JPS63143496U - - Google Patents

Info

Publication number
JPS63143496U
JPS63143496U JP3591987U JP3591987U JPS63143496U JP S63143496 U JPS63143496 U JP S63143496U JP 3591987 U JP3591987 U JP 3591987U JP 3591987 U JP3591987 U JP 3591987U JP S63143496 U JPS63143496 U JP S63143496U
Authority
JP
Japan
Prior art keywords
exhaust duct
test device
gap
wavelength
combustion chamber
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.)
Pending
Application number
JP3591987U
Other languages
Japanese (ja)
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
Application filed filed Critical
Priority to JP3591987U priority Critical patent/JPS63143496U/ja
Publication of JPS63143496U publication Critical patent/JPS63143496U/ja
Pending legal-status Critical Current

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  • Testing Of Engines (AREA)

Description

【図面の簡単な説明】[Brief explanation of the drawing]

第1図はこの考案の一実施例によるロケツト燃
焼試験装置を側面方向から見た断面図、第2図は
第1図におけるA―A線断面図、第3図は従来の
ロケツト燃焼試験装置を側面方向から見た断面図
である。 1……ロケツト燃焼試験装置、2b……天井面
(排気ダクトの内面)、2c……側壁(排気ダク
トの内面)、5……燃焼室、6……排気ダクト、
13……消音用壁体、13a……波長撹乱用孔、
S……隙間。
Fig. 1 is a cross-sectional view of a rocket combustion test device according to an embodiment of this invention, as seen from the side, Fig. 2 is a cross-sectional view taken along the line A--A in Fig. 1, and Fig. 3 is a cross-sectional view of a conventional rocket combustion test device. It is a sectional view seen from the side direction. 1... Rocket combustion test device, 2b... Ceiling surface (inner surface of exhaust duct), 2c... Side wall (inner surface of exhaust duct), 5... Combustion chamber, 6... Exhaust duct,
13... Sound deadening wall, 13a... Wavelength disturbance hole,
S...Gap.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 燃焼室とこれに連続する排気ダクトとを備えた
ロケツト燃焼試験装置において、前記排気ダクト
に、多数の波長撹乱用孔を備えた消音用壁体を、
前記排気ダクトの内面との間に隙間をおいて設け
、前記波長撹乱用孔を介して前記排気ダクトの中
心側と隙間とを連通状態にしてあることを特徴と
するロケツト燃焼試験装置。
In a rocket combustion test device equipped with a combustion chamber and an exhaust duct continuous with the combustion chamber, the exhaust duct is provided with a noise-reducing wall body equipped with a large number of wavelength-disturbing holes,
A rocket combustion test device characterized in that a gap is provided between the exhaust duct and the inner surface of the exhaust duct, and the center side of the exhaust duct and the gap are in communication with each other via the wavelength disturbance hole.
JP3591987U 1987-03-13 1987-03-13 Pending JPS63143496U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3591987U JPS63143496U (en) 1987-03-13 1987-03-13

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3591987U JPS63143496U (en) 1987-03-13 1987-03-13

Publications (1)

Publication Number Publication Date
JPS63143496U true JPS63143496U (en) 1988-09-21

Family

ID=30845850

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3591987U Pending JPS63143496U (en) 1987-03-13 1987-03-13

Country Status (1)

Country Link
JP (1) JPS63143496U (en)

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