JPS598100U - Let's fly - Google Patents
Let's flyInfo
- Publication number
- JPS598100U JPS598100U JP9897082U JP9897082U JPS598100U JP S598100 U JPS598100 U JP S598100U JP 9897082 U JP9897082 U JP 9897082U JP 9897082 U JP9897082 U JP 9897082U JP S598100 U JPS598100 U JP S598100U
- Authority
- JP
- Japan
- Prior art keywords
- flying object
- thermal energy
- ignition
- ignition device
- engine
- 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
Links
Landscapes
- Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
Abstract
(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
第１図は従来の飛しよう体の内部構成例を示す概略の構
成図、第２図はこの考案による飛しよう体の内部構成例
を示す構成図であり、図中１は飛しよう体、２は推進機
関、３は電源装置、４は油圧装置、５は点火装置、６は
安全装置、７は油圧配管、Ａは母機、Ｂは発射指令信号
、Ｃは点火指令信号である。尚、図中同一部分あるいは
相当部分にｉマ同−符号を付しである。FIG. 1 is a schematic configuration diagram showing an example of the internal configuration of a conventional flying body, and FIG. 2 is a configuration diagram showing an example of the internal configuration of a flying body according to this invention. 3 is a propulsion engine, 3 is a power supply device, 4 is a hydraulic system, 5 is an ignition device, 6 is a safety device, 7 is a hydraulic piping, A is a base machine, B is a firing command signal, and C is an ignition command signal. In the drawings, the same or equivalent parts are given the same reference numerals.
Claims (1)
り動作し、飛しよう体推進機関の点火装” 置に電気
信号を供給する電源装置と、操舵翼等を駆動させる油圧
装置と、上記推進機関を燃焼させるための熱エネルギー
を発生する点火装置と、この点火装置から発生した熱エ
ネルギーにより推薬を燃焼し、その燃焼により、推進力
を得る推進機関とを有する飛しよう体において上記油圧
装置で発生する油圧により上記安全装置を解除し、上記
点火装置からの熱エネルギーを推進機関に伝えるように
構成したことを特徴とする飛しよう体。A power supply device that operates in response to a launch command signal from the mother aircraft on which the flying object is mounted and supplies an electric signal to the ignition system of the flying object propulsion engine, a hydraulic device that drives the steering blades, etc., and the above-mentioned propulsion device. The above-mentioned hydraulic system in a flying object having an ignition device that generates thermal energy to combust an engine, and a propulsion engine that burns a propellant using the thermal energy generated from the ignition device and obtains propulsive force by the combustion. A flying object characterized in that the safety device is released by hydraulic pressure generated by the ignition device, and the thermal energy from the ignition device is transmitted to the propulsion engine.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9897082U JPS598100U (en) | 1982-06-30 | 1982-06-30 | Let's fly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9897082U JPS598100U (en) | 1982-06-30 | 1982-06-30 | Let's fly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS598100U true JPS598100U (en) | 1984-01-19 |
Family
ID=30234739
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP9897082U Pending JPS598100U (en) | 1982-06-30 | 1982-06-30 | Let's fly |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS598100U (en) |
-
1982
- 1982-06-30 JP JP9897082U patent/JPS598100U/en active Pending
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