GB2072602A - Fuel tank component - Google Patents
Fuel tank component Download PDFInfo
- Publication number
- GB2072602A GB2072602A GB8106668A GB8106668A GB2072602A GB 2072602 A GB2072602 A GB 2072602A GB 8106668 A GB8106668 A GB 8106668A GB 8106668 A GB8106668 A GB 8106668A GB 2072602 A GB2072602 A GB 2072602A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wall
- fronds
- spine
- atangling
- tangling
- 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.)
- Granted
Links
- 239000002828 fuel tank Substances 0.000 title claims abstract description 16
- 229920002635 polyurethane Polymers 0.000 claims abstract description 7
- 239000004814 polyurethane Substances 0.000 claims abstract description 7
- 239000000463 material Substances 0.000 claims description 11
- 239000000446 fuel Substances 0.000 abstract description 14
- 238000007789 sealing Methods 0.000 abstract description 10
- 230000035515 penetration Effects 0.000 abstract description 3
- 230000008961 swelling Effects 0.000 abstract description 2
- 150000001875 compounds Chemical class 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000565 sealant Substances 0.000 description 1
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
- B64D37/32—Safety measures not otherwise provided for, e.g. preventing explosive conditions
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Abstract
An inner wall 1 for a self-sealing fuel tank in which the inner wall is provided with a plurality of fronds 6 bonded at one end to the wall, the fronts facing towards the inside of the tank such that on penetration of the wall of the tank by a projectile the fronds are carried by the surge of escaping fuel through the wall to become entangled as at 17,18 in the hole and choke off escaping fuel. The fronds may be formed by cuts 7,8 in strips 2,3,4 of polyurethane. Wall 1 is also of polyurethane. The tank outer wall, not shown, contains a known swelling sealing medium. <IMAGE>
Description
SPECIFICATION
Fuel tank component
This invention relates to fuel tank components and has particular reference to walls for use in selfsealing fuel tanks.
It is well-known to provide self-sealing fuel tanks formilitary aircraft. By virtue of their nature military aircraft are subject to penetration of projectiles such as bullets and shrapnel from exploding missiles etc.
The use of a self-sealing fuel tank helps the aircraft survive in two ways. Firstly, it chokes off the escape of fuel from the fuel tank which might cause fires in the aircraft and thus destroy it. Secondly, the conventional military aircraft by virtue of the large weight of stores it has to carry has problems in providing sufficient fuel capacity. Thus, when working at long ranges the aircraft will normally only have sufficient fuel just to get back to base. If this, however, is lost as a result of enemy action the aircraft will have to be abandoned even though it is flyable. Thus, retaining the fuel in the tank by means of self-sealing tanks enables the aircraft to return to base and thus be repaired and re-used. The second feature is probably of greater importance than the first feature.
Conventional self-sealing fuel tanks have a layer of material, normally on the outside of the tank, which swells up to choke off fuel escaping from the tank.
The layer may be of a type which is swellable when in contact with the fuel or may be activated by the heat of a projectile passing through it. It has been found that small diameter projectiles which leave small diameter holes can be dealt with quite adequately byswellable sealing means of this type.
However, recent advances in military technology have resulted in the use of larger diameter projectiles which can give rise to larger diameter holes.
The escaping fuel through these holes has been found to pass through the hole with sufficient velocity to wash out the expanding sealant so that the hole is never fully sealed.
In US Patent No 4088 240 there is described a wall for use in self-sealing tanks which is intended to help reduce problems of this type. Basically, the wall comprises a mat of thin elongate fibres arranged on the inside of the fuel tank. Once the projectile has passed through the wall the surge of escaping fuel carries with it strands of the mat adjacent the hole so as to restrict the flow of fuel through the hole.
The present invention is concerned with devices of this general type but which have improved choking characteristics compared to the prior art described in
US Patent No 4088240 and which may be easily and cheaply manufactured.
By the present invention there is provided a tangling wall for the inside of a fuel tank comprising a support layer having attached thereto strips of material, some at least of the strips having a spine and extending therefrom a plurality of strands having free ends remote from the spine.
The spines are preferably disposed in parallel rows. The strands of one spine preferably overlap the spine of the next adjacent row. The spine and strands are preferably integrally formed from a single strip of material. The spines are preferably bonded to the support layer. The spines are preferably welded to the support layer. Preferably the spine and strands are formed from the same material as the support layer. The material may be polyurethane. The strands are preferably in the form of flat elongate fronds. Preferably the edges of the fronds are not straight. The thickness of the fronds is preferably sufficient to make them self-supporting when held vertically upright.
The present invention further provides a fuel tank incorporating a tangling wall of the type herein disclosed. The strips are preferably disposed horizontally along the upright portions of the wall.
By way of example embodiments of the present invention will now be described with reference to the accompanying drawings, of which:
Figure 1 is a perspective view of a tangling wall in accordance with the present invention;
Figure 2 is a cross-section of a tank incorporating walls of the present invention;
Figure 3 is a side elevational view of one portion of a tangling wall;
Figure 4 is a side elevational view of a wall being penetrated buy a projectile; and
Figure 5 is a side elevational view of the wall of
Figure 4 after penetration.
Referring to Figure 1 this shows a tangling wall comprising a support layer 1 formed of a polyurethane sheet having bonded thereto strips 2,3 and 4 of polyurethane. Each strip comprises a spine such as 5 together with a series of fronds 6 which are formed integrally with the spine. The spines such as 5 are welded directly to the support layer 1. The fronds 6 are formed by cutting into the strips along a plurality of lines such as 7, 8. The tangling wall is located in a fuel tank as is shown in Figure 2.
The outer wall of the fuel tank 9 contains a suitable swelling sealing medium of known type. The inner wall 10 comprises a support layer equivalent to layer 1 of Figure 1. The strips of material are indicated schematically as at 11.
Referring to Figure 3 it can be seen that the strips each comprise a spine 12 integrally formed with fronds 13 which are produced by cutting the strip along lines 14.
As shown in Figure 4 the fronds to each strip overlap slightly so that when a projectile 15 passes through the support layer 1 it displaces the fronds such as frond 16. Because polyurethane is sufficiently tough it has been found that the frond is not destroyed by the projectile passing through the wall.
Once the projectile has passed through the wall fuel immediately attempts to escape through the hole thus formed in a surge which carries through the fronds so that they become entangled in the hole as is shown in Figure 5.
It can be clearly seen from Figure5 that the fronds such as 17 from the layer 3 have become entangled with fronds such as 18 from the layer below.
Because of the roughness of the fronds resulting from the zig-zag or sinusoidal cuts used to make the fronds the fronds become trapped in the hole. It has been found that following the initial surge of fuel out of the tank there is a negative pressure developed in the tank (which is often formed of a flexible material in any case) such that there is an attempt to suck back the fronds from the hole in the tank. With thin fibres it is believed that the fibres are simply swept back into the tank, thus undoing the good they have formed by entering the hole in the first place. With the thicker fronds provided by the strips of the present invention, however, particularly when the fronds have rough edges, the fronds stay in the hole to choke off the fuel supply and to restrict it to a sufficiently significant amount such that conventional self-sealing compounds are able to completely seal the tank.
Claims (15)
1. A tangling wall for the inside of a fuel tank comprising a support layer having attached thereto strips of material, some at least of the strips having a spine and extending therefrom a plurality of strands having free ends remote from the spine.
2. Atangling wall as claimed in Claim 1 in which the spines are disposed in parallel rows.
3. Atangling wall as claimed in Claim 1 or Claim 2 in which the strands of one spine overlap the spine of the next adjacent row.
4. Atangling wall as claimed in any one of
Claims 1 to 3 in which the spine and strands are formed integrally from a single strip of material.
5. A tangling wall as claimed in any one of
Claims 1 to 4 in which the spines are bonded to the support layer.
6. Atangling wall as claimed in Claim 5 in which the spines are welded to the support layer.
7. A tangling wall as claimed in any one of
Claims 1 to 6 in which the spine and strands are formed from the same material as the support layer.
8. A tangling wall as claimed in Claim 7 in which the material is a polyurethane.
9. A tangling wall as claimed in any one of
Claims 1 to 8 in which the strands are in the form of flat elongate fronds.
10. Atangling wall as claimed in Claim 9 in which the edges of the fronds are not straight.
11. Atangling wall as claimed in any one of
Claims 9 or 10 in which the thickness of the fronds is sufficient to make them self-supporting when held vertically upright.
12. Afuel tank incorporating a tangling wall as claimed in any one of Claims 1 to 11.
13. Afuel tank as claimed in Claim 12 in which the strips are disposed horizontally along the upright portions of the wall.
14. Atangling wall substantially as herein described with reference to the accompanying drawings.
15. A fuel tank substantially as herein described with reference to and as illustrated by the accompanying drawings.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8106668A GB2072602B (en) | 1980-03-29 | 1981-03-03 | Fuel tank component |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8010703 | 1980-03-29 | ||
GB8106668A GB2072602B (en) | 1980-03-29 | 1981-03-03 | Fuel tank component |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2072602A true GB2072602A (en) | 1981-10-07 |
GB2072602B GB2072602B (en) | 1983-07-27 |
Family
ID=26275029
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8106668A Expired GB2072602B (en) | 1980-03-29 | 1981-03-03 | Fuel tank component |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2072602B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2155873A (en) * | 1984-03-17 | 1985-10-02 | British Aerospace | Liquid storage tanks |
-
1981
- 1981-03-03 GB GB8106668A patent/GB2072602B/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2155873A (en) * | 1984-03-17 | 1985-10-02 | British Aerospace | Liquid storage tanks |
Also Published As
Publication number | Publication date |
---|---|
GB2072602B (en) | 1983-07-27 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4422561A (en) | Fuel tank component | |
US4076100A (en) | Oil impervious acoustical board | |
US4125053A (en) | Armor | |
US5070764A (en) | Combined reactive and passive armor | |
US6200664B1 (en) | Explosion barrier | |
RU2108434C1 (en) | Multilayer explosion-proof panel and method for protection of structure from shock action of explosion | |
EP0076899A1 (en) | Bullet catcher | |
DE69635449T2 (en) | MEANS OF PROTECTION FROM RADIATION ENERGY | |
US4469295A (en) | Hydrodynamic ram attenuating fuel tank | |
US4088240A (en) | Fuel tank leakage fiber flow sealant | |
US5563364A (en) | Anti-explosion pads and their method of use | |
AU2012203499B2 (en) | Armor element and an armor module comprising the same | |
GB2072602A (en) | Fuel tank component | |
GB2054457A (en) | Self-sealing flexible fuel tank | |
DE2655674C3 (en) | Fire body with anchoring point | |
US2851054A (en) | Flutter valves | |
US1776610A (en) | Heat-insulating panel | |
DE4223538C1 (en) | Device to damp effect of exploding munition on window - comprises optically transparent, UV-resistant screen plate with no tendency to splinter | |
FI84392C (en) | Fire retardant barriers for conducting wiring in a wall opening | |
GB2054456A (en) | Fuel tank protection means | |
DE3842677C1 (en) | Active armour esp. for armoured vehicle | |
DE1961549A1 (en) | Packaging for drop ammunition, especially artillery cartridges | |
JPH05222912A (en) | Muffler | |
US2318966A (en) | Wall and building structure | |
DE303983C (en) |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
732 | Registration of transactions, instruments or events in the register (sect. 32/1977) | ||
PCNP | Patent ceased through non-payment of renewal fee |