[특허]Airframe display systems and methods

Skyline Displays, Inc.

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()	우선순위가 가장 높은 연산자	예1) (나노 (기계 \| machine))
공백	두 개의 검색어(식)을 모두 포함하고 있는 문서 검색	예1) (나노 기계) 예2) 나노 장영실
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내보내기 페이스북 공유 트위터 공유 카카오톡 공유

Airframe display systems and methods

특허상세정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	G09F-015/00 G09F-013/02 G09F-013/04
출원번호	US-0355442 (2012-10-26)
등록번호	US-9355581 (2016-05-31)
국제출원번호	PCT/US2012/062034 (2012-10-26)
국제공개번호	WO2013/066738 (2013-05-10)
발명자 / 주소	Lindblom, Curtis H. Elliott, John Sommerville, Jim Nelson, Nathaniel J.
출원인 / 주소	Skyline Displays, Inc.
대리인 / 주소	Oppold, Thomas J.
인용정보	피인용 횟수 : 0 인용 특허 : 36

초록

An airframe display system and method. The airframe display system has an airtight airframe having at least one airbeam. The airbeam has a sleeve of dimensionally stable material. A stretch fabric cover is received over the airframe whereby, upon inflation, the airframe is substantially rigid and the stretch fabric cover is taut over the airframe defining a display surface area.

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1. A display system, comprising: a stretch fabric cover forming an enclosure having a predetermined configuration and predetermined dimensions when in a non-stretched condition, said enclosure further having a front surface area and a back surface area, said enclosure further having an opening providing access to an interior of said enclosure;an airtight inflatable airframe having an inflated condition and a non-inflated condition, said airframe received within said interior of said enclosure through said opening when in said non-inflated condition, said airframe comprising at least one airbeam, said at least one airbeam comprising a sleeve of dimensionally stable material defining a predetermined sleeve dimension, said predetermined sleeve dimension defining a depth of said airframe, said airframe, when in said inflated condition, configured to have a shape corresponding to said predetermined configuration of said enclosure, said airframe, when in said inflated condition having dimensions greater than said dimensions of said enclosure when in said non-stretched condition;whereby, when in said inflated condition, said airframe is substantially rigid and said stretch fabric cover is drawn taut over said airframe such that said front surface area and said back surface area of said stretch fabric cover are substantially smooth and spaced a distance apart by said predetermined sleeve dimension. 2. The display system of claim 1 wherein said at least one airbeam has an airtight air bladder. 3. The display system of claim 2 wherein said airtight air bladder is removable from said sleeve. 4. The display system of claim 3 wherein said sleeve includes an opening for removing said removable air bladder, said opening having a closing means. 5. The display system of claim 1 wherein said airtight airframe comprises a plurality of airbeams, each of said plurality of airbeams comprising a sleeve of dimensionally stable material. 6. The display system of claim 5 wherein each of said plurality of airbeams has an airtight air bladder. 7. The display system of claim 6 wherein each of said airbladders are fluidly connected by tubular jumpers. 8. The display system of claim 1 wherein said airtight airframe comprises a plurality of modular airtight airframes, each of said plurality of modular airtight airframes having an airbeam comprising a sleeve of dimensionally stable material. 9. The display system of claim 8 wherein each of said airbeam of said plurality of modular airframes has an airtight bladder. 10. The display system of claim 9 wherein each of said air bladders of said airbeams are fluidly connected by tubular jumpers. 11. The display system of claim 8 wherein said plurality of modular airframes are secured together at adjacent ends. 12. The display system of claim 8 wherein said plurality of modular airframes are secured together by said stretch fabric cover enclosure. 13. The display system of claim 12 wherein said modular airframes, when inflated, together with said stretch fabric cover enclosure, define a three dimensional shape. 14. The display system of claim 13 wherein said front and back surface areas of each of said plurality of separate stretch fabric cover enclosures are substantially planar. 15. The display system of claim 13 wherein at least one of said plurality of modular airframes is curvilinear. 16. The display system of claim 13 wherein at least one of said plurality of modular airframes includes a curvilinear side. 17. The display system of claim 8 wherein said stretch fabric cover enclosure comprises a plurality of separate stretch fabric cover enclosures each received over one of said plurality of modular airframes. 18. The display system of claim 17 wherein said separate stretch fabric cover enclosures are secured together at adjacent ends with one of said adjacent ends of said stretch fabric cover enclosures has a first partial zipper element and another of said adjacent ends of said stretch fabric cover enclosures has a second partial zipper element, whereby said first and second partial zipper elements cooperate to form a complete zipper such that said adjacent ends of said stretch fabric covers enclosures removably zip together. 19. The display system of claim 1 wherein said stretch fabric cover enclosure comprises at least two layers with one of said layers being substantially opaque. 20. The display system of claim 1 wherein said stretch fabric cover enclosure comprises at least three layers with one of said layers being substantially opaque. 21. The display system of claim 1 wherein said stretch fabric cover enclosure comprises an intermediate stretch fabric cover enclosure and a stretch fabric display panel; said stretch fabric display panel removably attachable to said intermediate stretch fabric cover enclosure, said stretch fabric display panel comprising said front surface area. 22. The display system of claim 21 wherein said intermediate stretch fabric cover enclosure includes a substantially opaque surface. 23. The display system of claim 22 wherein said intermediate stretch fabric cover enclosure has a first partial zipper element and said stretch fabric display panel has a second partial zipper element, wherein said first and second partial zipper elements cooperate to form a complete zipper such that said stretch fabric display panel removably zips to said intermediate stretch fabric cover enclosure. 24. The display system of claim 21 wherein said intermediate stretch fabric cover enclosure has a first partial zipper element and said stretch fabric display panel has a second partial zipper element, wherein said first and second partial zipper elements cooperate to form a complete zipper such that said stretch fabric display panel removably zips to said intermediate stretch fabric cover enclosure. 25. The display system of claim 1 wherein said airframe, when inflated, together with said stretch fabric cover enclosure, defines a substantially two dimensional shape wherein length and height dimensions of said airframe when in said inflated condition is substantially greater than said sleeve dimension. 26. The display system of claim 25 wherein said front and back surface areas are substantially planar. 27. The display system of claim 25 wherein said front and back surface areas are curvilinear. 28. The display system of claim 25 wherein said airframe includes at least one curvilinear side. 29. The display system of claim 1 further comprising LED lighting secured to said airframe, said LED lighting units connected to a power source whereby said front surface area of said stretch fabric cover enclosure is illuminated by said LED lighting units. 30. The display system of claim 1 further comprising LED lighting units secured to said stretch fabric cover enclosure, said LED lighting units connected to a power source whereby said front surface area is illuminated by said LED lighting units. 31. The display system of claim 1 further comprising an inflator. 32. The display system of claim 31 wherein said inflator is a compressed air tank. 33. The display system of claim 31 wherein said inflator is an air pump. 34. The display system of claim 1 wherein said airframe is inflated to a pressure between a range of about 1 psi to about 15 psi. 35. The display system of claim 34 wherein said airbeam includes at least one air port for inflating and deflating said airframe, said air port having sufficient volumetric capacity such that upon opening said at least one air port, said airframe will deflate from a pressure of about 15 psi to a pressure of about 1 psi in about 10 seconds. 36. The display system of claim 35 wherein said at least one air port includes a spring biased valve that is movable between a closed position and an open position, and wherein said valve is lockable in said open position for deflation of said airframe. 37. The display system of claim 1 further including an accessory mount for mounting an accessory to said at least one airbeam of said airframe, said accessory mount comprising a removable sleeve of dimensionally stable fabric with a closing means for removably but fixably securing said accessory mount to said at least one airbeam. 38. The display system of claim 37 wherein said removable sleeve comprises a pocket for receiving an accessory mounting bracket. 39. The display system of claim 37 wherein said removable sleeve includes a metal plate and said accessory mount further comprises a spacer member having first and second magnetic ends, whereby said spacer member is magnetically supported at said first magnetic end from said metal plate and wherein said accessory is magnetically supported from said second magnetic end. 40. The display of claim 37 wherein said accessory is a monitor. 41. The display of claim 37 wherein said accessory is a shelf. 42. The display system of claim 37 wherein said accessory is a second airframe display system comprising: an airtight airframe having at least one airbeam comprising a sleeve of dimensionally stable material; anda stretch fabric cover received over said airframe;whereby, upon inflation, said airframe is substantially rigid and said stretch fabric cover is taut over said airframe defining a front surface area. 43. The display system of claim 1 further comprising a compression sack, said compression sack capable of compressing said deflated airframe display system such that said display system, when deflated and compressed, is entirely received and stored within said compression sack. 44. The display system of claim 43 wherein said compression sack is capable of compressing said deflated airframe display system into a size that will fit into an airline carry-on baggage size together with an inflator. 45. The display system of claim 1 further comprising a storage case having a compression system, said compression system capable of compressing said deflated airframe display system such that said display system, when deflated and compressed, is entirely received and stored within said storage case. 46. The display system of claim 45 wherein said storage case is an airline carry-on baggage size. 47. A display method comprising the steps of: a) placing an airframe display system on a surface, said airframe display system comprising: i) a stretch fabric cover forming an enclosure having a predetermined configuration and predetermined dimensions when in a non-stretched condition, said enclosure further having a front surface area and a back surface area, said enclosure further having an opening providing access to an interior of said enclosure;ii) an airtight inflatable airframe having an inflated condition and a non-inflated condition, said airframe received within said interior of said enclosure through said opening when in said non-inflated condition, said airframe comprising at least one airbeam, said at least one airbeam comprising a sleeve of dimensionally stable material defining a predetermined sleeve dimension, said predetermined sleeve dimension defining a depth of said airframe, said airframe, when in said inflated condition, configured to have a shape corresponding to said predetermined configuration of said enclosure, said airframe, when in said inflated condition having dimensions greater than said dimensions of said enclosure when in said non-stretched condition;b) attaching an inflator to an air port on said at least one airbeam;c) inflating said airframe to said inflated condition with said inflator until said airframe is substantially rigid and said stretch fabric cover is drawn taut over said airframe such that said front surface area and said back surface area of said stretch fabric cover are substantially smooth and spaced a distance apart by said predetermined sleeve dimension. 48. The method of claim 47 wherein said at least one airbeam has an airtight air bladder. 49. The method of claim 48 wherein said airtight air bladder is removable from said sleeve. 50. The method of claim 49 wherein said sleeve includes an opening for removing said removable air bladder, said opening having a closing means. 51. The method of claim 48 wherein said airtight airframe comprises a plurality of airbeams, each of said plurality of airbeams comprising a sleeve of dimensionally stable material. 52. The method of claim 51 wherein each of said plurality of airbeams has an airtight air bladder. 53. The method of claim 52 wherein each of said airbladders are fluidly connected by tubular jumpers. 54. The method of claim 47 wherein said airtight airframe comprises a plurality of modular airtight airframes, each of said plurality of modular airtight airframes having an airbeam comprising a sleeve of dimensionally stable material. 55. The method of claim 54 wherein each of said airbeams of said plurality of modular airframes has an airtight bladder. 56. The method of claim 55 wherein each of said air bladders of said airbeams are fluidly connected by tubular jumpers. 57. The method of claim 54 further comprising the step of securing said plurality of modular airframes together at adjacent ends. 58. The method of claim 54 further comprising the step of securing said plurality of modular airframes together by said stretch fabric cover enclosure. 59. The method of claim 58 wherein said modular airframes, when inflated, together with said stretch fabric cover enclosure, define a three dimensional shape. 60. The method of claim 59 wherein said front and back surface areas of each of said plurality of separate stretch fabric cover enclosures are substantially planar. 61. The method of claim 59 wherein at least one of said plurality of modular airframes is curvilinear. 62. The method of claim 59 wherein said at least one of said plurality of modular airframes includes a curvilinear side. 63. The method of claim 54 wherein said stretch fabric cover enclosure comprises a plurality of separate stretch fabric cover enclosures each received over one of said plurality of modular airframes, said method further comprising the step of securing each of said stretch fabric covers enclosures together at adjacent ends. 64. The method of claim 63 wherein one of said adjacent ends of said stretch fabric cover enclosures has a first partial zipper element and another of said adjacent ends of said stretch fabric cover enclosures has a second cooperating partial zipper element, said method further comprising the step of zipping said first and second partial zipper elements together. 65. The method of claim 47 wherein said stretch fabric cover enclosure comprises at least two layers with one of said layers being substantially opaque. 66. The method of claim 47 wherein said stretch fabric cover enclosure comprises at least three layers with one of said layers being substantially opaque. 67. The method of claim 47 wherein said stretch fabric cover enclosure comprises an intermediate stretch fabric cover and a stretch fabric display panel, said stretch fabric display panel comprising said front surface area, said method further comprising the step of attaching said stretch fabric display panel to said intermediate stretch fabric cover enclosure. 68. The method of claim 67 wherein said intermediate stretch fabric cover enclosure includes a substantially opaque surface. 69. The method of claim 68 wherein said intermediate stretch fabric cover enclosure has a first partial zipper element and said stretch fabric display panel has a second cooperating partial zipper element, wherein said attaching step comprises zipping said stretch fabric display panel to said intermediate stretch fabric cover enclosure. 70. The method of claim 67 wherein said intermediate stretch fabric cover enclosure has a first partial zipper element and said stretch fabric display panel has a second cooperating partial zipper element, wherein said attaching step comprises zipping said stretch fabric display panel to said intermediate stretch fabric cover enclosure. 71. The method of claim 47 wherein said airframe, when inflated, together with said stretch fabric cover enclosure, defines a substantially two dimensional shape wherein length and height dimensions of said airframe, when in an inflated condition, is substantially greater than said predetermined sleeve dimension. 72. The method of claim 71 wherein said front and back surface areas are substantially planar. 73. The method of claim 71 wherein said front and back surface areas are curvilinear. 74. The method of claim 71 wherein said airframe includes at least one curvilinear side. 75. The method of claim 47 further including the steps of illuminating said front surface area. 76. The method of claim 75 wherein the step of illuminating said front surface area includes securing LED lighting units to said airframe and electrically connecting said LED lighting units to a power source. 77. The method of claim 75 wherein the step of illuminating said front surface area includes securing LED lighting units to said stretch fabric cover enclosure and electrically connecting said LED lighting units to a power source. 78. The method of claim 47 wherein said inflator is a compressed air tank. 79. The method of claim 47 wherein said inflator is an air pump. 80. The method of claim 47 wherein said airframe is inflated to a pressure between a range of about 1 psi to about 15 psi. 81. The method of claim 47 further comprising the step of deflating said airframe display system by locking a spring biased valve of said air port in an open position. 82. The method of claim 81 wherein said air port has sufficient volumetric capacity such that upon locking said valve in said open position, said airframe will deflate from a pressure of about 15 psi to a pressure of about 1 psi in about 10 seconds. 83. The method of claim 47 further comprising the step of deflating said airframe display and compressing said deflated airframe display system with a compression sack and storing said deflated and compressed airframe display system within said compressions sack. 84. The method of claim 83 wherein said compression sack is capable of compressing said airframe display to fit into an airline carry-on baggage. 85. The method of claim 47 further comprising the step of deflating said airframe display and storing said deflated airframe into a storage case having a compression system, said compression system capable of compressing said deflated airframe display system such that said display system, when deflated and compressed, is entirely received and stored within said storage case, said storage case meeting airline carry-on baggage size limits. 86. The method of claim 47 further comprising attaching an accessory mount to said at least one airbeam of said airframe for mounting an accessory, said accessory mount comprising a removable sleeve of dimensionally stable fabric with a closing means for removably but fixably securing said accessory mount to said at least one airbeam. 87. The method of claim 86 wherein said removable sleeve comprises a pocket for receiving an accessory mounting bracket. 88. The method of claim 86 wherein said removable sleeve includes a metal plate and said accessory mount further comprises a spacer member having first and second magnetic ends, whereby said spacer member is magnetically supported at said first magnetic end from said metal plate and wherein said accessory is magnetically supported from said second magnetic end. 89. The method of claim 86 wherein said accessory is a monitor. 90. The method of claim 86 wherein said accessory is a shelf. 91. The method of claim 86 wherein said accessory is a second airframe display system comprising: an airtight airframe having at least one airbeam comprising a sleeve of dimensionally stable material; anda stretch fabric cover received over said airframe;whereby, upon inflation, said airframe is substantially rigid and said stretch fabric cover is taut over said airframe defining a front surface area.

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