A US606872 A US 606872A US 60687222 A US60687222 A US 60687222A US 1591618 A US1591618 A US 1591618A
- Authority
- US
- United States
- Prior art keywords
- fuel
- tank
- fuel tank
- reservoirs
- cells
- 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
- 239000002828 fuel tank Substances 0.000 title description 10
- 210000004027 cell Anatomy 0.000 description 15
- 230000001413 cellular effect Effects 0.000 description 11
- 239000000446 fuel Substances 0.000 description 11
- 239000012530 fluid Substances 0.000 description 6
- 239000002184 metal Substances 0.000 description 4
- 238000010276 construction Methods 0.000 description 3
- 238000007789 sealing Methods 0.000 description 3
- 230000001066 destructive effect Effects 0.000 description 2
- 210000002421 cell wall Anatomy 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 210000003141 lower extremity Anatomy 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- AHLBNYSZXLDEJQ-FWEHEUNISA-N orlistat Chemical compound CCCCCCCCCCC[C@H](OC(=O)[C@H](CC(C)C)NC=O)C[C@@H]1OC(=O)[C@H]1CCCCCC AHLBNYSZXLDEJQ-FWEHEUNISA-N 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 210000001364 upper extremity Anatomy 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
- B64D37/08—Internal partitioning
-
- 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
Definitions
- This invention relates to fuel tanks in general and more particularly to a tank which is so designed as to greatly resist rupture under shock or pressure and if ruptured to permit a minimum of fuel leakage therefrom.
- FIG. 1 is a top plan view ofmy device with the upper outer wall removed.
- Fig. 2 is an end view of the same partly in section showing in dotted lines the central reservoir and the cell end closures.
- Fig. 3 is a view of one of the cell forminv sheets.
- Fig. 4 shows the cap for sealing the ends of the cells.
- Fig. 5 shows a detail of the method of joining the cells together.
- my device is constructed as follows.
- a plurality of formed metal sheets l such as is shown in detail in Fig. 3. These metal sheets are secured to the side walls by any suitable means such as rivets 9 and fluid tight connections made therewith.
- the sheets are assembled in the tank by placing each formed sheet on its predecessor with its formed surface reversed so that a plurality of hexagonal cells as shown in Fig. l will be formed. These sheets may be secured to each other and to rods 2 which extend throughout the length of the sheets, or may be merely held in place by the tight fit between the sheets and the rods.
- the hexagonal cells are sealed at their upper ends by means of suitable caps 8 as shown in Fig. 4, similar sealing caps being also provided for the lower ends of the cells.
- suitable caps 8 as shown in Fig. 4, similar sealing caps being also provided for the lower ends of the cells.
- One hole 13 as shown in Fig. 4 is provided inuthe sealing caps for the lower endsof the ce s.
- a main fuel reservoir or well 6 is located at approximately the center of the tank and is suitably provided with rivets for securing it to its adjacent metal sheet ends.
- a suitable drain or outlet lO is provided for the tank at the base of this well and a suitable filler openingll is also provided for filling the tank.
- a small. opening l2 is provided near the base of each cell to connect it to its neighboring cell and to other cells, and thence to the central reservoir.
- a set of air openings 13 is provided for ingress of air to permit the egress of the fuel.
- the cells thus constructed lend great structural strength to t-he whole tank assembly and rende-r a crashing of the tank unlikely. Further, the cells are of such small cross sectional area as to prevent the building up of a destructivo pressure wave in the fuel contained therein,
- a reservoir a plurality ol I claimz-f- 1.
- a Centrally located main reservoir for initially receiving said fuel
- a plurality of cellular reservoirs mounted Conoentrieally about said main reservoir and Within said casing7 apertures in the Walls ot said reservoirs allowing distribution of said -fuel 'from Said main to said cellular reservoirs and allowing interdistribution among Said cellular reservoirs.
- a casing a oentralliv located cylindrical main reservoir, a plurality oi cellular reservoirs mounted oonoentricallj,1 about Said main reeervoirand within said casing, each ot said Cellular reservoirs being connected at ite4 upper and lower extremitj7 to said easing, apertures arranged in the Walls of said reservoirs allowing distribution of Said fluid fuel from said main to said cellular reservoirs and allowing interdistribution among ⁇ said Cellular reeervoirs7 the latter being provided with additional apertures 'for tlie admission of air for pressure preeautional purposes.
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Description
' July 6 1926.
v A. C. FouLK cRAsHPRooF FUEL TANK Filed nec. 14, 1922` 2 sheets-shut 2 Iliff!! A` -y awww www! I .l y dummy Patente-d July 6, P*1926.
UNITED STATES ALBERT C. FOULK, OF I-IOLTON, KANSAS.
CRASI-IPROOF FUEL TANK.
Application :filed December 14, 1922.
This invention relates to fuel tanks in general and more particularly to a tank which is so designed as to greatly resist rupture under shock or pressure and if ruptured to permit a minimum of fuel leakage therefrom.
The necessity for the use of such a tank as is above described for fire prevention in motor vehicles and particularly in aircraft is so well known that its various applications need not be dealt with in detail.
It is an object of my invention to provide a. fuel tank internally braced in such a manner as to make it almost crash-proof in all but extraordinarily severe accidents.
It is a further object of my invention to provide a tank in which a main reservoir is surrounded by a plurality of smaller reservoirs so that in case of an accident which is severe enough to crash the outer walls of the tank only that fuel will escape rapidly which was in the smaller reservoir thus broken.
It is a further object of my structure as discussed in the preceding paragraph to diminish the destructive effect of a bullet passing through such a tank. In a fuel tank of the usual construction the hole caused by the entrance is usually a small one while the hole caused by its exit is much larger due, principally, to the pressure wave built up in the liquid fuel due to the passage of the bullet therethrough. By my construction, as will. be readily seen, each of the small reservoirs is of such narrow cross section that it would be possible for the bullet in its passage to build up a compression wave of any great or destructive magnitude.
Other objects of my invention will appear as the accompanying specification progresses and my device will be illustrated in the accompanying drawings in which Fig. 1 is a top plan view ofmy device with the upper outer wall removed.
Fig. 2 is an end view of the same partly in section showing in dotted lines the central reservoir and the cell end closures.
Fig. 3 is a view of one of the cell forminv sheets.
Fig. 4 shows the cap for sealing the ends of the cells.
Fig. 5 shows a detail of the method of joining the cells together.
Referring with greater particularty to the drawings, it will e noted that my device is constructed as follows.
serial No. 606,872.
Mounted upon and extending between side walls A and B are a plurality of formed metal sheets l such as is shown in detail in Fig. 3. These metal sheets are secured to the side walls by any suitable means such as rivets 9 and fluid tight connections made therewith.
The sheets are assembled in the tank by placing each formed sheet on its predecessor with its formed surface reversed so that a plurality of hexagonal cells as shown in Fig. l will be formed. These sheets may be secured to each other and to rods 2 which extend throughout the length of the sheets, or may be merely held in place by the tight fit between the sheets and the rods.
The hexagonal cells are sealed at their upper ends by means of suitable caps 8 as shown in Fig. 4, similar sealing caps being also provided for the lower ends of the cells. One hole 13 as shown in Fig. 4 is provided inuthe sealing caps for the lower endsof the ce s.
A main fuel reservoir or well 6 is located at approximately the center of the tank and is suitably provided with rivets for securing it to its adjacent metal sheet ends.
A suitable drain or outlet lO is provided for the tank at the base of this well and a suitable filler openingll is also provided for filling the tank.
A small. opening l2 is provided near the base of each cell to connect it to its neighboring cell and to other cells, and thence to the central reservoir. A set of air openings 13 is provided for ingress of air to permit the egress of the fuel.
From the foregoing it will be seen that a blow of such strength as to fracture one of the cell walls will only permit egress of fuel from that relatively small fracture plus the relatively slow egress of fuel from other cells leading through the very small openings in the bases of the cells.
The cells thus constructed lend great structural strength to t-he whole tank assembly and rende-r a crashing of the tank unlikely. Further, the cells are of such small cross sectional area as to prevent the building up of a destructivo pressure wave in the fuel contained therein,
I do not wish to limit my invention to the specific embodimentv shown in this s ecification. but contend that it is entitle to all the broad applications of the principles ins veived.
reservoir, a plurality ol I claimz-f- 1. In combination, in a fluid fuel tank, a easing, a Centrally located main reservoir for initially receiving said fuel, a plurality of cellular reservoirs mounted Conoentrieally about said main reservoir and Within said casing7 apertures in the Walls ot said reservoirs allowing distribution of said -fuel 'from Said main to said cellular reservoirs and allowing interdistribution among Said cellular reservoirs.
Q. In Combination, in a fluid fuel tank, a easing, a centrally located cylindrical `main c Cellular reservoirs mounted concentricall;vv about Said main reservoir end Within said seeing, each oi said cellular reservoirs being connected at its upper and lower extremity to said easing, apertures `arranged in the Walls of said reservoirs rallowing distribution ot said fluid -uel from said main to said cellular reservoirs and allowing interdistribution among said cellular reservoirs.
3. In combination, 1n a fluid fuel tank,
a casing, a oentralliv located cylindrical main reservoir, a plurality oi cellular reservoirs mounted oonoentricallj,1 about Said main reeervoirand within said casing, each ot said Cellular reservoirs being connected at ite4 upper and lower extremitj7 to said easing, apertures arranged in the Walls of said reservoirs allowing distribution of Said fluid fuel from said main to said cellular reservoirs and allowing interdistribution among` said Cellular reeervoirs7 the latter being provided with additional apertures 'for tlie admission of air for pressure preeautional purposes.
4. In Combination in a fuel tank Casing;7 a Central reservoir mounted in Said Casing, a
,plurality oit rods attached to the ends of said easing, and a nuinber of Sheets of iornied metal of generally corruguted construction having a series of depressione to receive part oi said rods, Said rods and Sheets forming tubular cells entending substantially `the tull length of Said easing. i
In testimony whereof I alli): my signature.
ALBERT C. FOULK.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US606872A US1591618A (en) | 1922-12-14 | 1922-12-14 | Crashproof fuel tank |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US606872A US1591618A (en) | 1922-12-14 | 1922-12-14 | Crashproof fuel tank |
Publications (1)
Publication Number | Publication Date |
---|---|
US1591618A true US1591618A (en) | 1926-07-06 |
Family
ID=24429825
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US606872A Expired - Lifetime US1591618A (en) | 1922-12-14 | 1922-12-14 | Crashproof fuel tank |
Country Status (1)
Country | Link |
---|---|
US (1) | US1591618A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2850083A (en) * | 1952-10-08 | 1958-09-02 | A V Roe Canada Ltd | Cellular fuel tank |
FR2684970A1 (en) * | 1991-12-11 | 1993-06-18 | Nordon Cryogenie Snc | Fluid tank divided into several elementary volumes |
CN106314810A (en) * | 2016-10-19 | 2017-01-11 | 佛山市海科知识产权交易有限公司 | Oil tank structure and unmanned aerial vehicle |
-
1922
- 1922-12-14 US US606872A patent/US1591618A/en not_active Expired - Lifetime
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2850083A (en) * | 1952-10-08 | 1958-09-02 | A V Roe Canada Ltd | Cellular fuel tank |
FR2684970A1 (en) * | 1991-12-11 | 1993-06-18 | Nordon Cryogenie Snc | Fluid tank divided into several elementary volumes |
CN106314810A (en) * | 2016-10-19 | 2017-01-11 | 佛山市海科知识产权交易有限公司 | Oil tank structure and unmanned aerial vehicle |
CN106314810B (en) * | 2016-10-19 | 2019-06-14 | 佛山市海科知识产权交易有限公司 | A kind of Oiltank structure and unmanned plane |
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