US3109611A - Balloon seam structure and method of sealing balloon materials - Google Patents
Balloon seam structure and method of sealing balloon materials Download PDFInfo
- Publication number
- US3109611A US3109611A US125559A US12555961A US3109611A US 3109611 A US3109611 A US 3109611A US 125559 A US125559 A US 125559A US 12555961 A US12555961 A US 12555961A US 3109611 A US3109611 A US 3109611A
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- Prior art keywords
- seam
- balloon
- strip
- envelope
- gas
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- 239000000463 material Substances 0.000 title claims description 65
- 238000000034 method Methods 0.000 title description 6
- 238000007789 sealing Methods 0.000 title description 6
- 238000010276 construction Methods 0.000 claims description 6
- 230000002401 inhibitory effect Effects 0.000 claims description 3
- 238000001881 scanning electron acoustic microscopy Methods 0.000 claims 3
- 239000004744 fabric Substances 0.000 description 12
- 230000004888 barrier function Effects 0.000 description 9
- 229920001169 thermoplastic Polymers 0.000 description 8
- 239000004416 thermosoftening plastic Substances 0.000 description 8
- 230000008901 benefit Effects 0.000 description 5
- 238000009958 sewing Methods 0.000 description 4
- 239000004033 plastic Substances 0.000 description 3
- 229920003023 plastic Polymers 0.000 description 3
- 239000012815 thermoplastic material Substances 0.000 description 3
- 229920002799 BoPET Polymers 0.000 description 2
- 239000005041 Mylar™ Substances 0.000 description 2
- 239000004698 Polyethylene Substances 0.000 description 2
- 238000005299 abrasion Methods 0.000 description 2
- 238000007667 floating Methods 0.000 description 2
- 230000000149 penetrating effect Effects 0.000 description 2
- -1 polyethylene Polymers 0.000 description 2
- 229920000573 polyethylene Polymers 0.000 description 2
- 241000557626 Corvus corax Species 0.000 description 1
- 229920000742 Cotton Polymers 0.000 description 1
- 239000004677 Nylon Substances 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 239000004568 cement Substances 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 229920001778 nylon Polymers 0.000 description 1
- LFULEKSKNZEWOE-UHFFFAOYSA-N propanil Chemical group CCC(=O)NC1=CC=C(Cl)C(Cl)=C1 LFULEKSKNZEWOE-UHFFFAOYSA-N 0.000 description 1
- 238000004826 seaming Methods 0.000 description 1
- 230000007480 spreading Effects 0.000 description 1
Images
Classifications
-
- D—TEXTILES; PAPER
- D05—SEWING; EMBROIDERING; TUFTING
- D05B—SEWING
- D05B93/00—Stitches; Stitch seams
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/72—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by combined operations or combined techniques, e.g. welding and stitching
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/112—Single lapped joints
- B29C66/1122—Single lap to lap joints, i.e. overlap joints
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
- B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
- B29C66/43—Joining a relatively small portion of the surface of said articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/723—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined being multi-layered
- B29C66/7234—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined being multi-layered comprising a barrier layer
- B29C66/72343—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined being multi-layered comprising a barrier layer for liquids
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/58—Arrangements or construction of gas-bags; Filling arrangements
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/71—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2022/00—Hollow articles
- B29L2022/02—Inflatable articles
- B29L2022/022—Balloons
-
- D—TEXTILES; PAPER
- D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B2507/00—Sport; Military
- D10B2507/10—Balloons
Definitions
- the present invention relates to improvements in balloons and more particularly to a ballon seam structure which per-mits the attachment of adjacent sheets or gores of a ballon by stitching lwithout the leakage of gas through the stitched seam.
- the present invention contemplates the provision ⁇ of a balloon formed of a material which is resistant to soulfs and abrasions by contact with objects, has a good tensile strength, and yet is light in weight and impervious to the escape of gas.
- Thin lightweight plastics are desirable for balloon materials because of their gas impervious and lightweight properties, and because -successful gas impervious seams can be easily made such as by using heat seals between gores or shts of the balloon material.
- the materials are however easily punctured or torn.
- Fabric materials are scuff resistant and have a good tensile strength but are quite porous to gas and are not conveniently seamed to provide a joint which will not leak gas.
- a feature ⁇ of the present invention is the provision of a bal-lon structure utilizing the advantageous properties oi these different materials by combining them, and providing a seam of a unique nature which permits the adjacent sheets or gores lof ⁇ combined material to be simply and quickly joined to provide a strong but gas impervious seam.
- a further lobject ⁇ of the invention i-s to provide an improved seam -for joining adjacent sheets or gores of balloon material formed of layers of scul resistant fabric and gas impervious thermoplastic wherein the seam has a tensile strength approaching the lstrength of the fabric and has the ygasproof integrity of the thermoplastic material.
- a still further object of the invention is to provide an improved seam structure wherein adjacent sheets of balloon material can be sewn together and wherein an inner seam strip is provided opposite the sewn seam to prevent leakage of gas between the layers at the seam, to prevent gas from penetrating the seam gap, and to readily accommodate seams of different shapes.
- -A feature of the invention is to provide a seam for joining adjacent sheets or gores of balloon material having an outer fabric layer and an inner thermoplastic layer by sewing the sheets together to form a seam, providing an inner thermoplastic seam strip layer within the balloon heat sealed at its edges at each side of the sewn seam.
- a still further object of the invention is to provide an improved method of forming a seam at the edges of ballon sheets or gores utilizing a seam strip.
- FIGURE l is an elevational view of a balloon of the type embodying the principles of the present invention.
- FIGURE 2 is a greatly enlarged sectional view shown in somewhat schematic form illustrating a step in forming a seam between the gores of the balloon;
- FIGURE 3 is a horizontal sectional view shown greatly enlarged and taken -substantially along line III-III of FIGURE l;
- FIGURE 4 is a fragmentary perspective view of a seam formed at the edge of gores, constructed in accordance with the invention.
- FIGURE l illustrates a balloon lll of the free floating type lled with a lifting gas wherein the balloon envelope is formed of a series of shaped gores 11 and 12 joined to each other by seams 13 at their edges. Whilerin the preferred example a shaped gored balloon is shown, it will be understood that the balloon seam may be employed in various other ballons joining the edges of adjacent sheets of balloon material, such as in a balloon formed of non-shaped rectangular strip gores. The features of the seam also may be used to advantage in captive balloons as well as free floating balloons and can be used in' balloons employed basically for load carrying functions such as for carrying scientific instruments aloft or can be Iused for man flight balloons.
- the sheets or gores of the balloon are formed of plural layers ⁇ with the outer layer being a scuif resistant fabric 16 and 18 ⁇ for the respective gores.
- the cloth or fabric may be various suitable materials, having a scuff resistance and tensile strength and beinfY of a light Weight, such as nylon, Daeron, Orion, polypropelene or other plastic or cotton materials.
- the inner layers 17 and 19 of the :gores are of a gas barrier lm preferably thermoplastic such as polyethylene, Mylar or other suitable lightweight gas impervious material.
- the layers 16 and 17, and 18 and 19 are preferably joined such as by a thermoplastic cement but need not be rmly bonded, although they may be laminated so as to be non-separable or in some instances can be formed of separate sheets superimposed upon each other.
- the inner layer forms a gas barrier and need not contribute tensile strength and therefore can be very thin and lightweight, while the outer layer provides the tensile strength and abrasion resistance for the balloon envelope, thereby avoiding the vulnerability to punctures and rips that is present with a balloon envelope made solely of thermoplastic material.
- the seam strip is doubled so that it edges 25 and 26 project in the same direction as the edges 27 and 28 of the gores.
- the seam strip is a lightweight thin gas impervious -film such as a thermoplastic, and can be polyethylene, Mylar or conveniently of the same material as the inner layers 17 and 19 of the balloon gores.
- the edges of the seam strip 2d are joined to the inner surfaces of the gores by strip seams 21 and 22, FIGURES 2 and 3. This can conveniently be done by heat sealing devices shown at 23 for the seam 21 and at 24 for the seam 22.
- the heat sealing devices may be of known types such as rollers or heated air Sealers such as used for joining thermoplastic balloon materials.
- the edges of the gores are next joined by sewing with a thread to form stitching 29, to form an envelope seam, as illustrated in FIGURES 3 and 4 in the finished form with the stitching being applied at the locations indicated by the arrows Sil in FIGURE 2.
- the stitching can be easily accomplished by a sewing machine after the edges 27 and 28 are brought together, and the entire seam may be formed in'a single operation, in a single pass through a machine. Also, for long balloon gores, a carriage may be provided supporting heat sealing equipment ahead of 3 a sewing machine with the carriage running along the edges ofthe gores.
- the thread for forming the stitches Z9 may be any suitable thread, light in weight and having adequate tensile strength so that the sewn seam holds together the adjacent fabric gores with a strength approaching the original strength of the fabric. Lateral pulling on the seam may tend to spread the threads and separate the layers at the seam, but this is of no consequence insofar as the gas integrity of the seam'is concerned inasmuch as the escape of gas is positively prevented by the inner seam strip Ztl which lies along the inside of the balloon in the manner shown in FIGURE 3.
- FIGURE 3 illustrates the condition of the seam in the balloon when the balloon is iniiated to form the balloon envelope.
- the iiexible seam strip Ztl will conform to the shape of the seam and the doubled over ends 3i and 32 and seams 2l and CL2 will form a gas barrier.
- the extra strip material against the gores aids in maintaining the integrity of the seals Zi and 22 and the spreading of the'gores is not acting to separate the seals 2li and 22. Therefore no leakage will occur and a gastight joint is provided.
- the seam strip material 2li between the seams 2l and 22 is greater than the distance between the seams 21 and 22 to provide a bulging of material preventing stresses on the materials.
- the seam strip 2i prevents gas from directly penetrating between the threads. ln some instances the seam strip will provide insulation if the outer skin is hot or cold relative to the gas within the balloon envelope.
- sewn seam is not to be limited to the precise arrangement illustrated, although advantages are obtained in a strong seam which is simply made, but other seams of different sewn structures or seams not sewn may be employed.
- a balloon construction comprising a balloon envelope having an outer layer of fabric material with a relatively high tensile strength, an inner layer of nonporous gas impervious material coextensive with the outer layer, a thread-stitched seam joining adjacent edges of the combinedrinner and outer layers to form a balloon envelope, a strip of non-porous gas impervious material Within the balloon over said seam, inhibiting the leakage of gas therethrough, and gas impervious str-ip seams joining the strip to the inner layer at each side of said stitched seam.
- a balloon construction comprising a balloon envelope having an outer layer of fabric material with a relatively high tensile strength, an inner layer of a thermo- '4 plastic non-porous gas impervious material coextensiv with the outer layer, a stitched seam joining adjacent edges of the combined inner and outer layers to form a balloon envelope, a strip of lightweight thin thermoplastic material within the envelope over said seam inhibiting the leal'a of gas therethrough, and vertical gas impervious conL nuous heat seals forming strip seams attaching the strip to the inner layer at each side of the stitched seam.
- a balloon envelope having a seam joining adjacent portions or balloon material, a strip of gas impervious material positioned over the envelope seam, and strip seams attaching the strip to the balloon material at each side oi said envelope seam with said strip having a greater Width between the strip seams than the width of balloon material between said strip seams for an excess of strip material over'said envelope seam so that the strip will fold when pressed against the envelope seam, said width of strip material between said strip seams being sufficient so that space exists between the inner surface ofthe envelope seam and the strip when the strip is not pressed against the seam from pressure within the balloon envelope and so that the strip is not stressed in the direction of balloon material when forces on the balloon material stress said envelope seam.
- the method of forming a seam between adjacent first and second sheets providing layers of balloon envelope material having inner and outer surfaces and a length of strip material comprising positioning first and second layers formed by the edges of the strip material adjacent the respective edges of the sheet layers against said inner surfaces of the sheet layers with the edges of the strip layers extending in the same direction as the edges of the sheet layers and joining the layers to form an envelope seam so that the strip will straddle said envclope seam when the sheet layers are drawn apart to be coplanar.
- a balloon construction comprising a plurality of gores of material each joined to an adjacent gore by a stress sustaining gas pervious envelope seam to form a balloon envelope, and seam strips within the balloon envelope positioned over the envelope seams and each joined to the gores by a gas impervious seam to lie against the inner surface of the stress sustaining envelope seam and inhibit the leakage of gas through the envelope seam, said seam strips being substantially relaxed so that no stress is placed on the gas impervious seams when forces are applied on the gores and the envelope seams are stressed, and the strips are freely pressed against the inner surface of the balloon envelope with gas pressure therein.
- a balloon envelope having a gas pervious stress sustaining balloon envelope seam joining adjacent portions of balloon material, a layer of gas impervious seam barrier material positioned over the balloon envelope seam, and a supporting means for supporting said layer in place over the seam so that said barrier material forms a gas barrier against the inner surface of the balloon material at the sides of the envelope seam to inhibit the leakage of gas through the envelope seam, said layer being substantially relaxed so that no stress is placed on the supporting means when the envelope seams are stressed and the layer is freely pressed against the inner surface of the balloon envelope with gas pressure therein.
- a balloon envelope having a longitudinalrballoon envelope seam joining adjacent portions of balloon material, a layer oi seam barrier material positioned over said balloon envelope seam, portions at the edges of said seam barirer material turned under and free of attachment to the envelope material adjacent the edges of the turned under portions so that the barrier material is free of stresses in a lateral direction, and means for supporting said layer of barrier material in place over the envelope seam to inhibit t'ne leakage of gas through the seam, said layer being free of stress in said lateral direction along the balloon material when forces are applied to said adjacent portions and the searn is under stress, and said layer freely pressed against the inner surface of the balloon envelope with gas pressure therein.
- a balloon construction comprising a plurality of vertically extending balloon gores each joined to an adjacent gore by a gore seam to form a balloon envelope for containing a lifting gas, a vertical horizontally narrow strip over each of said seams within the balloon to prevent leakage through the seam, and means for supporting said vertical strip on the inner surface of the balloon, said narrow strip being free of stress in the direction of balloon gores when the balloon seam is stressed and said strip being freely pressed against the inner surface of the ballon with gas pressure within the balloon.
- a balloon envelope adjacent sheets of balloon material joined by a balloon seam capable of withstanding tensile stresses on said sheets, and a layer of material positioned over said seam joined to said sheets by gas 6 proof seams incapable in itself of sustaining said tensile stresses and being impervious to gas, said layer being relaxed and unstressed and said gas proof seams being unstressed when said balloon seam is stressed and said layer freely pressed against the inner surface of the balloon envelope with gas pressure therein.
- a seam structure comprising adjacent sheets of balloon material joined by stitching forming an envelope seam securing the edges of the sheets together, and a seam strip against said seam on the inner surrace of the balloon having side edges turned inwardly beneath the strip against the balloon material with said seam strip held against the envelope seam by pressure within the balloon, said turnedizider side edges providing excess material so that said strip is unstressed in the direction of balloon material when said envelope seam is stressed.
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Description
Nov. 5, 1963 P. E. YosT 3,109,611
BALLooN STAM STRUCTURE AND METHOD oF sEALING BALLooN MATERIALS Filed July 20. 1961 IN VEN TOR. ,000/ [da/Qro J/osz BY Y@ MW @uw M0/@1 /T MTEYS A TT() United States Patent O 3,109,611 EALLQN SESAM STRUCTURE ANI) METHD @F SEALING BALLN MATERIALS Paul E. Yost, Sioux Falls, S. Dali., assigner to Raven industries, Inc., Sioux Falls, S. Dak., a corporation or" South Dakota Filed July 2t), 1961, Ser. No. 125,559 11 Claims. (fCl. 24d-31) The present invention relates to improvements in balloons and more particularly to a ballon seam structure which per-mits the attachment of adjacent sheets or gores of a ballon by stitching lwithout the leakage of gas through the stitched seam.
The present invention contemplates the provision `of a balloon formed of a material which is resistant to soulfs and abrasions by contact with objects, has a good tensile strength, and yet is light in weight and impervious to the escape of gas. Thin lightweight plastics are desirable for balloon materials because of their gas impervious and lightweight properties, and because -successful gas impervious seams can be easily made such as by using heat seals between gores or shts of the balloon material. The materials are however easily punctured or torn. Fabric materials are scuff resistant and have a good tensile strength but are quite porous to gas and are not conveniently seamed to provide a joint which will not leak gas. A feature `of the present invention is the provision of a bal-lon structure utilizing the advantageous properties oi these different materials by combining them, and providing a seam of a unique nature which permits the adjacent sheets or gores lof `combined material to be simply and quickly joined to provide a strong but gas impervious seam.
Accordingly, it is an object `of the present invention to provide an improved balloon structure with a balloon envelope material that is ptmcture and tear resistant so that it can be used in adverse circumstances and is rugged and durable for reuse, and is impervious to the leakage of gas.
A further lobject `of the invention i-s to provide an improved seam -for joining adjacent sheets or gores of balloon material formed of layers of scul resistant fabric and gas impervious thermoplastic wherein the seam has a tensile strength approaching the lstrength of the fabric and has the ygasproof integrity of the thermoplastic material.
A still further object of the invention is to provide an improved seam structure wherein adjacent sheets of balloon material can be sewn together and wherein an inner seam strip is provided opposite the sewn seam to prevent leakage of gas between the layers at the seam, to prevent gas from penetrating the seam gap, and to readily accommodate seams of different shapes.
-A feature of the invention is to provide a seam for joining adjacent sheets or gores of balloon material having an outer fabric layer and an inner thermoplastic layer by sewing the sheets together to form a seam, providing an inner thermoplastic seam strip layer within the balloon heat sealed at its edges at each side of the sewn seam.
A still further object of the invention is to provide an improved method of forming a seam at the edges of ballon sheets or gores utilizing a seam strip.
Other objects, advantages and features will become more apparent with the teaching of the principles of the invention in connection with the disclosure of the preferred embodiment thereof in the speciiication, claims and drawings, in which:
FIGURE l is an elevational view of a balloon of the type embodying the principles of the present invention;
FIGURE 2 is a greatly enlarged sectional view shown in somewhat schematic form illustrating a step in forming a seam between the gores of the balloon;
"ree
FIGURE 3 is a horizontal sectional view shown greatly enlarged and taken -substantially along line III-III of FIGURE l; and
FIGURE 4 is a fragmentary perspective view of a seam formed at the edge of gores, constructed in accordance with the invention.
As shown on the drawings:
FIGURE l illustrates a balloon lll of the free floating type lled with a lifting gas wherein the balloon envelope is formed of a series of shaped gores 11 and 12 joined to each other by seams 13 at their edges. Whilerin the preferred example a shaped gored balloon is shown, it will be understood that the balloon seam may be employed in various other ballons joining the edges of adjacent sheets of balloon material, such as in a balloon formed of non-shaped rectangular strip gores. The features of the seam also may be used to advantage in captive balloons as well as free floating balloons and can be used in' balloons employed basically for load carrying functions such as for carrying scientific instruments aloft or can be Iused for man flight balloons.
Extending downwardly from the base of the balloon envelope are tapes or load lines 14 supporting a pay load 15.
The sheets or gores of the balloon, as illustrated by the two gores 11 and 12 in FIGURES 2 and 3 are formed of plural layers `with the outer layer being a scuif resistant fabric 16 and 18 `for the respective gores. The cloth or fabric may be various suitable materials, having a scuff resistance and tensile strength and beinfY of a light Weight, such as nylon, Daeron, Orion, polypropelene or other plastic or cotton materials. The inner layers 17 and 19 of the :gores are of a gas barrier lm preferably thermoplastic such as polyethylene, Mylar or other suitable lightweight gas impervious material. The layers 16 and 17, and 18 and 19 are preferably joined such as by a thermoplastic cement but need not be rmly bonded, although they may be laminated so as to be non-separable or in some instances can be formed of separate sheets superimposed upon each other. The inner layer forms a gas barrier and need not contribute tensile strength and therefore can be very thin and lightweight, while the outer layer provides the tensile strength and abrasion resistance for the balloon envelope, thereby avoiding the vulnerability to punctures and rips that is present with a balloon envelope made solely of thermoplastic material.
For seaming the edges of the gores, they are positioned as illustrated in FIGURE 2, and a narrow seam strip 2li is positioned therebetween.
The seam strip is doubled so that it edges 25 and 26 project in the same direction as the edges 27 and 28 of the gores. The seam strip is a lightweight thin gas impervious -film such as a thermoplastic, and can be polyethylene, Mylar or conveniently of the same material as the inner layers 17 and 19 of the balloon gores.
The edges of the seam strip 2d are joined to the inner surfaces of the gores by strip seams 21 and 22, FIGURES 2 and 3. This can conveniently be done by heat sealing devices shown at 23 for the seam 21 and at 24 for the seam 22. The heat sealing devices may be of known types such as rollers or heated air Sealers such as used for joining thermoplastic balloon materials.
The edges of the gores are next joined by sewing with a thread to form stitching 29, to form an envelope seam, as illustrated in FIGURES 3 and 4 in the finished form with the stitching being applied at the locations indicated by the arrows Sil in FIGURE 2. The stitching can be easily accomplished by a sewing machine after the edges 27 and 28 are brought together, and the entire seam may be formed in'a single operation, in a single pass through a machine. Also, for long balloon gores, a carriage may be provided supporting heat sealing equipment ahead of 3 a sewing machine with the carriage running along the edges ofthe gores.
VThe thread for forming the stitches Z9 may be any suitable thread, light in weight and having adequate tensile strength so that the sewn seam holds together the adjacent fabric gores with a strength approaching the original strength of the fabric. Lateral pulling on the seam may tend to spread the threads and separate the layers at the seam, but this is of no consequence insofar as the gas integrity of the seam'is concerned inasmuch as the escape of gas is positively prevented by the inner seam strip Ztl which lies along the inside of the balloon in the manner shown in FIGURE 3.
FIGURE 3 illustrates the condition of the seam in the balloon when the balloon is iniiated to form the balloon envelope. The iiexible seam strip Ztl will conform to the shape of the seam and the doubled over ends 3i and 32 and seams 2l and CL2 will form a gas barrier. The extra strip material against the gores aids in maintaining the integrity of the seals Zi and 22 and the spreading of the'gores is not acting to separate the seals 2li and 22. Therefore no leakage will occur and a gastight joint is provided.
lay the seam strip at against `the inner surface of the balloon envelope without the doubled over arrangement* illustrated in FGURE 3. While not essential, it is advantageous to use an abundance of strip material between the seams 2i and 22 so that the material can bulge and fold freely against the seam-33 without stress. In other Words, the width of seam strip material 2li between the seams 2l and 22 is greater than the distance between the seams 21 and 22 to provide a bulging of material preventing stresses on the materials.
It will be noted that in addition to providing a seal at the seam 33 the seam strip 2i) prevents gas from directly penetrating between the threads. ln some instances the seam strip will provide insulation if the outer skin is hot or cold relative to the gas within the balloon envelope.
Thus it will be seen that I have provided an improved balloon and balloon seam structure which meets the features, objectives and advantages above set forth. The seam is rapidly and easily made, and permits full utilization or" the advantages of balloon material formed or' combined fabric and gas impervious thermoplastic.
It will be understood that the sewn seam is not to be limited to the precise arrangement illustrated, although advantages are obtained in a strong seam which is simply made, but other seams of different sewn structures or seams not sewn may be employed.
The drawings and specification present a detailed disclosure of the preferred embodiments of the invention, and it is to be understood that the invention is not limited to the speciiic forms disclosed, but covers all modifications, changes and alternative constructions and methods fallin within the scope of the principles taught by the invention.
I claim as my invention:
1; A balloon construction comprising a balloon envelope having an outer layer of fabric material with a relatively high tensile strength, an inner layer of nonporous gas impervious material coextensive with the outer layer, a thread-stitched seam joining adjacent edges of the combinedrinner and outer layers to form a balloon envelope, a strip of non-porous gas impervious material Within the balloon over said seam, inhibiting the leakage of gas therethrough, and gas impervious str-ip seams joining the strip to the inner layer at each side of said stitched seam.
2. A balloon construction comprising a balloon envelope having an outer layer of fabric material with a relatively high tensile strength, an inner layer of a thermo- '4 plastic non-porous gas impervious material coextensiv with the outer layer, a stitched seam joining adjacent edges of the combined inner and outer layers to form a balloon envelope, a strip of lightweight thin thermoplastic material within the envelope over said seam inhibiting the leal'a of gas therethrough, and vertical gas impervious conL nuous heat seals forming strip seams attaching the strip to the inner layer at each side of the stitched seam.
3. The method of forming a seam between adjacent sheets of balloon envelope material with a seam strip comprising positioning one sheet over the other with the edges projecting outwardly in the same direction, doubling the seam strip and positioning it between the sheets with the edges projecting outwardly, forming first and second strip seams joining the edges of the strip to the sheets, and subsequentlyrjoining the edges of the sheets.
4. ln a balloon envelope having a seam joining adjacent portions or balloon material, a strip of gas impervious material positioned over the envelope seam, and strip seams attaching the strip to the balloon material at each side oi said envelope seam with said strip having a greater Width between the strip seams than the width of balloon material between said strip seams for an excess of strip material over'said envelope seam so that the strip will fold when pressed against the envelope seam, said width of strip material between said strip seams being sufficient so that space exists between the inner surface ofthe envelope seam and the strip when the strip is not pressed against the seam from pressure within the balloon envelope and so that the strip is not stressed in the direction of balloon material when forces on the balloon material stress said envelope seam.
5. The method of forming a seam between adjacent first and second sheets providing layers of balloon envelope material having inner and outer surfaces and a length of strip material comprising positioning first and second layers formed by the edges of the strip material adjacent the respective edges of the sheet layers against said inner surfaces of the sheet layers with the edges of the strip layers extending in the same direction as the edges of the sheet layers and joining the layers to form an envelope seam so that the strip will straddle said envclope seam when the sheet layers are drawn apart to be coplanar.
6. A balloon construction comprising a plurality of gores of material each joined to an adjacent gore by a stress sustaining gas pervious envelope seam to form a balloon envelope, and seam strips within the balloon envelope positioned over the envelope seams and each joined to the gores by a gas impervious seam to lie against the inner surface of the stress sustaining envelope seam and inhibit the leakage of gas through the envelope seam, said seam strips being substantially relaxed so that no stress is placed on the gas impervious seams when forces are applied on the gores and the envelope seams are stressed, and the strips are freely pressed against the inner surface of the balloon envelope with gas pressure therein.
7. In a balloon envelope having a gas pervious stress sustaining balloon envelope seam joining adjacent portions of balloon material, a layer of gas impervious seam barrier material positioned over the balloon envelope seam, and a supporting means for supporting said layer in place over the seam so that said barrier material forms a gas barrier against the inner surface of the balloon material at the sides of the envelope seam to inhibit the leakage of gas through the envelope seam, said layer being substantially relaxed so that no stress is placed on the supporting means when the envelope seams are stressed and the layer is freely pressed against the inner surface of the balloon envelope with gas pressure therein.
8. A balloon envelope having a longitudinalrballoon envelope seam joining adjacent portions of balloon material, a layer oi seam barrier material positioned over said balloon envelope seam, portions at the edges of said seam barirer material turned under and free of attachment to the envelope material adjacent the edges of the turned under portions so that the barrier material is free of stresses in a lateral direction, and means for supporting said layer of barrier material in place over the envelope seam to inhibit t'ne leakage of gas through the seam, said layer being free of stress in said lateral direction along the balloon material when forces are applied to said adjacent portions and the searn is under stress, and said layer freely pressed against the inner surface of the balloon envelope with gas pressure therein.
9. A balloon construction comprising a plurality of vertically extending balloon gores each joined to an adjacent gore by a gore seam to form a balloon envelope for containing a lifting gas, a vertical horizontally narrow strip over each of said seams within the balloon to prevent leakage through the seam, and means for supporting said vertical strip on the inner surface of the balloon, said narrow strip being free of stress in the direction of balloon gores when the balloon seam is stressed and said strip being freely pressed against the inner surface of the ballon with gas pressure within the balloon.
10. In a balloon envelope, adjacent sheets of balloon material joined by a balloon seam capable of withstanding tensile stresses on said sheets, and a layer of material positioned over said seam joined to said sheets by gas 6 proof seams incapable in itself of sustaining said tensile stresses and being impervious to gas, said layer being relaxed and unstressed and said gas proof seams being unstressed when said balloon seam is stressed and said layer freely pressed against the inner surface of the balloon envelope with gas pressure therein.
1l. in a balloon envelope, a seam structure comprising adjacent sheets of balloon material joined by stitching forming an envelope seam securing the edges of the sheets together, and a seam strip against said seam on the inner surrace of the balloon having side edges turned inwardly beneath the strip against the balloon material with said seam strip held against the envelope seam by pressure within the balloon, said turned luider side edges providing excess material so that said strip is unstressed in the direction of balloon material when said envelope seam is stressed.
References Cited in the le of this patent UNITED STATES PATENTS 2,441,087 Symer May 4, 1948 2,526,719 Winzen Oct. 24, 1950 2,633,172 Treiber Mar. 31, 1953 2,767,941 Gegner et al Oct. 23, 1956 2,993,663 Froehlich et al. July 25, 1961
Claims (1)
1. A BALLOON CONSTRUCTION COMPRISING A BALLOON ENVELOPE HAVING AN OUTER LAYER OF FABRIC MATERIAL WITH A RELATIVELY HIGH TENSILE STRENGTH, AN INNER LAYER OF NONPOROUS GAS IMPERVIOUS MATERIAL COEXTENSIVE WITH THE OUTER LAYER, A THREAD-STITCHED SEAM JOINING ADJACENT EDGES OF THE COMBINED INNER AND OUTER LAYERS TO FORM A BALLOON ENVELOPE, A STRIP OF NON-POROUS GAS IMPERVIOUS MATERIAL WITHIN THE BALLOON OVER SAID SEAM INHIBITING THE LEAKAGE OF GAS THERETHROUGH, AND GAS IMPERVIOUS STRIP SEAMS JOINING THE STRIP TO THE INNER LAYER AT EACH SIDE OF SAID STITCHED SEAM.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US125559A US3109611A (en) | 1961-07-20 | 1961-07-20 | Balloon seam structure and method of sealing balloon materials |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US125559A US3109611A (en) | 1961-07-20 | 1961-07-20 | Balloon seam structure and method of sealing balloon materials |
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| Publication Number | Publication Date |
|---|---|
| US3109611A true US3109611A (en) | 1963-11-05 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US125559A Expired - Lifetime US3109611A (en) | 1961-07-20 | 1961-07-20 | Balloon seam structure and method of sealing balloon materials |
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| Country | Link |
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| US (1) | US3109611A (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3182932A (en) * | 1963-08-30 | 1965-05-11 | Raven Ind Inc | Simulated variable thickness balloon |
| US3533865A (en) * | 1966-04-08 | 1970-10-13 | Centre Nat Etd Spatiales | Method for continuous welding of plastics sheets,in particular for use in the manufacture of exploratory balloons |
| US3664401A (en) * | 1969-10-24 | 1972-05-23 | Dodelino Sa | Method for the manufacture of inflated articles |
| US4084771A (en) * | 1975-03-27 | 1978-04-18 | Robert Armand Creuzet | Hot air aerostat |
| US4877205A (en) * | 1987-12-28 | 1989-10-31 | Winzen International, Inc. | High-altitude balloon and method and apparatus for making it |
| US9669918B1 (en) * | 2015-07-28 | 2017-06-06 | X Development Llc | Sealing ducts into a balloon |
| US10029776B1 (en) | 2015-09-18 | 2018-07-24 | X Development Llc | Seals for gored balloon |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2441087A (en) * | 1945-05-11 | 1948-05-04 | Gerald D Symer | Control surface cover |
| US2526719A (en) * | 1948-04-02 | 1950-10-24 | Gen Mills Inc | Balloon construction |
| US2633172A (en) * | 1948-11-01 | 1953-03-31 | Kenneth L Treiber | Flexible container |
| US2767941A (en) * | 1953-11-04 | 1956-10-23 | Gen Mills Inc | Seam for gored balloons |
| US2993663A (en) * | 1956-04-16 | 1961-07-25 | Gen Mills Inc | Gondola assembly |
-
1961
- 1961-07-20 US US125559A patent/US3109611A/en not_active Expired - Lifetime
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2441087A (en) * | 1945-05-11 | 1948-05-04 | Gerald D Symer | Control surface cover |
| US2526719A (en) * | 1948-04-02 | 1950-10-24 | Gen Mills Inc | Balloon construction |
| US2633172A (en) * | 1948-11-01 | 1953-03-31 | Kenneth L Treiber | Flexible container |
| US2767941A (en) * | 1953-11-04 | 1956-10-23 | Gen Mills Inc | Seam for gored balloons |
| US2993663A (en) * | 1956-04-16 | 1961-07-25 | Gen Mills Inc | Gondola assembly |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3182932A (en) * | 1963-08-30 | 1965-05-11 | Raven Ind Inc | Simulated variable thickness balloon |
| US3533865A (en) * | 1966-04-08 | 1970-10-13 | Centre Nat Etd Spatiales | Method for continuous welding of plastics sheets,in particular for use in the manufacture of exploratory balloons |
| US3664401A (en) * | 1969-10-24 | 1972-05-23 | Dodelino Sa | Method for the manufacture of inflated articles |
| US4084771A (en) * | 1975-03-27 | 1978-04-18 | Robert Armand Creuzet | Hot air aerostat |
| US4877205A (en) * | 1987-12-28 | 1989-10-31 | Winzen International, Inc. | High-altitude balloon and method and apparatus for making it |
| US9669918B1 (en) * | 2015-07-28 | 2017-06-06 | X Development Llc | Sealing ducts into a balloon |
| US10472040B1 (en) | 2015-07-28 | 2019-11-12 | Loon Llc | Sealing ducts into a balloon |
| US10029776B1 (en) | 2015-09-18 | 2018-07-24 | X Development Llc | Seals for gored balloon |
| US10173764B1 (en) * | 2015-09-18 | 2019-01-08 | Loon Llc | Seals for gored balloon |
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