|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 8|
Aspects of the disclosure are directed to a system that includes a boot configured to attach to a chevron of an aircraft nacelle, and an attachment mechanism configured to attach the boot and the chevron. In some embodiments, a boot includes a first surface and a second surface, where the surfaces are attached by inwardly tapering sidewalls that form an opening that is configured to surround a chevron of an aircraft nacelle. In some embodiments, a repair of a chevron on an exhaust nozzle of an aircraft engine includes placing a chevron-shaped boot with a...
1. A method of repairing a damaged chevron structure on an exhaust nozzle of an aircraft engine, the damaged chevron structure defining a first end including a first side and a second side which meet at a rounded corner and an opposed second end which extends into two opposed flange portions which are connected to the exhaust nozzle, the method comprising: providing a repair boot defining a substantially triangular shape defining a first boot end having a first side and a second side which meet at a rounded corner corresponding with the rounded corner of...