|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/42DA ; 244/113|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 47 인용 특허 : 0|
An aircraft wing having a relatively thin airfoil cross section including a main body portion and a plurality of auxiliary airfoil sections disposed at the trailing edge of the wing and movable relative to the main body portion and to one another. In a normal cruise position the auxiliary sections and the main body portion form a complete airfoil having a substantially contiguous and unbroken exterior airfoil surface which preserves the high speed characteristics of the wing. At least two of the auxiliary sections comprising a leading auxiliary section a...
An aircraft wing comprising in combination a main body portion, a plurality of movable auxiliary sections disposed at the trailing edge of said main body portion, said movable auxiliary sections comprising a leading auxiliary section and a trailing auxiliary section, hinge means operably connecting said auxiliary sections and said main body portion, said hinge means including a fixed hinge member disposed on said main body portion and connecting said leading and trailing auxiliary sections to the main body portion, said leading and trailing auxiliary sec...