|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/217; 244/218; 244/076.0R; 244/099.4|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 12 인용 특허 : 225|
Systems and methods for providing differential motion to wing high lift devices are disclosed. A system in accordance with one embodiment of the invention includes a wing having a leading edge, a trailing edge, a first deployable lift device with a first spanwise location, and a second deployable lift device with a second spanwise location different than the first. The wing system can further include a drive system having a drive link operatively coupleable to both the first and second deployable lift devices, and a control system operatively coupled to ...
We claim: 1. An aircraft wing system, comprising: a wing having a leading edge and a trailing edge; a first deployable lift device having a first spanwise location and being movable relative to the wing from a stowed position to at least one first deployed position; a second deployable lift device having a second spanwise location different than the first and being movable relative to the wing from a stowed position to at least one second deployed position; a drive system that includes: a first motor; a first motor brake coupled to the first motor to se...