다음과 같은 기능을 한번의 로그인으로 사용 할 수 있습니다.NTIS 바로가기
다음과 같은 기능을 한번의 로그인으로 사용 할 수 있습니다.DataON 바로가기
다음과 같은 기능을 한번의 로그인으로 사용 할 수 있습니다.Edison 바로가기
다음과 같은 기능을 한번의 로그인으로 사용 할 수 있습니다.Kafe 바로가기
|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/117R ; 244/123 ; 244/119|
|발명자 / 주소||
|출원인 / 주소||
|인용정보||피인용 횟수 : 17 인용 특허 : 0|
A design and construction method, for a graduated series of aircraft of various sizes, in which development costs are minimized by maintaining a consistent scale configuration from model to model, and production costs are minimized through the use of a universal tooling concept for the manufacturing of detail parts, subsassemblies and components of the airframes. For each model (M11, M12 . . . M1n) of a series size-graduated elements such as the main wing airfoils (31, 32, 33) are designed with similar characteristics and overlapping dimensions. A common...
A method for economically constructing a size-graduated range of airframes characterized by a generally similar profile wherein each of a plurality of airfoils and other sub-assemblies in each of said airframes comprises a plurality of series of size-graduated but otherwise generally identical components and wherein each component Cxy is characterized by a basic dimension Dxy from which all other measurements of said components can be derived wherein x indicates a size of airframe in said range and y indicates a size of component in said series; which co...