IP Library › Granted Patent US 8,082,726
Granted Patent B2
US 8,082,726 · App. 11/768,240 · Granted Dec 27, 2011

Tangential anti-swirl air supply

Assignee: United Technologies Corporation
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Quick Facts
Patent No.
US 8,082,726
App. No.
11/768,240
Filed
Jun 26, 2007
Granted
Dec 27, 2011
Kind
B2
Art Unit
3741
USPC
60/226.1
Abstract

A turbofan flow delivery system includes a fan case housing a fan. Flow exit guide vanes are arranged downstream from the fan and extend radially inwardly from the fan case toward a bypass flow path. A supply passage includes an opening provided in the fan case between the fan and flow exit guide vanes configured to selectively provide pressurized air to a component using air from the bypass flow path. Swirling air from the bypass flow path enters the supply passage and is converted to a static pressure.

Claims (9)

1. A turbofan flow delivery system comprising:

a fan case housing a fan, and flow exit guide vanes downstream from the fan and extending radially inwardly from the fan case toward a bypass flow path;

a supply passage having an opening provided in the fan case between the fan and flow exit guide vanes configured to selectively provide static pressurized air to a component using air from the bypass flow path;

a fan nacelle surrounding the fan case, the supply passage arranged within the fan nacelle, wherein the fan nacelle includes a bulkhead supporting a portion of the supply passage within a cavity provided between inner and outer surfaces of the fan nacelle; and

wherein the cavity includes a pressurized vessel forward of the bulkhead, and apertures are provided in the inner surface near an inlet of the fan nacelle, the apertures in fluid communication with the pressure vessel.

2. A turbofan flow delivery system comprising:

a fan case housing a fan, and flow exit guide vanes downstream from the fan and extending radially inwardly from the fan case toward a bypass flow path;

a supply passage having an opening provided in the fan case between the fan and flow exit guide vanes configured to selectively provide static pressurized air to a component using air from the bypass flow path; and

wherein the supply passage includes first and second portions at an angle relative to one another, the first portion arranged generally tangentially relative to the bypass flow path, and the second portion arranged generally axially relative to the bypass flow path and configured to convert the bypass flow to static pressure.

Assignments (3)
CORRECTIVE ASSIGNMENT TO CORRECT THE AND REMOVE PATENT APPLICATION NUMBER 11886281 AND ADD PATENT APPLICATION NUMBER 14846874. TO CORRECT THE RECEIVING PARTY ADDRESS PREVIOUSLY RECORDED AT REEL: 054062 FRAME: 0001. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF ADDRESS. Recorded Mar 4, 2021
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 055659/0001 →
CHANGE OF NAME Recorded Sep 4, 2020
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 054062/0001 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 26, 2007
From: CLOFT, THOMAS G.
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 019476/0691 →
Continuity (1)
Related Publication 20090000272A1 · Jan 1, 2009