IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0912120
(2001-07-23)
|
발명자
/ 주소 |
|
대리인 / 주소 |
Chan, Raymond Y.David and Raymond Patent Group
|
인용정보 |
피인용 횟수 :
8 인용 특허 :
6 |
초록
▼
A universal accessory adapter, which is adapted for attaching to a collapsible outdoor furniture, includes a supporting device for rigidly supporting an accessory item, at least a connector for detachably attaching the supporting device to a frame leg of the collapsible outdoor furniture, and a fold
A universal accessory adapter, which is adapted for attaching to a collapsible outdoor furniture, includes a supporting device for rigidly supporting an accessory item, at least a connector for detachably attaching the supporting device to a frame leg of the collapsible outdoor furniture, and a foldable frame arranged for selectively folding the supporting device from a folded position to an unfolded position. In which, in the folded position, the supporting device is moved to a position close to the frame leg of the collapsible outdoor furniture, and in the unfolded position, the supporting device is moved away from the frame leg of the collapsible outdoor furniture, so as to spacedly mount the supporting device with respect to the frame leg of the collapsible outdoor furniture. Therefore, the universal accessory is substantially supported by the collapsible outdoor furniture, so as to rigidly support the accessory item on the universal accessory adapter.
대표청구항
▼
A universal accessory adapter, which is adapted for attaching to a collapsible outdoor furniture, includes a supporting device for rigidly supporting an accessory item, at least a connector for detachably attaching the supporting device to a frame leg of the collapsible outdoor furniture, and a fold
A universal accessory adapter, which is adapted for attaching to a collapsible outdoor furniture, includes a supporting device for rigidly supporting an accessory item, at least a connector for detachably attaching the supporting device to a frame leg of the collapsible outdoor furniture, and a foldable frame arranged for selectively folding the supporting device from a folded position to an unfolded position. In which, in the folded position, the supporting device is moved to a position close to the frame leg of the collapsible outdoor furniture, and in the unfolded position, the supporting device is moved away from the frame leg of the collapsible outdoor furniture, so as to spacedly mount the supporting device with respect to the frame leg of the collapsible outdoor furniture. Therefore, the universal accessory is substantially supported by the collapsible outdoor furniture, so as to rigidly support the accessory item on the universal accessory adapter. back into an aft portion of said by-pass passage. 6. An integrated aircraft system according to claim 5, wherein during flight said fan compresses said air before said air enters said secondary gas turbine engine. 7. An integrated aircraft system comprising an aircraft frame, a nacelle cowl mounted to said aircraft frame, a primary gas turbine engine mounted within said nacelle cowl, a secondary power system incorporated within said nacelle cowl and being driven by a flow of air created by or through said primary gas turbine engine, an electrical power and cooling unit for supplying electrical power and cabin cooling air, said electrical power and cooling unit being pneumatically driven by engine bleed air, said electrical power and cooling unit having a shaft and a power turbine, an electrical generator, and a cooling turbine mounted on said shaft, said power turbine and said cooling turbine being supplied with bleed air from said primary gas turbine engine, and said primary gas turbine engine having two bleed ports for delivering at least one of high temperature, high pressure high stage bleed air and mid-stage bleed air to said electrical power and cooling unit. 8. An integrated aircraft system comprising an aircraft frame, a nacelle cowl mounted to said aircraft frame, a primary gas turbine engine mounted within said nacelle cowl, a secondary power system incorporated within said nacelle cowl and being driven by a flow of air created by or through said primary gas turbine engine, an electrical power and cooling unit for supplying electrical power and cabin cooling air, said electrical power and cooling unit being pneumatically driven by engine bleed air, said electrical power and cooling unit having a shaft and a power turbine, an electrical generator, and a cooling turbine mounted on said shaft, a fan positioned within a ram air duct, said fan being mounted to said shaft, a first heat exchanger means for cooling bleed air from said primary gas turbine engine and secondary heat exchanger means for removing heat from said bleed air exiting said first heat exchanger means. 9. An integrated aircraft system according to claim 8, wherein said secondary heat exchanger means is positioned within said ram air duct. 10. An integrated aircraft system according to claim 8, wherein bleed air exiting from said secondary heat exchanger means is delivered to said cooling turbine at altitudes above 30,000 feet and said cooling turbine drives said shaft and said generator. 11. An integrated aircraft system according to claim 10, wherein said bleed air is supplied to said power turbine when said cooling turbine does not generate sufficient power. 12. An integrated aircraft system according to claim 8, further comprising means for receiving air exiting from said secondary heat exchanger means and for drying said air and means for supplying said dried air to said cooling turbine. 13. An integrated aircraft system according to claim 12, further comprising means for delivering air exiting said c
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