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DE1531452C - Jet nozzle for a gas turbine jet engine - Google Patents

Jet nozzle for a gas turbine jet engine

Info

Publication number
DE1531452C
DE1531452C DE19671531452 DE1531452A DE1531452C DE 1531452 C DE1531452 C DE 1531452C DE 19671531452 DE19671531452 DE 19671531452 DE 1531452 A DE1531452 A DE 1531452A DE 1531452 C DE1531452 C DE 1531452C
Authority
DE
Germany
Prior art keywords
jet
gas turbine
jet nozzle
engine
nozzle
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.)
Expired
Application number
DE19671531452
Other languages
German (de)
Other versions
DE1531452B2 (en
DE1531452A1 (en
Inventor
Francis Jeffrey Sutton-in-Ashfield Nottingham; Cresswell Roger Anthony Derbyshire; Colville (Großbritannien)
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.)
UK Secretary of State for Defence
Original Assignee
UK Secretary of State for Defence
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 GB53702/66A external-priority patent/GB1139958A/en
Application filed by UK Secretary of State for Defence filed Critical UK Secretary of State for Defence
Publication of DE1531452A1 publication Critical patent/DE1531452A1/en
Publication of DE1531452B2 publication Critical patent/DE1531452B2/en
Application granted granted Critical
Publication of DE1531452C publication Critical patent/DE1531452C/en
Expired legal-status Critical Current

Links

Description

Hierzu 1 Blatt Zeichnungen1 sheet of drawings

Claims (2)

Patentansprüche:Patent claims: 1. Strahldüse für ein Gasturbinenstrahltriebwerk, die über einen im Querschnitt ringförmigen1. Jet nozzle for a gas turbine jet engine, which has an annular cross-section • Kanal in eine Vielzahl von kranzförmig angeordneten Einzeldüsen aufgespalten ist, von denen jede am Ende ein bewegliches Düsenglied trägt, dadurch gekennzeichnet, daß Druckluft vom stromabwärtigen Ende des Verdichters über Leitungen (20) in den ringförmigen Kanal (18) geführt wird.• Channel is split into a large number of individual nozzles arranged in a ring, of which each carrying a movable nozzle member at the end, characterized in that compressed air from the downstream end of the compressor via lines (20) into the annular channel (18) to be led. 2. Strahldüse nach Anspruch 1, dadurch gekennzeichnet, daß jede Druckluftleitung (20) in einen Verteiler (21) endet, der zwischen benachbarten Einzeldüsen (16) angeordnet ist und über Öffnungen (22) mit dem ringförmigen Kanal (18) in Verbindung steht.2. Jet nozzle according to claim 1, characterized in that each compressed air line (20) in ends a manifold (21) which is arranged between adjacent individual nozzles (16) and over Openings (22) with the annular channel (18) is in communication.
DE19671531452 1966-11-30 1967-11-22 Jet nozzle for a gas turbine jet engine Expired DE1531452C (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB53702/66A GB1139958A (en) 1966-11-30 1966-11-30 Jet nozzle assembly for a gas turbine engine
GB5370266 1966-11-30
DER0047420 1967-11-22

Publications (3)

Publication Number Publication Date
DE1531452A1 DE1531452A1 (en) 1970-05-06
DE1531452B2 DE1531452B2 (en) 1971-05-13
DE1531452C true DE1531452C (en) 1973-09-06

Family

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