IP Library Granted Patent US 10,532,802
Granted Patent B2
US 10,532,802 · App. 15/100,619 · Granted Jan 14, 2020

Propulsion assembly comprising a box for retaining drained fluids

Inventors: Julien Sayn-Urpar (Moissy-Cramayel, FR); Hervé Jean Albert Mouton (Moissy-Cramayel, FR); Julien Pavillet (Moissy-Cramayel, FR)
Assignee: SAFRAN AIRCRAFT ENGINES
B64C1/1453B64D29/00F01D25/24F01D25/28F01D25/32F05D2260/602
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Quick Facts
Patent No.
US 10,532,802
App. No.
15/100,619
Granted
Jan 14, 2020
Kind
B2
Abstract

A propulsion assembly includes an engine surrounded by a nacelle, structure for draining the fluids from the engine and structure for guiding said fluids to a retention box. The retention box is arranged outside the engine and has a cavity for storing drained fluids. The retention box is fixed to a cowling of the nacelle and supported thereby.

Claims (20)

1. A propulsion assembly, comprising:

an engine surrounded by a nacelle;

means for draining liquids from the engine; and

means for conveying said liquids to a retaining box outside the engine, the retaining box comprising a mast having an aerodynamic profile which comprises an internal cavity for storing the liquids and at least one opening for discharging the liquids held in the cavity,

wherein the retaining box is attached to a cowl of the nacelle and is supported thereby, the cowl being removable for access to the engine and defining an outer surface of the propulsion assembly, and

wherein the retaining box comprises, at one end of the mast, an attachment plate comprising means for attachment to the cowl of the nacelle and connection means that interact with means for conveying said liquids,

wherein said means for conveying said liquids comprise ducts each having an outlet, and said connection means comprising channels, each channel opening both on a radially inner surface of the attachment plate and into the internal cavity for storing the liquids, the outlet of each duct being fitted in one of the channels.

2. The propulsion assembly according to claim 1 , wherein the plate is covered with a heat protection sheet.

3. The propulsion assembly according to claim 1 , wherein the retaining box is located at a lowest circumferential position on the nacelle.

4. The propulsion assembly according to claim 1 , wherein the attachment plate abuts a radially inner face of the cowl.

5. The propulsion assembly according to claim 1 , wherein a seal is located between the attachment plate and the cowl.

6. A propulsion assembly, comprising:

an engine surrounded by a nacelle;

a retaining box disposed outside of said engine and carried by the nacelle, the retaining box comprising a drainage mast having an aerodynamic profile, the drainage mast comprising an internal cavity for collection and storage of liquids from said engine, the drainage mast further comprising an attachment plate at one end thereof and at least one opening for discharging liquids held in the internal cavity;

a plurality of ducts, each duct having an outlet arranged to supply said liquids to the retaining box;

a plurality of channels, each channel having a first opening that opens to a radially inner surface of the attachment plate and a second opening that opens into the internal cavity,

wherein the outlets of said ducts are connected in fluid communication with said first openings of said channels, respectively.

7. The propulsion assembly according to claim 6 , wherein the nacelle comprises a cowl defining an outer surface of the propulsion assembly, and wherein the drainage mast protrudes outwardly away from said outer surface of said cowl.

8. The propulsion assembly according to claim 7 , wherein the attachment plate includes at least one attachment interface configured for coupling with said cowl.

9. The propulsion assembly according to claim 7 , wherein the retaining box is located at a lowest circumferential position on the nacelle.

Assignments (3)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
NUNC PRO TUNC ASSIGNMENT Recorded May 31, 2016
From: SAYN-URPAR, JULIEN; MOUTON, HERVÉ JEAN ALBERT; PAVILLET, JULIEN
To: SNECMA
Reel/Frame 038754/0915 →
Priority Claims (1)
FR 13 62076 · Dec 4, 2013 · national
Continuity (1)
Related Publication 20160304184A1 · Oct 20, 2016
Cited By (1)
US 12,320,269