GB1247092A - Creación de Inventos y Patentes con Inteligencia Artificial

GB1247092A – Improvements in or relating to gas purification devices
– Google Patents

GB1247092A – Improvements in or relating to gas purification devices
– Google Patents
Improvements in or relating to gas purification devices

Info

Publication number
GB1247092A

GB1247092A
GB54143/69A
GB5414369A
GB1247092A
GB 1247092 A
GB1247092 A
GB 1247092A
GB 54143/69 A
GB54143/69 A
GB 54143/69A
GB 5414369 A
GB5414369 A
GB 5414369A
GB 1247092 A
GB1247092 A
GB 1247092A
Authority
GB
United Kingdom
Prior art keywords
casing
vanes
section
gas
sleeve
Prior art date
1968-11-06
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)

Expired

Application number
GB54143/69A
Inventor
Louis Leonard Bou Ru
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)

Safran Aircraft Engines SAS

Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
1968-11-06
Filing date
1969-11-05
Publication date
1971-09-22

1969-11-05
Application filed by Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS
filed
Critical
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA

1971-09-22
Publication of GB1247092A
publication
Critical
patent/GB1247092A/en

Status
Expired
legal-status
Critical
Current

Links

Espacenet

Global Dossier

Discuss

Classifications

F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING

F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES

F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES

F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups

F01D25/18—Lubricating arrangements

B—PERFORMING OPERATIONS; TRANSPORTING

B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL

B01D—SEPARATION

B01D45/00—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces

B01D45/12—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces by centrifugal forces

B01D45/14—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces by centrifugal forces generated by rotating vanes, discs, drums or brushes

F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING

F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES

F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING

F01M13/00—Crankcase ventilating or breathing

F01M13/04—Crankcase ventilating or breathing having means for purifying air before leaving crankcase, e.g. removing oil

F01M2013/0422—Separating oil and gas with a centrifuge device

Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS

Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC

Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS

Y10S494/00—Imperforate bowl: centrifugal separators

Y10S494/90—Imperforate bowl: centrifugal separators involving mixture containing one or more gases

Abstract

1,247,092. Centrifugal separator. SOC. NATIONALE D’ETUDE ET DE CONSTRUCTION DE MOTEURS D’AVIATION. 5 Nov., 1969 [6 Nov., 1968], No. 54143/69. Heading B2P. An apparatus for separating solid or liquid particles from gas comprises a hollow rotatable casing 3 having an annular lateral wall 3a formed with. passages 3ab for the discharge of the particles and two end covers 3b, 3c, one of which, 3c, has an entry orifice 5 for the gas to be purified, passages 1d being provided radially inwardly for discharging the purified gas. Vanes 4 divide the interior of the casing into a number of ducts 6 each delimited by opposite faces 4aa, 4ab of consecutive vanes and extending over the whole axial length of the casing interior. Each vane 4 presents, viewed in section in a plane perpendicular to the axis of the casing, Fig. 2, substantially the shape of a wedge so that the opposite faces 4aa, 4ab of consecutive vanes are substantially parallel to one another. A baffle 4b projecting into each of the ducts 6 co-operates with the internal faces of the lateral wall 3a and of the end covers 3b, 3c of the casing in order to subdivide the respective duct into a centrifugal entry section 6a communicating with the entry orifice 5 and having a substantially constant flow area, a convergent intermediate section substantially parallel to the axis of the casing, and a centripetal divergent exit section 6c communicating with a corresponding passage 1d through which the purified gas is discharged. The vanes 4, which are undercut at 4aba adjacent the discharge passages 3ab, are carried by a ring 4c and by a sleeve 4b which constitute the baffle in each duct. The casing 3 is secured with the ring 4c on a hollow shaft by means of screws 7 and the casing, vanes 4 and sleeve 4b are held together by screws 8. The interior of the shaft 1 forms a passage 1a closed in one direction by a deflector cone 1b. The ring 4c has an inclined face 4cb which co-operates with the opposite face 4bc, of the sleeve 4b to form in each duct 6 a convergent section downstream of the divergent exit section 6c through which the gas is accelerated prior to discharge through the corresponding passage 1d.

GB54143/69A
1968-11-06
1969-11-05
Improvements in or relating to gas purification devices

Expired

GB1247092A
(en)

Applications Claiming Priority (1)

Application Number
Priority Date
Filing Date
Title

FR172808

1968-11-06

Publications (1)

Publication Number
Publication Date

GB1247092A
true

GB1247092A
(en)

1971-09-22

Family
ID=8656558
Family Applications (1)

Application Number
Title
Priority Date
Filing Date

GB54143/69A
Expired

GB1247092A
(en)

1968-11-06
1969-11-05
Improvements in or relating to gas purification devices

Country Status (4)

Country
Link

US
(1)

US3561195A
(en)

DE
(1)

DE1955966C3
(en)

FR
(1)

FR1590886A
(en)

GB
(1)

GB1247092A
(en)

Families Citing this family (34)

* Cited by examiner, † Cited by third party

Publication number
Priority date
Publication date
Assignee
Title

US3712032A
(en)

1970-11-19
1973-01-23
Anco Corp
High speed centrifugal air-oil separator

GB1508212A
(en)

1975-02-10
1978-04-19
Rolls Royce
Apparatus for separating suspension of liquids in gas

US4093397A
(en)

1976-04-15
1978-06-06
Lovelady Grady R
High vacuum pump

US4236868A
(en)

1978-07-19
1980-12-02
Airco, Inc.
Tangential RIF turbine with particle removing means

FR2541437B1
(en)

1982-05-13
1985-08-23
Zimmern Bernard

CENTRIFUGAL ECONOMIZER FOR REFRIGERATION

FR2556778B1
(en)

1983-12-14
1986-08-22
Snecma

GAS-LIQUID SEPARATION DEVICE AND ITS APPLICATION TO DECOILING THE VENTILATION AIR OF THE BEARING SPEAKERS OF A TURBOMACHINE

US5273163A
(en)

1992-01-23
1993-12-28
Luzenac America, Inc.
Centrifugal particle classifier having uniform influx distributor

SE9302921A0
(en)

1993-03-05
1994-09-06
P A S Material Ab

Separation of dust from an air stream and dust separator for this

FR2742804B1
(en)

1995-12-20
1998-01-16
Snecma

LUBRICATION ENCLOSURE ROTOR ROTOR

DE19607919B4
(en)

1996-03-01
2005-03-17
Bayerische Motoren Werke Ag

Centrifugal oil separator for the blow-by gases of an internal combustion engine

DE19704845A1
(en)

1997-02-08
1998-08-13
Bmw Rolls Royce Gmbh
Aircraft power plant oil separator

DE19803872C2
(en)

1998-01-31
2001-05-10
Daimler Chrysler Ag

Ventilation device for a crankcase of an internal combustion engine

US6810849B1
(en)

1999-01-25
2004-11-02
Briggs & Stratton Corporation
Four-stroke internal combustion engine

DE19909434C2
(en)

1999-03-04
2001-02-08
Daimler Chrysler Ag

Device for separating oil from the blowby gases of an internal combustion engine

DE19931740C2
(en)

1999-07-08
2001-06-13
Daimler Chrysler Ag

Reciprocating internal combustion engine with a camshaft

US6451093B1
(en)

2001-01-22
2002-09-17
Charles C. Miles
Centripetal demister

GB0206243D0
(en)

2002-03-16
2002-05-01
Rolls Royce Plc
An air/oil separator

US7377110B2
(en)

2004-03-31
2008-05-27
United Technologies Corporation
Deoiler for a lubrication system

DE112006000356A5
(en)

2005-05-10
2007-11-22
Mahle International Gmbh

Centrifugal oil mist separator integrated in an axially hollow shaft of an internal combustion engine

FR2913061B1
(en)

2007-02-27
2009-05-22
Snecma Sa

SHEATHING SYSTEM FOR AN AIRCRAFT ENGINE.

FR2937680B1
(en)

2008-10-24
2013-11-08
Snecma

ROTOR DEHUILEUR FOR TURBOMACHINE

DE102010014546A1
(en)

2010-04-10
2011-10-13
Mahle International Gmbh

Internal combustion engine

DE102011000458A1
(en)

2011-02-02
2012-08-02
Thyssenkrupp Presta Teccenter Ag

Shaft, in particular camshaft with a hollow shaft section

CN103939178B
(en)

2014-04-10
2015-12-23
安徽全柴动力股份有限公司
A kind of high efficiency, low cost diesel engine oil gas separating device

GB201415727D0
(en)

2014-09-05
2014-10-22
Rolls Royce Plc
A liquid-capturing shaft

JP5918881B1
(en)

2015-04-24
2016-05-18
光洋サーモシステム株式会社

Stirring fan for heat treatment apparatus and heat treatment apparatus provided with the same

US20160325214A1
(en)

2015-05-06
2016-11-10
Caterpillar Inc.
Contaminate separator for seals of rotating shafts

US10473206B2
(en)

2015-07-02
2019-11-12
Deere & Company
Transmission vent

US10385729B2
(en)

2015-11-24
2019-08-20
General Electric Company
Cylindrical air guide in a turbine engine

DE102017105241B4
(en)

2017-03-13
2019-12-19
Thyssenkrupp Ag

Centrifugal oil separator, oil separator and internal combustion engine

FR3064672B1
(en)

2017-03-28
2021-03-05
Sogefi Filtration Spa

ROTATING DEVICE FOR SEPARATING THE OIL FROM THE CRANKCASE GASES OF AN INTERNAL COMBUSTION ENGINE

US10918989B2
(en)

2018-04-10
2021-02-16
Pratt & Whitney Canada Corp.
Air-oil separator with two flow paths

US10870079B2
(en)

2018-04-10
2020-12-22
Pratt & Whitney Canada Corp.
Air-oil separator with first separator radially outward of matrix separator

FR3096275B1
(en)

2019-05-24
2021-06-18
Safran Helicopter Engines

Part for a turbomachine centrifugal degasser with adapted longitudinal walls

1968

1968-11-06
FR
FR172808A
patent/FR1590886A/fr
not_active
Expired

1969

1969-11-04
US
US873990A
patent/US3561195A/en
not_active
Expired – Lifetime

1969-11-05
GB
GB54143/69A
patent/GB1247092A/en
not_active
Expired

1969-11-06
DE
DE1955966A
patent/DE1955966C3/en
not_active
Expired

Also Published As

Publication number
Publication date

FR1590886A
(en)

1970-04-20

DE1955966A1
(en)

1970-06-11

DE1955966C3
(en)

1973-11-22

DE1955966B2
(en)

1973-04-26

US3561195A
(en)

1971-02-09

Información de contacto