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US2415260A - Container - Google Patents

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US2415260A
US2415260A US504473A US50447343A US2415260A US 2415260 A US2415260 A US 2415260A US 504473 A US504473 A US 504473A US 50447343 A US50447343 A US 50447343A US 2415260 A US2415260 A US 2415260A
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Prior art keywords
container
tube
end portion
strips
secured
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US504473A
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Richards Alfred Augustus
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Edward Lloyd Ltd
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Edward Lloyd Ltd
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00Arrangements in connection with fuel supply for power plant
    • B64D37/02Tanks
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S229/00Envelopes, wrappers, and paperboard boxes
    • Y10S229/941Box having joint structure for preventing leakage

Definitions

  • This invention relates to containers made substantially of paper material.
  • a container according tothe invention is suitable for use as a supplementary fuel tank for aircraft.
  • Such fuel tanks have hitherto been made of metal but there is the advantage of a saving of metal in making the tanks of paper, especially in the case Where it is intended that the tanks may be jettisoned from the aircraft when in flight.
  • containers according to the invention are a primary use of containers according to the invention as a supplementary fuel tank for aircraft, it is to be understood that the construction is such as to render the container suitable for many other purposes and not necessarily for holding fuel or other liquids.
  • a feature of the construction of container according to the invention is that the container has a tapering or rounded end portion joined to a body portion by means of an internal ring overlapped by the adjoining parts of the end portion and body portion and secured to these parts by adhesive.
  • the ring is advantageously provided in its outer surface Viig/ith circumferential recesses filled with adhesive or sealing medium in order to strengthen the joint and adequately seal it.
  • the adhesive or sealing medium is preferably forced into the recessesl under high pressure.
  • the end portion may comprise strips of paper material which have been laid lengthwise and are tapered in accordance with a rounded or bulbous form of the end portion so that their edges abut and whose forward narrow ends are folded back and anchored to a tube.
  • the anchoring is suitably effected by folding back the narrow ends of the strips inside the tube and securingthem to the tube by adhesive.
  • the end portion is built up to the desired thickness with a plurality of layers of strips adhesively bonded together.
  • a layer or plurality of strips may be part of a sheet of paper which has been cut out accordingly, leaving an uncut portion at the base of the strips which corresponds to a cylindrical or non-rounded part of the end portion adjacent to its joint with the body portion.
  • the hole at the front 'or nose of the container Where the ends of the strips are folded back and anchored to the tube may be covered by a cap secured in position by ⁇ a tie connecting it to a member held by the tube.
  • the securing of the cap may be effected by a nut and bolt, the latter being carried by a dog or bracket held by the inner end of the tube.
  • the rim of the cap when secured in position may be embedded in the front or nose of the container at or about the point Where the strips are folded back so that the cap makes a substan tially flush contour therewith.
  • the container may have two tapering or rounded end portions each joined to a body portion as hereinbefore described and being otherwise characterised as indicated.
  • the container When the container is for use as a supplementary fuel tank for aircraft or vehicles where it is in the slip stream the end portions will be respectively shaped so 'as to give a streamline to the whole container.
  • the paper material When intended to contain liquidy e. g. fuel for internal combustion engines, the paper material is made or is proofed so as to resist permeation of or attack by the liquid concerned.
  • a suitable procilng for coating the internal surface of the paper material when the container is required to hold liquid fuel is a plasticised shellac composition.
  • a liquid container according to the invention may be internally tted with transverse bailles serving to break fore and aft wash of the liquid but allowing the liquid and air to pass from one side of the baille to the other side.
  • a baille for this purpose is preferably secured within a ring tted inside the container and the baille may be made of wood, e. g. plywood, whilst the ring is of paper material.
  • An appropriate number of rings may be secured inside the container for mounting the transverse baffles and there may be used for the purpose a ring which is employed for the joining of an end portion of the container to a body portion.
  • Passage for liquid vfrom one side of al baille to the other side is provided by apertures in the baille.
  • a passage for liquid at the bottom of the container may also be provided by forming the baille and ring with a flat or other deformation so as to leave a space between that part of the ring and the container.
  • This form of passage is particularly applicable in the case where there are-A openings in the top of the body of the container provided for liquid intake and take-off Where the body isilattened at the places where the openings ⁇ are made, so that the flat or otherwise deformed part of the ring enables the latter, with the said part uppermost, to be inserted in position past the flattened place of the body of the containerV and then turned round until the said part is lowermost.
  • the container when used as a supplementary fuel tank on aircraft will comprise means for connecting it to a part of the aircraft structure.
  • Such connecting means is preferably secured to a part of the container where the latter is reinforced by an internal ring so as to distribute the stresses transmitted by the connecting means.
  • the connecting means may be a bracket secured to the top of the container and adapted to receive a suspension connection which is readily detachable so that the container may be jettisoned from the aircraft at will.
  • Means may be provided in the container for holding against displacement the end of a liquid take-off pipe extending into the interior of the container.
  • Such means may comprise blocks secured to the bottom of the container and adapted to bear against the sides of a filter box on the end of the take-off pipe.
  • FIG. 1 is a longitudinal section
  • Figure 2 is a transverse section on the line 2-2 of Figure l
  • Figure 3 is a transverse section on the line 3-3 of Figure 1
  • Figure 4 is a section of the detail at the nose of the container.
  • the container shown is made 'up of three pre-formed sections, the central body portion I and two bulbous or rounded end portions 2 and 3, each made of paper material.
  • the end portion 2 is at the front of the container and the end portion 3 at the rear, and
  • the shapes are such that theY container is of streamlined form renderingl it suitable for its intended purpose of being carried by an aircraft by being suspended either underneath the wing or the fuselage of the aircraft where it will serve as a supplementary fuel tank which can be jettisoned if and when desired,
  • the paper stock used for making the'portions of the container may be substantially the same as that which is now commonly used in the manufacture of fibre containers, shell cases and the like.
  • the end portions 2 and 3 are joined to the body portion I by means of the rings or tubes 4 and 5 respectively which are overlapped by the adjoining parts of the end'portion and body portion and secured to these parts by adhesive.
  • the rings 4 and 5 are each provided with circumferential recesses 5 which are filled with adhesive, e. g. glue, under high pressure.
  • the end portions 2 and 3 of the container are built up of a number of layers of thin paper strips, say about twelve layers, to the desired thickness which may be of the order of one fth of an inch which is a suitable thickness for the container shown, which is intended to hold ninety gallons of liquid fuel.
  • the strips of paper material used for making the end portions of the container are laid lengthwise over a former and are suitably tapered in Width-so thatwhen they have been laidtheir 4 edges abut.
  • the several layers of strips are adhesively bonded together with glue.
  • the rim of the cap is embedded in the end of the container at or about the point where the paper is folded back into the tube so that the cap makes a substantially flush contour with the adjacent part of the end of the container.
  • the container is internally fitted with transverse baffles I5, I6 and Il, for the purpose of breaking the fore and aft wash of the liquid con tents.
  • the baffles are provided with large circular apertures I8 shown in Figures A2 and 3 for the purpose of allowing the liquid to pass from one side of the baflie to the other side.
  • the holes I9 at the top of the baffles shown in Figures 2 and 3 permit the passage of air through the baffles when the liquid contents are being taken off.
  • the bailies which are made of plywood, are secured as shown in rings of paper material 20, 2
  • the rings are made of paper material but the actual baboards are preferably made of plywood.
  • the fuelA take-off pipe 24 carries at its lower end a-lter box ZGand this bears against blocks 21 and 28 secured to the bottom of the ⁇ container whereby the liquid take-'off pipe is held against displacement when the container Vis in use.
  • the means for connecting the container to the aircraft structure consists of the bracket indicated in dotted lines at 29 (see Figures 1 and 3)
  • the bracket base plate is secured to the top of the container by rivets, and the ring 5 which is extended as shown at 30 to underlap the bracket,r
  • bracket ⁇ the stresses which are transmitted through the bracket.
  • the holes 3l in the bracket ⁇ serve to receive detachable suspension connections from the aircraft structure.
  • substantially the whole of the container is made from paper material excepting the accessory metal parts such as the nose cap securing devices, the filler bush and plug, the fuel take-off iitment including the take-off pipe, the filter box and air inlet tube, and the connecting bracket for receiving the suspension connection from the aircraft.
  • These metal parts are connected together as previously indicated by the metal wire I4 which is shown in Figure 4 but not otherwise indicated in the drawing.
  • 51, I6 and l1 are preferably made of plywood.
  • the construction is Such as to provide a fuel tank which is comparatively light in weight and yet is nevertheless of a robust character and which is not readily dented or damaged as is a corresponding metal tank. Moreover, it is completely pressure tightand is suitable for the use of compressed air or gas to ensure discharge of the contents.
  • the interior of the container and the parts iitted therein are coated with prooiing material such as plasticised shellac.
  • the outer part of the container is coated with any suitable weatherproof varnish.
  • a container comprising a body portion, a tapering end portion of paper material, a tube, the said end portion being composed of bonded layers of tapering strips of paper material laid lengthwise with their edges abutting, and the forward narrow ends of the strips being folded back and anchored to said tube, and an internal ring of paper material overlapped by and secured by adhesive to adjoining parts of said body portion and said tapering end portion.
  • a container comprising a body portion, a tapering end portion of paper material, a tube, the said end portion being composed of bonded layers of tapering strips of paper material laid lengthwise with their edges abutting, and the forward narrow ends of the strips being folded back and anchored to.said tube, and an internal ring of paper material overlapped by and secured by adhesive to adjoining parts of said body portion and said tapering end portion, the said ring having circumferential recesses. lled with said adhesive.
  • a container comprising a body portion, a tapering end portion of paper material, a tube, the said end portion being composed of bonded layers of tapering strips of paper material laid lengthwise with their edges abutting, and the forward narrow ends of the strips being folded back and anchored to said tube, and an internal ring of paper material overlapped by and secured by adhesive to adjoining parts of said body portion and said tapering end portion, the said paper material being proofed so as to resist permeation and attack by liquid contents.
  • a container comprising a body portion, a tapering end portion of paper material, a tube, the said end portion being composed of bonded layers of tapering strips of paper material laid lengthwise with their edges abutting, and the forward narrow ends of the strips being folded back and anchored to said tube, and an internal ring of paper material overlapped by and secured by adhesive to adjoining parts of said body portion and said tapering end portion, the said paper material being proofed so as to resistl permeation and attack by liquid fuel.
  • a container comprising a body portion, a tapering end portion of paper material, a tube, the said end portion being composed of bonded layers of tapering strips of paper material laid lengthwise with their edges abutting, and the forward narrow ends of the strips being folded back and anchored to said tube, and means securing together the adjoining parts of said body portion and said end portion.
  • a container as claimed in claim 1 in which a plurality of said tapering strips are integrally combined in a cut sheet of paper having an uncut portion at the base of the strips which corresponds to a substantially cylindrical portion of the said end portion adjacent to its joint with the said body portion.
  • a container according to claim 1 in which a cap is secured in position so as to cover the end 0f said tube in the front of the said end portion.
  • a container according to claim 1 in which a cap covering the end of said tube in the front of the said end portion is secured in position by a tie connecting it to a member held by the said tube.
  • a container according to claim 1 in which a cap covering the end of said tube in the front of the said end portion is secured in position by a nut and bolt, the latter being carried by a bracket held by the inner end of the said tube.
  • a container according to claim 14 in which a cap covering the end of said tube in the front of the said end portion is secured in position by a nut and bolt, the latter being carried by a bracket held by the inner end of the said tube, the arrangement being such that the rim of the cap is embedded in the front of the container about the place where the said paper strips are folded back so that the cap makes a substantially flush contour therewith.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Details Of Rigid Or Semi-Rigid Containers (AREA)

Description

A. A. RICHARDS CONTAINER Feb. 4, 1947.`
N SE
Patented Feb. 4, 1947 l UNITED STATES PATENT OFFICE bourne, England, assigner to Edward Limited, London, EnglandA Lloyd Application September 30, 1943, Serial No. 504,473 In Great Britain July 20, 1943 Claims. l
This invention relates to containers made substantially of paper material.
A container according tothe invention is suitable for use as a supplementary fuel tank for aircraft. Such fuel tanks have hitherto been made of metal but there is the advantage of a saving of metal in making the tanks of paper, especially in the case Where it is intended that the tanks may be jettisoned from the aircraft when in flight. There is, however, a further advantage of the paper container according to the invention that it is more robust than, and at the same time as light as, a metal tank of the same capacity.
Although a primary use of containers according to the invention is as a supplementary fuel tank for aircraft, it is to be understood that the construction is such as to render the container suitable for many other purposes and not necessarily for holding fuel or other liquids.
A feature of the construction of container according to the invention is that the container has a tapering or rounded end portion joined to a body portion by means of an internal ring overlapped by the adjoining parts of the end portion and body portion and secured to these parts by adhesive.
The ring is advantageously provided in its outer surface Viig/ith circumferential recesses filled with adhesive or sealing medium in order to strengthen the joint and adequately seal it. The adhesive or sealing medium is preferably forced into the recessesl under high pressure.
'I'he adjoining parts of the end portion and body portion may be connected by staples across their abutting edges.
The end portion may comprise strips of paper material which have been laid lengthwise and are tapered in accordance with a rounded or bulbous form of the end portion so that their edges abut and whose forward narrow ends are folded back and anchored to a tube. The anchoring is suitably effected by folding back the narrow ends of the strips inside the tube and securingthem to the tube by adhesive. The end portion is built up to the desired thickness with a plurality of layers of strips adhesively bonded together. A layer or plurality of strips may be part of a sheet of paper which has been cut out accordingly, leaving an uncut portion at the base of the strips which corresponds to a cylindrical or non-rounded part of the end portion adjacent to its joint with the body portion.
The hole at the front 'or nose of the container Where the ends of the strips are folded back and anchored to the tubemay be covered by a cap secured in position by `a tie connecting it to a member held by the tube. The securing of the cap may be effected by a nut and bolt, the latter being carried by a dog or bracket held by the inner end of the tube.
The rim of the cap when secured in position may be embedded in the front or nose of the container at or about the point Where the strips are folded back so that the cap makes a substan tially flush contour therewith.
It will be understood that the container may have two tapering or rounded end portions each joined to a body portion as hereinbefore described and being otherwise characterised as indicated.
When the container is for use as a supplementary fuel tank for aircraft or vehicles where it is in the slip stream the end portions will be respectively shaped so 'as to give a streamline to the whole container.
When intended to contain liquidy e. g. fuel for internal combustion engines, the paper material is made or is proofed so as to resist permeation of or attack by the liquid concerned. A suitable procilng for coating the internal surface of the paper material when the container is required to hold liquid fuel is a plasticised shellac composition.
A liquid container according to the invention may be internally tted with transverse bailles serving to break fore and aft wash of the liquid but allowing the liquid and air to pass from one side of the baille to the other side. A baille for this purpose is preferably secured within a ring tted inside the container and the baille may be made of wood, e. g. plywood, whilst the ring is of paper material.
An appropriate number of rings may be secured inside the container for mounting the transverse baffles and there may be used for the purpose a ring which is employed for the joining of an end portion of the container to a body portion.
Passage for liquid vfrom one side of al baille to the other side is provided by apertures in the baille.
p A passage for liquid at the bottom of the container may also be provided by forming the baille and ring with a flat or other deformation so as to leave a space between that part of the ring and the container. This form of passage is particularly applicable in the case where there are-A openings in the top of the body of the container provided for liquid intake and take-off Where the body isilattened at the places where the openings `are made, so that the flat or otherwise deformed part of the ring enables the latter, with the said part uppermost, to be inserted in position past the flattened place of the body of the containerV and then turned round until the said part is lowermost.
The container when used as a supplementary fuel tank on aircraft will comprise means for connecting it to a part of the aircraft structure. Such connecting means is preferably secured to a part of the container where the latter is reinforced by an internal ring so as to distribute the stresses transmitted by the connecting means.
The connecting means may be a bracket secured to the top of the container and adapted to receive a suspension connection which is readily detachable so that the container may be jettisoned from the aircraft at will. y
Means may be provided in the container for holding against displacement the end of a liquid take-off pipe extending into the interior of the container. Such means may comprise blocks secured to the bottom of the container and adapted to bear against the sides of a filter box on the end of the take-off pipe.
A supplementary fuel tank for laircraft is illustrated by way of example in the accompanying drawing, in which Figure 1 is a longitudinal section, Figure 2 is a transverse section on the line 2-2 of Figure l, Figure 3 is a transverse section on the line 3-3 of Figure 1 and Figure 4 is a section of the detail at the nose of the container.
Referring to the drawing, the container shown is made 'up of three pre-formed sections, the central body portion I and two bulbous or rounded end portions 2 and 3, each made of paper material. The end portion 2 is at the front of the container and the end portion 3 at the rear, and
the shapes are such that theY container is of streamlined form renderingl it suitable for its intended purpose of being carried by an aircraft by being suspended either underneath the wing or the fuselage of the aircraft where it will serve as a supplementary fuel tank which can be jettisoned if and when desired, The paper stock used for making the'portions of the container may be substantially the same as that which is now commonly used in the manufacture of fibre containers, shell cases and the like.
. The end portions 2 and 3 are joined to the body portion I by means of the rings or tubes 4 and 5 respectively which are overlapped by the adjoining parts of the end'portion and body portion and secured to these parts by adhesive. To improve the adhesion and sealing of the joint the rings 4 and 5 are each provided with circumferential recesses 5 which are filled with adhesive, e. g. glue, under high pressure.
The adjoining parts of the end portion and body portion are connected by metal staples which bridge the actual joint which is indicated by the numeral 1, the staples being inserted at suitable angular spacing around the joint. These staples are not shown in the drawing.
The end portions 2 and 3 of the container are built up of a number of layers of thin paper strips, say about twelve layers, to the desired thickness which may be of the order of one fth of an inch which is a suitable thickness for the container shown, which is intended to hold ninety gallons of liquid fuel.
The strips of paper material used for making the end portions of the container are laid lengthwise over a former and are suitably tapered in Width-so thatwhen they have been laidtheir 4 edges abut. The several layers of strips are adhesively bonded together with glue.
The forward narrow ends of the strips, shown in Figure 4 in their bonded composite state 8, are folded back inside a paper tube 9 as shown in Figure 4 and are secured to the tube 9 by glue.
The hole at the front or nose, and likewise at the rear of the container, where the end of the strips are folded back and secured to the tube 9,
is covered by a cap I0 which is secured in position by the nut II and bolt I2. The bolt I2 is carried by the dog or bracket I3 held by the inner end of the tube 9. In Figure 4 it will be noted that there is a part marked I4 and this is a wire which is provided for the purpose of connecting all metal accessories to the container so as to equalize their electric potential.
It will be noted in Figure 4 that the rim of the cap is embedded in the end of the container at or about the point where the paper is folded back into the tube so that the cap makes a substantially flush contour with the adjacent part of the end of the container.
The container is internally fitted with transverse baffles I5, I6 and Il, for the purpose of breaking the fore and aft wash of the liquid con tents. The baffles are provided with large circular apertures I8 shown in Figures A2 and 3 for the purpose of allowing the liquid to pass from one side of the baflie to the other side. The holes I9 at the top of the baiiles shown in Figures 2 and 3 permit the passage of air through the baffles when the liquid contents are being taken off.
The bailies, which are made of plywood, are secured as shown in rings of paper material 20, 2|, and also in the ring 5 previously referred to, these rings being secured in the container by adhesive. The rings are made of paper material but the actual baiiles are preferably made of plywood.
On the top of the container openings are formed which provide for liquid intake at 22 and liquid take-oil" at 23. At 22 a metal flange bush and removable stopper are fitted whilst at 2'3 a metal tment is incorporated which carries the take-olf pipe which extends as indicated 'at 24 into the interior of the container and an air inlet pipe not shown. At both the points 22 and 23 the body of the container is flattened as shown.
In order to enable the baille I5 and the ring 2B to be inserted past the ilattened part of the body of the container at 23 the baille is cut away to a flat at 25 (see Figure 2) and the ring is correspondingly flattened. Accordingly the baiile I5 is inserted past the flattened part 23.
Ywith its flat 25 uppermost and is then turned round to bring the flat 25 to the lowermost posi Y tion as shown in Figure 2. It will be noted that a further passage for liquid flow past the baffle is provided by tlie space between the flattened part of the ring and the bottom of the container.
The fuelA take-off pipe 24 carries at its lower end a-lter box ZGand this bears against blocks 21 and 28 secured to the bottom of the `container whereby the liquid take-'off pipe is held against displacement when the container Vis in use.
The means for connecting the container to the aircraft structure consists of the bracket indicated in dotted lines at 29 (see Figures 1 and 3) The bracket base plate is secured to the top of the container by rivets, and the ring 5 which is extended as shown at 30 to underlap the bracket,r
tainer the stresses which are transmitted through the bracket. The holes 3l in the bracket` serve to receive detachable suspension connections from the aircraft structure.
It will be appreciated that substantially the whole of the container is made from paper material excepting the accessory metal parts such as the nose cap securing devices, the filler bush and plug, the fuel take-off iitment including the take-off pipe, the filter box and air inlet tube, and the connecting bracket for receiving the suspension connection from the aircraft. These metal parts are connected together as previously indicated by the metal wire I4 which is shown in Figure 4 but not otherwise indicated in the drawing. The bailies |51, I6 and l1, as has already been mentioned, are preferably made of plywood.
The construction is Such as to provide a fuel tank which is comparatively light in weight and yet is nevertheless of a robust character and which is not readily dented or damaged as is a corresponding metal tank. Moreover, it is completely pressure tightand is suitable for the use of compressed air or gas to ensure discharge of the contents.
The interior of the container and the parts iitted therein are coated with prooiing material such as plasticised shellac. The outer part of the container is coated with any suitable weatherproof varnish.
What I claim is:
1. A container comprising a body portion, a tapering end portion of paper material, a tube, the said end portion being composed of bonded layers of tapering strips of paper material laid lengthwise with their edges abutting, and the forward narrow ends of the strips being folded back and anchored to said tube, and an internal ring of paper material overlapped by and secured by adhesive to adjoining parts of said body portion and said tapering end portion.
2. A container comprising a body portion, a tapering end portion of paper material, a tube, the said end portion being composed of bonded layers of tapering strips of paper material laid lengthwise with their edges abutting, and the forward narrow ends of the strips being folded back and anchored to.said tube, and an internal ring of paper material overlapped by and secured by adhesive to adjoining parts of said body portion and said tapering end portion, the said ring having circumferential recesses. lled with said adhesive.
3. A container comprising a body portion, a tapering end portion of paper material, a tube, the said end portion being composed of bonded layers of tapering strips of paper material laid lengthwise with their edges abutting, and the forward narrow ends of the strips being folded back and anchored to said tube, and an internal ring of paper material overlapped by and secured by adhesive to adjoining parts of said body portion and said tapering end portion, the said paper material being proofed so as to resist permeation and attack by liquid contents.
4. A container comprising a body portion, a tapering end portion of paper material, a tube, the said end portion being composed of bonded layers of tapering strips of paper material laid lengthwise with their edges abutting, and the forward narrow ends of the strips being folded back and anchored to said tube, and an internal ring of paper material overlapped by and secured by adhesive to adjoining parts of said body portion and said tapering end portion, the said paper material being proofed so as to resistl permeation and attack by liquid fuel.
5. A container comprising a body portion, a tapering end portion of paper material, a tube, the said end portion being composed of bonded layers of tapering strips of paper material laid lengthwise with their edges abutting, and the forward narrow ends of the strips being folded back and anchored to said tube, and means securing together the adjoining parts of said body portion and said end portion.
6. A container as claimed in claim 1 in which a plurality of said tapering strips are integrally combined in a cut sheet of paper having an uncut portion at the base of the strips which corresponds to a substantially cylindrical portion of the said end portion adjacent to its joint with the said body portion.
'7. A container according to claim 1 in which a cap is secured in position so as to cover the end 0f said tube in the front of the said end portion.
8. A container according to claim 1 in which a cap covering the end of said tube in the front of the said end portion is secured in position by a tie connecting it to a member held by the said tube.
9. A container according to claim 1 in which a cap covering the end of said tube in the front of the said end portion is secured in position by a nut and bolt, the latter being carried by a bracket held by the inner end of the said tube.
10. A container according to claim 14 in which a cap covering the end of said tube in the front of the said end portion is secured in position by a nut and bolt, the latter being carried by a bracket held by the inner end of the said tube, the arrangement being such that the rim of the cap is embedded in the front of the container about the place where the said paper strips are folded back so that the cap makes a substantially flush contour therewith.
ALFRED AUGUSTUS RICHARDS.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 2,310,818 Tomphins Feb. 9, 1943 2,172,504 Fish Sept. 12, 1939 2,201,332 Bensel May 21, 1940 2,284,499 Van Saun May 26, 1942 1,716,907 Staley June 11, 1929 1,713,170 Davis May 14, 1929 1,146,206 Quinlan July 13, 1915 948,951 Busby Feb. 9. 1910 170,377 Johnson Nov. 23, 1876 2,134,678 Billig et al Oct. 25, 1938 2,365,080 Humphreys Dec. '12, 1944
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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2756105A (en) * 1953-02-09 1956-07-24 American Can Co Protective shatterproof outer container for bottle
DE1013175B (en) * 1954-04-09 1957-08-01 Fletcher Aviat Corp Streamlined fuel tank
DE1038407B (en) * 1954-09-23 1958-09-04 Bristol Aircraft Ltd Dump container for external attachment to aircraft
US2895635A (en) * 1954-09-23 1959-07-21 Bristol Aircraft Ltd Containers for attachment to the exterior of aircraft
US20130220124A1 (en) * 2012-02-23 2013-08-29 Airbus Operations Limited Filter for a pipe

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US170377A (en) * 1875-11-23 Improvement in lightning-rods
US948951A (en) * 1906-10-01 1910-02-08 L A Busby Interchangeable shipping-case.
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US1713170A (en) * 1928-09-07 1929-05-14 Hugh B Daviss Fluid stabilizer
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US2172504A (en) * 1936-01-10 1939-09-12 Frederick C Fisk Bottle and blank for forming it
US2201332A (en) * 1936-12-15 1940-05-21 Albert Borden Bottom fill paperboard container
US2284499A (en) * 1940-10-21 1942-05-26 Container Corp Container
US2310818A (en) * 1942-05-26 1943-02-09 Harold D Tompkins Container
US2365080A (en) * 1943-08-02 1944-12-12 Ohio Rubber Co Droppable gasoline tank

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US170377A (en) * 1875-11-23 Improvement in lightning-rods
US948951A (en) * 1906-10-01 1910-02-08 L A Busby Interchangeable shipping-case.
US1146206A (en) * 1914-04-24 1915-07-13 Charles H Quinlan Mailing-tube.
US1716907A (en) * 1927-01-18 1929-06-11 Earl B Staley Multiple-compartment tank
US1713170A (en) * 1928-09-07 1929-05-14 Hugh B Daviss Fluid stabilizer
US2134678A (en) * 1935-05-04 1938-10-25 Breeze Corp Liquid tank
US2172504A (en) * 1936-01-10 1939-09-12 Frederick C Fisk Bottle and blank for forming it
US2201332A (en) * 1936-12-15 1940-05-21 Albert Borden Bottom fill paperboard container
US2284499A (en) * 1940-10-21 1942-05-26 Container Corp Container
US2310818A (en) * 1942-05-26 1943-02-09 Harold D Tompkins Container
US2365080A (en) * 1943-08-02 1944-12-12 Ohio Rubber Co Droppable gasoline tank

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2756105A (en) * 1953-02-09 1956-07-24 American Can Co Protective shatterproof outer container for bottle
DE1013175B (en) * 1954-04-09 1957-08-01 Fletcher Aviat Corp Streamlined fuel tank
DE1038407B (en) * 1954-09-23 1958-09-04 Bristol Aircraft Ltd Dump container for external attachment to aircraft
US2895635A (en) * 1954-09-23 1959-07-21 Bristol Aircraft Ltd Containers for attachment to the exterior of aircraft
US20130220124A1 (en) * 2012-02-23 2013-08-29 Airbus Operations Limited Filter for a pipe
US9289706B2 (en) * 2012-02-23 2016-03-22 Airbus Operations Limited Filter for a pipe

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