|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-001/10 B64C-007/00 B64D-001/02 B64D-001/14|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 4 인용 특허 : 3|
An apparatus includes a first tube portion forming a portion of an air vehicle deployable pod and a second tube portion. The first and second tube portions are slidably coupled. The apparatus also includes a cavity formed between the tube portions. The second tube portion slides relative to the first tube portion to reduce the size of the cavity and dissipate energy upon impact of the first tube portion.
1. An apparatus, comprising: a first tube portion forming a portion of an air vehicle deployable pod, the air vehicle deployable pod to be deployed from an aircraft;a second tube portion, the first and second tube portions being slidably coupled;a cavity formed by at least one of the first tube portion or the second tube portion, the second tube portion to slide relative to the first tube portion to change a size of the cavity and dissipate energy upon impact of the first tube portion with a deployment area, the impact to deform the air vehicle deployabl...