JPH0237098A - Multi-color smoke fuming device for aircraft - Google Patents

Multi-color smoke fuming device for aircraft

Info

Publication number
JPH0237098A
JPH0237098A JP18676588A JP18676588A JPH0237098A JP H0237098 A JPH0237098 A JP H0237098A JP 18676588 A JP18676588 A JP 18676588A JP 18676588 A JP18676588 A JP 18676588A JP H0237098 A JPH0237098 A JP H0237098A
Authority
JP
Japan
Prior art keywords
smoke
fuming
oil
aircraft
fuming oil
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
JP18676588A
Other languages
Japanese (ja)
Inventor
Makoto Hara
原 眞
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
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 by Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP18676588A priority Critical patent/JPH0237098A/en
Publication of JPH0237098A publication Critical patent/JPH0237098A/en
Pending legal-status Critical Current

Links

Landscapes

  • Exhaust Gas After Treatment (AREA)

Abstract

PURPOSE:To enable to have mottled smoke of multi-colors fumed by operating a control switch for switching valves connected with respective fuming oil tanks with different pigments mixed, and disposed at plural passages comprising a smoke nozzle opening into engine exhaust. CONSTITUTION:When a valve 5A is opened and a valve 5B is closed through a controller 10 by means of a control switch 8, the fuming oil 2A in a fuming oil tank 1A is injected into the exhaust pipe 13 of a jet engine 4 from a smoke nozzle 9 through a passage 11A, the valve 5A and a smoke nozzle tube 9 by means of a pump 3A. The fuming oil 2A is carburetted by exhaust air 6, and smoke 12 of the colors corresponding to the pigments mixed in the fuming oil 2A is generated. When the valves 5A, 5B are switched after the appropriate time elapsed through the controller 10 reoperating the control switch 8, the fuming oil 2B in the fuming oil tank 1B is injected into the exhaust pipe 13, and the smoke 12 of different colors is generated.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は、マダラ状等の多色煙を発煙することができる
航空機用の多色煙発煙装置に関する。
DETAILED DESCRIPTION OF THE INVENTION [Industrial Field of Application] The present invention relates to a multicolor smoke generator for aircraft, which is capable of emitting multicolored smoke such as a spot-shaped smoke.

〔従来の技術〕[Conventional technology]

従来の航空機用の発煙装置は、第5図及び第6図に示す
ように、航空機014内に発煙油タンクO1を設け、同
効ンク01内の顔料が混合された発煙油02を、タンク
01内のポンプ03により操作スイッチ08で操作され
るバルブ05を経て、発煙ノズルO9からジェットエン
ジン04の排気管013中のエンジン排気06中に噴射
し、発煙油02を排気06によって気化させることによ
って発煙油に混合された顔料に対応する一色の埋012
を発生させるようになっている。
As shown in FIGS. 5 and 6, the conventional smoke generating device for aircraft includes a smoking oil tank O1 in the aircraft 014, and the smoking oil 02 mixed with the pigment in the same effect tank 01 is transferred to the tank 01. The oil is injected from the smoke nozzle O9 into the engine exhaust 06 in the exhaust pipe 013 of the jet engine 04 through the valve 05 operated by the operation switch 08 by the pump 03 inside, and the smoke is generated by vaporizing the smoke oil 02 by the exhaust gas 06. One color 012 corresponding to pigment mixed in oil
is designed to occur.

(発明が解決しようとする課題] 前述のように、従来の技術では、発煙油に混合された顔
料による一色の煙しか発生することができないので、展
示効果が劣っている。
(Problems to be Solved by the Invention) As described above, in the conventional technology, only one color of smoke can be generated due to the pigment mixed in the fuming oil, and therefore the display effect is poor.

本発明は、多色のマダラ状等の煙を発煙する航空機用の
多色煙の発煙装置を提供しようとするものである。
The present invention aims to provide a multi-colored smoke generating device for an aircraft that generates multi-colored spotted smoke.

〔課題を解決するための手段] 本発明の航空機用多色煙発煙装置は、それぞれ異る顔料
を混合した発煙油を収容する?!数の発煙油タンク、各
発煙油タンクに接続されエンジン排気中に開口する発煙
ノズルを有する複数の通路、及び同通路に設けられたバ
ルブを開閉するコントローラを備えている。
[Means for Solving the Problems] The multicolored aircraft smoke generator of the present invention accommodates smoke oils each containing a mixture of different pigments. ! The engine includes several smoking oil tanks, a plurality of passages connected to each smoking oil tank and having smoke nozzles that open into the engine exhaust gas, and a controller that opens and closes valves provided in the passages.

〔作用] 本発明では、コントローラによってバルブを開閉するこ
とによって特定の発煙油タンク内の発埋油をエンジン排
気中に噴射し、発煙油を気化されることによって同発煙
油に混合された顔料に対応する煙をうることができる。
[Operation] In the present invention, the buried oil in a specific smoking oil tank is injected into the engine exhaust by opening and closing the valve by the controller, and the smoking oil is vaporized and converted into pigment mixed in the smoking oil. You can get the corresponding smoke.

コントローラにより、開かれるバルブを適宜切換えるこ
とによって、マダラ状の多色の煙が発生する。
By appropriately switching the valves opened by the controller, multicolored smoke is generated.

また、開かれるバルブを適宜選定することによって、所
望の色の煙をうることかできる。
Further, by appropriately selecting the valves to be opened, smoke of a desired color can be produced.

〔実施例〕〔Example〕

本発明の第1の実施例を第1図及び第2図によって説明
する。
A first embodiment of the present invention will be described with reference to FIGS. 1 and 2.

IA、 IBはそれぞれ異る顔料が混合された発煙油2
A、2Bが収容されると共にポンプ3A、3Bを内蔵し
た発煙油タンクであり、同タンクIA、IBには、それ
ぞれバルブ5A、5Bが設けられた通路11A、 II
Bが接続され、同通路11A、11Bは発煙ノズル管9
′に接続されている。同発煙ノズル管9′の先端の発煙
ノズル9は、ジェットエンジン4の排気管13内に開口
し−ている。
IA and IB are fuming oils 2 with different pigments mixed together.
It is a smoking oil tank that accommodates oil pumps A and 2B and also has built-in pumps 3A and 3B, and the tanks IA and IB have passages 11A and II that are provided with valves 5A and 5B, respectively.
B is connected, and the same passages 11A and 11B are smoke nozzle pipes 9.
'It is connected to the. The smoke nozzle 9 at the tip of the smoke nozzle pipe 9' opens into the exhaust pipe 13 of the jet engine 4.

上記バルブ5A、5Bは操作スイッチ8で操作されるコ
ントローラ10によってその開閉が制御されるようにな
っている。
The opening and closing of the valves 5A and 5B are controlled by a controller 10 operated by an operation switch 8.

本実施例においては、操作スイッチ8によってコントロ
ーラ10を介してバルブ56.5Bの一方を開、他方を
閉にする。例えば、バルブ5Aを開、バルブ5Bを閉に
すると、一方の発煙油タンク内A内の発煙油2^は、ポ
ンプ3Aによって通路11A、バルブ5A及び発煙ノズ
ル管9′を通って発煙ノズル9からジェットエンジンの
排気管13内に噴射される。噴射された発煙油は、ジェ
ットエンジン4の排気6によって気化し、発煙油2^に
混合された顔料に対応する色の煙12を発生させる。適
当な時間経過後に、再び操作スイッチ8を操作して、コ
ントローラ10を介してバルブ5A、5Bの開閉を切換
えると、発煙油タンク内B内の発煙油2Bが排気管13
内に噴射され、異った色の煙12が発生する。
In this embodiment, the operation switch 8 opens one of the valves 56.5B and closes the other through the controller 10. For example, when the valve 5A is opened and the valve 5B is closed, the fuming oil 2^ in one of the fuming oil tanks A is transferred from the fuming nozzle 9 through the passage 11A, the valve 5A, and the fuming nozzle pipe 9' by the pump 3A. It is injected into the exhaust pipe 13 of the jet engine. The injected fuming oil is vaporized by the exhaust 6 of the jet engine 4 and generates smoke 12 of a color corresponding to the pigment mixed in the fuming oil 2^. After an appropriate period of time has elapsed, when the operation switch 8 is operated again to open and close the valves 5A and 5B via the controller 10, the smoking oil 2B in the smoking oil tank B is discharged from the exhaust pipe 13.
The smoke 12 of different colors is generated.

以上の操作を繰り返すことによって、第2図に示すよう
に、航空機14からマダラ状の2色の煙12が発生する
ことになる。
By repeating the above operations, as shown in FIG. 2, a spotted two-color smoke 12 is generated from the aircraft 14.

また、本実施例によって、マダラ状の煙を発生させる外
状況によって航空機14からの煙12を一方の色から他
方の色に変更することもでき、また所望の色の煙を選択
して発生させることもできる。
Further, according to this embodiment, the color of the smoke 12 from the aircraft 14 can be changed from one color to the other depending on the outside situation that generates the spotted smoke, and smoke of a desired color can be selected and generated. You can also do that.

本発明の第2の実施例を第3図によって説明する。A second embodiment of the present invention will be described with reference to FIG.

本実施例は上記第1の実施例と次に説明する点が相違し
ており、第3図において共通する部分は第1図及び第2
図と同一の符号を付し、その説明を省略する。
This embodiment differs from the above-mentioned first embodiment in the following points, and the common parts in FIG. 3 are those in FIGS.
The same reference numerals as in the figure are given, and the explanation thereof will be omitted.

本実施例では、発煙油タンクIA、 IBに接続された
通路11A、 IIBのそれぞれに、ジェットエンジン
排気管13内に開口する発煙ノズル9A、9Bを接続し
ている。
In this embodiment, smoke nozzles 9A and 9B that open into the jet engine exhaust pipe 13 are connected to the passages 11A and IIB connected to the smoke oil tanks IA and IB, respectively.

本実施例においても、第1の実施例におけると同様にマ
ダラ状等の2色の煙12を発生させることができる。
In this embodiment as well, as in the first embodiment, it is possible to generate two-color smoke 12 such as a spotted shape.

本発明の第3の実施例を第4図によって説明する。A third embodiment of the present invention will be described with reference to FIG.

本実施例は、ジェットエンジンが2個、皿ちジェットエ
ンジン4A、4Bをもつ双発航空機の場合であって、上
記第2実施例の一方の発煙ノズル9^が一方のジェット
エンジン4Aの排気中に発埋油を噴射し、他方のジェッ
トエンジン4Bの排気中に他方の発煙ノズル9Bが発煙
油を噴射するようにしたものである。
This embodiment is for a twin-engine aircraft with two jet engines, counter-sink jet engines 4A and 4B, and one smoke nozzle 9^ of the second embodiment is inserted into the exhaust gas of one jet engine 4A. The other smoke nozzle 9B injects the smoke oil into the exhaust gas of the other jet engine 4B.

本実施例においても、上記第1及び第2の実施例と同様
に2色の煙を発生させることができる。
In this embodiment as well, smoke of two colors can be generated as in the first and second embodiments.

なお、上記実施例は、いづれも2色の煙を発生するもの
であるが、本発明によって、3色以上の煙を発生するこ
とができることはいう迄もない。
Although the above embodiments all generate smoke of two colors, it goes without saying that the present invention can generate smoke of three or more colors.

〔発明の効果〕〔Effect of the invention〕

以上説明したように、本発明は、航空機からマダラ状等
の多色の煙を得ることができ、展示効果を向上させるこ
とができる。
As explained above, according to the present invention, it is possible to obtain multi-colored smoke such as a spotted pattern from an aircraft, and it is possible to improve the display effect.

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

第1図は本発明の第1の実施例の説明図、第2図は同実
施例によって発生する煙の説明図、第3図及び第4図は
それぞれ本発明の第2及び第3の実施例の説明図、第5
図は従来の航空機用発煙装置の説明図、第6図は同従来
の航空機用発煙装置によって発生する煙の説明図である
。 1^、IB−発煙油タンク、2A、2B−・発煙油、3
^、3B・−ポンプ、 4.4A、4B・・−ジェットエンジン、5A 5B・
バルブ、  6−エンジン排気、8−操作スイッチ、 
9A、9B−・発煙ノズル、10−・−コントローラ、
 IIA、IIB  −・通路、12−煙、  13 
 ジェットエンジンの排気管。 代理人 弁理士 坂 間   暁 外2名 第3図 第4図 第1図 第2図 第5図 第6図
FIG. 1 is an explanatory diagram of the first embodiment of the present invention, FIG. 2 is an explanatory diagram of smoke generated by the same embodiment, and FIGS. 3 and 4 are respectively the second and third embodiments of the present invention. Example illustration, 5th
FIG. 6 is an explanatory diagram of a conventional aircraft smoke generator, and FIG. 6 is an explanatory diagram of smoke generated by the conventional aircraft smoke generator. 1^, IB-fuming oil tank, 2A, 2B-・fuming oil, 3
^, 3B・-Pump, 4.4A, 4B・・-Jet engine, 5A 5B・
Valve, 6-engine exhaust, 8-operation switch,
9A, 9B-・Smoke nozzle, 10-・-Controller,
IIA, IIB--Aisle, 12-Smoke, 13
Jet engine exhaust pipe. Agent: Patent Attorney Akigai Sakama (2 people)Figure 3Figure 4Figure 1Figure 2Figure 5Figure 6

Claims (1)

【特許請求の範囲】[Claims] それぞれ異る顔料を混合した発煙油を収容する複数の発
煙油タンク、各発煙油タンクに接続されエンジン排気中
に開口する発煙ノズルを有する複数の通路、及び同通路
に設けられたバルブを開閉するコントローラを備えたこ
とを特徴とする航空機用多色煙発煙装置。
A plurality of smoke oil tanks each containing smoke oil mixed with different pigments, a plurality of passages connected to each smoke oil tank and having smoke nozzles that open into the engine exhaust, and valves provided in the passages that open and close. A multicolor smoke generator for aircraft, characterized by being equipped with a controller.
JP18676588A 1988-07-28 1988-07-28 Multi-color smoke fuming device for aircraft Pending JPH0237098A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP18676588A JPH0237098A (en) 1988-07-28 1988-07-28 Multi-color smoke fuming device for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP18676588A JPH0237098A (en) 1988-07-28 1988-07-28 Multi-color smoke fuming device for aircraft

Publications (1)

Publication Number Publication Date
JPH0237098A true JPH0237098A (en) 1990-02-07

Family

ID=16194241

Family Applications (1)

Application Number Title Priority Date Filing Date
JP18676588A Pending JPH0237098A (en) 1988-07-28 1988-07-28 Multi-color smoke fuming device for aircraft

Country Status (1)

Country Link
JP (1) JPH0237098A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2464161A (en) * 2008-10-11 2010-04-14 Stephen Desmond Lewis Aircraft Afterburner for Providing Coloured Flames
CN107487446A (en) * 2017-09-24 2017-12-19 宋忠春 A kind of smog ejecting device for model plane exhibition
CN111731484A (en) * 2020-05-21 2020-10-02 卓尔飞机制造(武汉)有限公司 General aircraft is with drawing cigarette device

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2464161A (en) * 2008-10-11 2010-04-14 Stephen Desmond Lewis Aircraft Afterburner for Providing Coloured Flames
GB2464161B (en) * 2008-10-11 2011-04-13 Stephen Desmond Lewis The airshow engine
CN107487446A (en) * 2017-09-24 2017-12-19 宋忠春 A kind of smog ejecting device for model plane exhibition
CN111731484A (en) * 2020-05-21 2020-10-02 卓尔飞机制造(武汉)有限公司 General aircraft is with drawing cigarette device
CN111731484B (en) * 2020-05-21 2021-03-12 卓尔飞机制造(武汉)有限公司 General aircraft is with drawing cigarette device

Similar Documents

Publication Publication Date Title
US5884611A (en) Effervescent injector for diesel engines
JPS5484128A (en) Internal combustion engine with two intake passages
KR950014565A (en) Internal combustion engine and mixer forming device of internal combustion engine
JPH10185109A (en) Method for operating burner
US4836453A (en) Fuel injector with continuous air flow
JPS5543269A (en) Intermittent gas injection valve
JPH0237098A (en) Multi-color smoke fuming device for aircraft
JP2632567B2 (en) Pneumatic fuel injector for cylinders of internal combustion engines
KR20040091396A (en) Apparatus for generating color flame
TW355192B (en) A two-stroke internal combustion engine
CN107191301A (en) A kind of air-fuel mixture injection apparatus
KR20050000023A (en) multi-color flame jets
JPS5762952A (en) Carburetor
ES8506378A1 (en) Fuel injection nozzles
KR100273586B1 (en) Fuel injection nozzle for diesel engine
CN105888903B (en) The double electromagnetism hybrid fuel jet devices of combined type
KR200328032Y1 (en) multi-color flame jets
SE7909166L (en) ARRANGEMENTS FOR CONVERSION OF CARBON GASES ON INCORPORATION ENGINES
CN109072849A (en) improved fuel injection device
JPS6187964A (en) Injection valve
JPH08177498A (en) Direct injection and spark-ignition type internal combustion engine
JPH0526135A (en) Intake deivce of compound intake valve type internal combustion engine
FR2354447A1 (en) Stratified charge IC engine - has inlet valve with shoulder to control flow from rich mixture duct
JPS57116150A (en) Internal combustion engine
KR100203874B1 (en) Intake device of engine