Aerospace Engineering
集成加力燃烧室
Integrated AfterburnerA combustion system designed to increase thrust by burning additional fuel in the exhaust stream of a gas turbine engine. / 一种旨在通过在燃气涡轮发动机排气流中燃烧额外燃料来增加推力的燃烧系统。
- Knowledge type
- 工艺技术
- First proposed or discovered
- Proposer
- Turkey Farm member
- Creator
- 农场主
- Last updated
- 2026-11-02 20:06:01
Sub-knowledge points
Ignition characteristicsFlameholder stability
Higher-order knowledge points
No connected node yet
Main parameters and performance indicators
Oxygen-lean conditions: The operating environment characterized by a low oxygen concentration.Combined cavity-strut-wall flameholder: A specific aerodynamic structure used to stabilize the flame.
Open problems
No unresolved problem recorded yet
Related literature
ranked by community starsExperimental investigation on ignition characteristics of an integrated afterburner with a combined cavity-strut-wall flameholder under oxygen-lean conditionsOpen source
Related products and links
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Creation and modification trail
1 recordsRecord title: Integrated Afterburner.
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