System and method for affixing gateboxes to an aircraft
원문보기
IPC분류정보
국가/구분 |
United States(US) Patent
등록
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국제특허분류(IPC7판) |
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출원번호 |
US-0078286
(2011-04-01)
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등록번호 |
US-8579234
(2013-11-12)
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발명자
/ 주소 |
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출원인 / 주소 |
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대리인 / 주소 |
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인용정보 |
피인용 횟수 :
2 인용 특허 :
1 |
초록
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A system for affixing a gatebox to an aircraft includes a first type of gatebox operable to release material from an aircraft, a second type of gatebox operable to release material from the aircraft, a frame coupled to the aircraft operable to receive a selected one of the first type of gatebox and
A system for affixing a gatebox to an aircraft includes a first type of gatebox operable to release material from an aircraft, a second type of gatebox operable to release material from the aircraft, a frame coupled to the aircraft operable to receive a selected one of the first type of gatebox and the second type of gatebox; and a plurality of fastenings operable to secure the selected one of the first type of gatebox and the second type of gatebox to the frame.
대표청구항
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1. A system for affixing a gatebox to an aircraft, comprising: a first type of gatebox operable to release material from an aircraft;a second type of gatebox operable to release material from the aircraft;a frame coupled to the aircraft operable to receive a selected one of the first type of gatebox
1. A system for affixing a gatebox to an aircraft, comprising: a first type of gatebox operable to release material from an aircraft;a second type of gatebox operable to release material from the aircraft;a frame coupled to the aircraft operable to receive a selected one of the first type of gatebox and the second type of gatebox;a compressible seal operable to create a barrier between the frame and the selected one of the first type of gatebox and the second type of gatebox; anda plurality of fastenings operable to secure the selected one of the first type of gatebox and the second type of gatebox to the frame. 2. The system of claim 1, wherein the compressible seal is coupled to the frame. 3. The system of claim 1, wherein the compressible seal is coupled to the selected one of the first type of gatebox and the second type of gatebox. 4. The system of claim 1, further comprising a cart comprising: a gatebox support operable to secure a gatebox; anda lift operable to vertically move the gatebox. 5. The system of claim 1, wherein the plurality of fastenings are latches. 6. The system of claim 1, further comprising a controller coupled to at least one of the aircraft, the selected one of the first type of gatebox and the second type of gatebox, and a sensor, wherein the controller is operable to receive signals to control the selected one of the first type of gatebox and the second type of gatebox. 7. The system of claim 1, further comprising a fairing operable to affix to at least one of the aircraft and the selected one of the first type of gatebox and the second type of gatebox, and further operable to change airflow around the selected one of the first type of gatebox and the second type of gatebox coupled to the aircraft. 8. The system of claim 1, further comprising: a seal housing structure adapted to house the compressible seal; anda seal compression structure adapted to mate to the seal housing structure, wherein when the plurality of fastenings secure the selected one of the first type of gatebox and the second type of gatebox to the frame, the seal compression structure mates with the seal housing structure and compresses the compressible seal against the seal housing structure. 9. An apparatus for affixing a gatebox to an aircraft, comprising: a frame affixable to an aircraft, wherein the frame is operable to receive a first type of gatebox and a second type of gatebox;a compressible seal operable to create a barrier between the frame and a selected one of the first type of gatebox and the second type of gatebox; anda plurality of fastenings operable to couple the selected one of the first type of gatebox and the second type of gatebox to the frame. 10. The apparatus of claim 9, wherein the compressible seal is coupled to the frame. 11. The apparatus of claim 9, wherein the compressible seal is coupled to the selected one of the first type of gatebox and the second type of gatebox. 12. The apparatus of claim 9, wherein the plurality of fastenings are latches. 13. The apparatus of claim 9, further comprising: a seal housing structure adapted to house the compressible seal; anda seal compression structure adapted to mate to the seal housing structure, wherein when the plurality of fastenings secure the selected one of the first type of gatebox and the second type of gatebox to the frame, the seal compression structure mates with the seal housing structure and compresses the compressible seal against the seal housing structure. 14. A method for affixing a gatebox to an aircraft, comprising: providing a first type of gatebox operable to release material from an aircraft;providing a second type of gatebox operable to release material from the aircraft;coupling a frame operable to receive a selected one of the first type of gatebox and the second type of gatebox to the aircraft;providing a compressible seal to create a barrier between the frame and the selected one of the first type of gatebox and the second type of gatebox;providing a plurality of fastenings operable to secure the selected one of the first type of gatebox and the second type of gatebox to the frame; andsecuring the selected one of the first type of gatebox and the second type of gatebox to the frame with the fastenings. 15. The method of claim 14, wherein the barrier is a water-proof barrier. 16. The method of claim 14, further comprising providing a cart to secure a gatebox and to vertically move the gatebox. 17. The method of claim 14, wherein the plurality of fastenings are latches. 18. The method of claim 14, further comprising providing a controller to receive signals to control the selected one of the first type of gatebox and the second type of gatebox. 19. The method of claim 14, further comprising providing a fairing to change airflow around the selected one of the first type of gatebox and the second type of gatebox coupled to the aircraft. 20. The method of claim 14, further comprising: providing a seal housing structure adapted to house the compressible seal; andproviding a seal compression structure adapted to mate to the seal housing structure, wherein when the plurality of fastenings secure the selected one of the first type of gatebox and the second type of gatebox to the frame, the seal compression structure mates with the seal housing structure and compresses the compressible seal against the seal housing structure.
이 특허에 인용된 특허 (1)
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Fima, Raoul G.; Gagliano, Thomas; Pope, Ralph E., Liquid dispensing lighter-than-air airship system.
이 특허를 인용한 특허 (2)
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Thompson, Larry D., Sliding door gatebox and detachable seeder plate.
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Thompson, Larry D., System and method for affixing gateboxes to an aircraft.
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