Invention Grant
- Patent Title: Gas ejection cone for aircraft turbojet engines
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Application No.: US14484684Application Date: 2014-09-12
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Publication No.: US09611807B2Publication Date: 2017-04-04
- Inventor: Pascal-Marie Paul Marcel Soulier , Jean-Bernard Guillon , Jean-Pierre Guegou
- Applicant: AIRCELLE
- Applicant Address: FR Gonfeville l'Orcher
- Assignee: AIRCELLE
- Current Assignee: AIRCELLE
- Current Assignee Address: FR Gonfeville l'Orcher
- Agency: Burris Law, PLLC
- Priority: FR1252473 20120320
- Main IPC: F02K1/36
- IPC: F02K1/36 ; F02K1/04 ; B64C7/02

Abstract:
A gas ejection cone includes a cylindrical-shaped front cone portion, a conical-shaped rear cone portion, a ventilation tube and a support bearing of this drainage and/or ventilation tube. The ventilation tube extends inside the cylindrical-shaped front and conical-shaped rear cone portions and emerges at the end of the conical-shaped rear cone portion. In particular, the conical-shaped rear cone portion includes a front sub-portion connected to the cylindrical-shaped front cone portion, and a rear sub-portion removably secured to the front sub-portion. The rear sub-portion is further equipped with an outlet port of the ventilation tube.
Public/Granted literature
- US20150000289A1 GAS EJECTION CONE FOR AIRCRAFT TURBOJET ENGINES Public/Granted day:2015-01-01
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