Invention Grant
- Patent Title: Inner cowl structure for aircraft turbine engine
- Patent Title (中): 飞机涡轮发动机内罩结构
-
Application No.: US13862941Application Date: 2013-04-15
-
Publication No.: US09404507B2Publication Date: 2016-08-02
- Inventor: Antony Brett Scarr , Thomas Joseph Weir , Allen Madsen Woolley , Carol Marie Janzon
- Applicant: MRA Systems, Inc.
- Applicant Address: US MD Baltimore
- Assignee: MRA SYSTEMS, INC.
- Current Assignee: MRA SYSTEMS, INC.
- Current Assignee Address: US MD Baltimore
- Agency: GE Global Patent Operation
- Agent William S. Munnerlyn
- Main IPC: B64D27/00
- IPC: B64D27/00 ; F04D29/40 ; B64D29/06
Abstract:
An inner cowl structure for circumscribing at least a portion of a jet engine extending from an aircraft includes an apron configured to mount directly to the engine independent of the pylon and overly an upper portion of the jet engine, and an inner body configured to circumscribe a portion of the jet engine not circumscribed by the apron.
Public/Granted literature
- US20140319269A1 INNER COWL STRUCTURE FOR AIRCRAFT TURBINE ENGINE Public/Granted day:2014-10-30
Information query
