IPC분류정보
국가/구분 |
United States(US) Patent
등록
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국제특허분류(IPC7판) |
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출원번호 |
US-0826031
(2001-04-04)
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발명자
/ 주소 |
- Page, Mark A.
- Whitlock, Jennifer P.
- Wilks, Matthew W.
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출원인 / 주소 |
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대리인 / 주소 |
Harness Dickey & Pierce P.L.C.
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인용정보 |
피인용 횟수 :
24 인용 특허 :
8 |
초록
▼
A blended wing body aircraft having a modular body. In one embodiment, the configuration or cargo capacity of the aircraft can be varied by adding or subtracting intermediate body structures rather than by adding or subtracting segments from the lateral sides of the aircraft body. Configuration in t
A blended wing body aircraft having a modular body. In one embodiment, the configuration or cargo capacity of the aircraft can be varied by adding or subtracting intermediate body structures rather than by adding or subtracting segments from the lateral sides of the aircraft body. Configuration in this manner preserves key aerodynamic parameters and permits several major components to be used in several aircraft configurations, each of which having a different cargo capacity. In another embodiment, the aircraft is formed from a plurality of laterally-extending body structures. Changes to the cargo capacity of the aircraft is accomplished through the employment of body structures that are wider or narrower. Configuration in this manner provides the aircraft with a structure that is relatively strong and efficient. While the body structures of this embodiment are not shared across a family of variously sized aircraft, the base design of the body structures is readily modifiable to adjust for an increase or decrease in width associated with a desired change to the aircraft's cargo capacity.
대표청구항
▼
A blended wing body aircraft having a modular body. In one embodiment, the configuration or cargo capacity of the aircraft can be varied by adding or subtracting intermediate body structures rather than by adding or subtracting segments from the lateral sides of the aircraft body. Configuration in t
A blended wing body aircraft having a modular body. In one embodiment, the configuration or cargo capacity of the aircraft can be varied by adding or subtracting intermediate body structures rather than by adding or subtracting segments from the lateral sides of the aircraft body. Configuration in this manner preserves key aerodynamic parameters and permits several major components to be used in several aircraft configurations, each of which having a different cargo capacity. In another embodiment, the aircraft is formed from a plurality of laterally-extending body structures. Changes to the cargo capacity of the aircraft is accomplished through the employment of body structures that are wider or narrower. Configuration in this manner provides the aircraft with a structure that is relatively strong and efficient. While the body structures of this embodiment are not shared across a family of variously sized aircraft, the base design of the body structures is readily modifiable to adjust for an increase or decrease in width associated with a desired change to the aircraft's cargo capacity. 4, 19961000, Frazier; US-5588615, 19961200, Batts; US-D377284, 19970100, Farrow et al.; US-5598987, 19970200, Wachowicz; US-5604992, 19970200, Robinson; US-5605250, 19970200, Meiron et al.; US-5609269, 19970300, Behnke et al.; US-5618008, 19970400, Dearwester et al.; US-5620148, 19970400, Mitchell; US-5624025, 19970400, Hixon; US-5630526, 19970500, Moody; US-5630563, 19970500, Meisner et al.; US-5631317, 19970500, Komatsu et al.; US-5642810, 19970700, Warner et al.; US-5649676, 19970700, Lord; US-D381851, 19970800, Sharpe; US-5653403, 19970800, Ritchey; US-5655661, 19970800, Rigby; US-5660313, 19970800, Newbold; US-5660636, 19970800, Shangold et al.; US-5667092, 19970900, Julius et al.; US-5669576, 19970900, Moody; US-5672206, 19970900, Gorman; US-D386025, 19971100, Mervar et al.; US-5687875, 19971100, Watts et al.; US-D387590, 19971200, Cameron et al.; US-5697576, 19971200, Bloch et al.; US-5697577, 19971200, Ogden; US-5704565, 19980100, Cheng; US-5704566, 19980100, Schutz et al.; US-5765717, 19980600, Gottselig; US-D397265, 19980800, Badillo; US-RE35976, 19981200, Gasparrini et al.; US-5848762, 19981200, Reinheimer et al.; US-5868275, 19990200, Moody; US-5868335, 19990200, Lebrun; US-5868344, 19990200, Melnick; US-5868345, 19990200, Beisser; US-5868346, 19990200, Cobos; US-5868347, 19990200, Paul et al.; US-5875985, 19990300, Cohen et al.; US-5887759, 19990300, Ayigbe; US-5887818, 19990300, Kelley; US-5893531, 19990400, Taylor et al.; US-5897074, 19990400, Marino; US-5901921, 19990500, Perlsweig; US-5904316, 19990500, Dunning et al.; US-5914177, 19990600, Smith, III et al.; US-5924617, 19990700, LaCount et al.; US-D412439, 19990800, Cormack; US-5938013, 19990800, Palumbo et al.; US-5950960, 19990900, Marino; US-5951762, 19990900, Shangold et al.; US-5958187, 19990900, Bhat et al.; US-5964351, 19991000, Zander; US-5967452, 19991000, Wilder; US-5971138, 19991000, Soughan; US-5971142, 19991000, Jones; US-D416794, 19991100, Cormack; US-D417109, 19991100, Johnson et al.; US-5979821, 19991100, LaCount et al.; US-5992718, 19991100, Zaranck; US-D417987, 1999
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