Invention Grant
- Patent Title: Dual mode frangible refueling nozzle
- Patent Title (中): 双模式易碎加油喷嘴
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Application No.: US14698515Application Date: 2015-04-28
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Publication No.: US09540115B2Publication Date: 2017-01-10
- Inventor: Jon F. Garruba
- Applicant: Jon F. Garruba
- Applicant Address: US VA Falls Church
- Assignee: NORTHROP GRUMMAN SYSTEMS CORPORATION
- Current Assignee: NORTHROP GRUMMAN SYSTEMS CORPORATION
- Current Assignee Address: US VA Falls Church
- Agency: Tarolli, Sundheim, Covell & Tummino LLP
- Main IPC: B64D39/06
- IPC: B64D39/06 ; B64D39/04

Abstract:
An in-flight refueling probe includes a first tubular member secured to an aircraft and a second tubular member having a releasable connection with the first tubular member such that the second tubular member detaches from the first tubular member in response to a predetermined force applied to the connection. A nozzle secured to the second tubular member can be coupled to a receptacle of a fuel dispensing aircraft. A tethering member is connected to the first tubular member and one of the second tubular member and the nozzle. The tethering member remains intact to connect the detached second tubular member to the first tubular member when a first tensile force is applied to the tethering member. The tethering member ruptures to disconnect the detached second tubular member from the first tubular member when a second tensile force greater than the first tensile force is applied to the tethering member.
Public/Granted literature
- US20160318621A1 DUAL MODE FRANGIBLE REFUELING NOZZLE Public/Granted day:2016-11-03
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