CA2845192C - Chambre de combustion pour turbine a gaz - Google Patents

Chambre de combustion pour turbine a gaz Download PDF

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Publication number
CA2845192C
CA2845192C CA2845192A CA2845192A CA2845192C CA 2845192 C CA2845192 C CA 2845192C CA 2845192 A CA2845192 A CA 2845192A CA 2845192 A CA2845192 A CA 2845192A CA 2845192 C CA2845192 C CA 2845192C
Authority
CA
Canada
Prior art keywords
annular
scoop
combustor
liner
air
Prior art date
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.)
Active
Application number
CA2845192A
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English (en)
Other versions
CA2845192A1 (fr
Inventor
Tin Cheung John Hu
Oleg Morenko
Lev Alexander Prociw
Parham Zabeti
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.)
Pratt and Whitney Canada Corp
Original Assignee
Pratt and Whitney Canada Corp
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.)
Filing date
Publication date
Priority claimed from US13/795,089 external-priority patent/US9228747B2/en
Application filed by Pratt and Whitney Canada Corp filed Critical Pratt and Whitney Canada Corp
Publication of CA2845192A1 publication Critical patent/CA2845192A1/fr
Application granted granted Critical
Publication of CA2845192C publication Critical patent/CA2845192C/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Abstract

Il est décrit une chambre à combustion pour une turbine à gaz comprend des chemises intérieure et extérieure définissant une chambre de combustion annulaire et au moins un anneau de ramassage disposé sur chacune des chemises intérieure et extérieure de la chambre de combustion. L'anneau de ramassage comprend une base intérieure radiale solide percée d'alésages qui donnent sur la chambre de combustion et forment des admissions de dilution d'air. L'anneau de ramassage comprend une partie extérieure radiale en forme de cuillère dont la face ouverte peut recevoir un flux d'air annulaire à haute vitesse. Les alésages des admissions qui donnent sur la partie de l'anneau en vue de diriger le flux d'air dans la chambre de combustion, dans laquelle les alésages des admissions forment des tuyères servant à fournir pénétration et orientation au jet d'air à l'intérieur de la chambre de combustion.
CA2845192A 2013-03-12 2014-03-06 Chambre de combustion pour turbine a gaz Active CA2845192C (fr)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US13/795,089 2013-03-12
US13/795,089 US9228747B2 (en) 2013-03-12 2013-03-12 Combustor for gas turbine engine
US14/063,449 US10378774B2 (en) 2013-03-12 2013-10-25 Annular combustor with scoop ring for gas turbine engine
US14/063,449 2013-10-25

Publications (2)

Publication Number Publication Date
CA2845192A1 CA2845192A1 (fr) 2014-09-12
CA2845192C true CA2845192C (fr) 2022-11-15

Family

ID=51730240

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2845192A Active CA2845192C (fr) 2013-03-12 2014-03-06 Chambre de combustion pour turbine a gaz

Country Status (1)

Country Link
CA (1) CA2845192C (fr)

Also Published As

Publication number Publication date
CA2845192A1 (fr) 2014-09-12

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