JPS59125070A - Pitot tube - Google Patents

Pitot tube

Info

Publication number
JPS59125070A
JPS59125070A JP23215082A JP23215082A JPS59125070A JP S59125070 A JPS59125070 A JP S59125070A JP 23215082 A JP23215082 A JP 23215082A JP 23215082 A JP23215082 A JP 23215082A JP S59125070 A JPS59125070 A JP S59125070A
Authority
JP
Japan
Prior art keywords
heat pipe
pressure tube
static pressure
tube
led out
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
JP23215082A
Other languages
Japanese (ja)
Inventor
Seiichi Takahashi
清一 高橋
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 JP23215082A priority Critical patent/JPS59125070A/en
Publication of JPS59125070A publication Critical patent/JPS59125070A/en
Pending legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
    • G01P5/14Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid
    • G01P5/16Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid using Pitot tubes, e.g. Machmeter
    • G01P5/165Arrangements or constructions of Pitot tubes

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Abstract

PURPOSE:To use a titled Pitot tube very easily and to derive a flow velocity, etc. of a fluid by constituting it of a heat pipe, a full pressure tube and a static pressure tube. CONSTITUTION:One end 1A of a heat pipe 1 which is bent in the shape of L is an evaporating part, and the other end 1B is a condensing part. A wick 2 consisting of a metallic net, a sintered metal, or a group, etc. is formed on the inside circumferential surface of the cylindrical heat pipe 1. A full pressure tube 4 passes through in the axial core direction of the heat pipe 1, its tip 4A is opened to the evaporating part end face of one end 1A of the heat pipe 1, and its rear end 4B is led out of the condensing part of the other end 1B of the heat pipe 1. The tip 5A of a pair of static pressure tubes 5 is opened at a position of 180 deg. of the evaporating part side face of one end 1A of the heat pipe 1, and the rear end 5B passes through the inside of the heat pipe 1 and is led out of the condensing part of the other end 1B. The full pressure tube 4 and the static pressure tube 5 are formed so as to be contained in this heat pipe 1, therefore, they are not heated themselves and the full pressure and the static pressure can be led out.

Description

【発明の詳細な説明】 る。[Detailed description of the invention] Ru.

流体の流速や流向を測定する場合には.ピトー管がよく
使用されている。ピトー管とは通常3孔,あるいは、5
孔を有しており,たとえばその孔の1つを流れ方向に向
けて全圧を導入し他の孔より静圧を導入し,その圧力を
全圧管および静圧管によってマノメータなどの差圧計に
導き,流速などを求めるものである。
When measuring the flow velocity and direction of fluid. Pitot tubes are commonly used. A pitot tube usually has 3 or 5 holes.
It has holes, for example, one of the holes faces the flow direction to introduce total pressure and the other hole introduces static pressure, and that pressure is guided to a differential pressure gauge such as a manometer through a total pressure pipe and a static pressure pipe. , flow velocity, etc.

流体として燃焼排ガスなど高温の流れを測定する場合に
は.全圧管および静圧管を冷却してやる必要があり,従
来は水冷式のピ)一一管を使用していた。
When measuring a high temperature flow such as combustion exhaust gas as a fluid. It is necessary to cool the total pressure tube and the static pressure tube, and conventionally water-cooled pipes have been used.

しかし、水冷のための水の給排設備が必要となるゆど、
手軽に使用できるはずのピトー管の取扱いも面倒なもの
であった。
However, water supply and drainage equipment is required for water cooling.
The pitot tube, which should be easy to use, was also troublesome to handle.

本発明のピトー管は.筒状をなし一端に蒸発部,他端に
凝縮部を有するヒートパイプと,同ヒートパイプの軸芯
方向に貫通し先端がヒーI・パイプの一端蒸発部端面に
開口し後端がヒートパイプの他端凝縮部より導出される
全圧管と。
The pitot tube of the present invention is. A heat pipe that is cylindrical in shape and has an evaporation section at one end and a condensation section at the other end, and a heat pipe that penetrates in the axial direction of the heat pipe and has a tip opening at the end surface of the evaporation section at one end of the heat pipe and a rear end of the heat pipe. and a total pressure pipe led out from the condensing section at the other end.

先端がヒートパイプの一端蒸発部側面に開口し後端がヒ
ートパイプ内部を通りその他端凝縮部より導出される静
圧管とからなるものであるので,極めて簡単に使用し流
体の流速などを求めることができるようになる。
It consists of a static pressure tube whose tip opens on the side of the evaporating section of the heat pipe, and whose rear end passes through the inside of the heat pipe and is led out from the condensing section at the other end, so it is extremely easy to use and can be used to determine the flow velocity of fluid, etc. You will be able to do this.

以下9本発明を第1図に示す一実施例のピトー管により
説明する。
The present invention will be explained below using an embodiment of a pitot tube shown in FIG.

図において1はL字状に曲げられたヒートパイプであっ
て、一端IAを蒸発部とし、他@IBが凝縮部となって
いる。筒状をなすヒートパイプエの内周面には、金属性
網、焼結金属、あるいは、グループなどからなるウィッ
ク2が形成されており、使用温度により水・アルコール
・ナトリウム・フレオンなどから適宜選択される動作液
3が毛細管現象によりウィック2内を移動する。
In the figure, 1 is a heat pipe bent into an L-shape, with one end IA serving as an evaporating part and the other end @IB serving as a condensing part. A wick 2 made of metal net, sintered metal, or group is formed on the inner peripheral surface of the cylindrical heat pipe, and the wick 2 is appropriately selected from water, alcohol, sodium, freon, etc. depending on the operating temperature. The working liquid 3 moves within the wick 2 by capillary action.

4は全圧管であって、ヒートパイプ1の軸芯方向に貫通
し、その先端4Aがヒートパイプ1の一端IA蒸発部端
面に開口して、後端4Bがヒートパイプ1の他端IB凝
縮部より導出される、      ′ 5は一対の静圧管であって、その先端5Aがヒートパイ
プ1の一端15蒸発部側面180度の位置に開口してい
て、後端5Bがヒートパイプ1内部を通り他端IB凝縮
部より導出される。
Reference numeral 4 denotes a full-pressure tube that penetrates the heat pipe 1 in the axial direction, with its tip 4A opening at the end face of the evaporator section of the heat pipe 1 at one end IA, and its rear end 4B opening at the end surface of the IB condensing section at the other end of the heat pipe 1. ' 5 is a pair of static pressure tubes, the tip 5A of which opens at a position 180 degrees from the side of the evaporation part 15 of the heat pipe 1, and the rear end 5B passes through the inside of the heat pipe 1. It is led out from the end IB condensing section.

なお、これら全圧東4および静圧管5は2図示しないマ
ノメータなどの差圧計に連接している。
The total pressure pipe 4 and the static pressure pipe 5 are connected to a differential pressure gauge such as a manometer (not shown).

6は、と−トパイプ1の他端IB凝縮部外周に取り付け
られた放熱用のフィンである。
Reference numeral 6 denotes a heat dissipation fin attached to the outer periphery of the condensing section at the other end of the exhaust pipe 1.

さて、このようにしてなるピト−管を排ガス煙道中に挿
入するが、ヒートパイプ1の他側IB凝縮部は煙道外に
あるようにする。
Now, the pitot tube thus formed is inserted into the exhaust gas flue, but the IB condensing section on the other side of the heat pipe 1 is placed outside the flue.

ヒートパイプ1がガスにより加熱されると内部に封入さ
れた動作液3が蒸発して熱を奪う。
When the heat pipe 1 is heated by gas, the working fluid 3 sealed inside evaporates and removes heat.

蒸発はヒートパイプ1の他端IB凝縮部へ流れて行き、
放熱用のフィン6を介して熱を発散させ液化する。なお
、液化した動作液3は、ウィック2内を移動して蒸発部
に戻り、このサイクルをくり返す。従って、ヒートパイ
プ1は絶す熱を発散させており、自己冷却をしている訳
である。
The evaporation flows to the other end of the heat pipe 1 IB condensing section,
The heat is dissipated through the heat dissipation fins 6 and liquefied. Note that the liquefied working fluid 3 moves within the wick 2 and returns to the evaporation section, and this cycle is repeated. Therefore, the heat pipe 1 is dissipating endless heat and is self-cooling.

全圧管4おまび静圧管5は、このヒートパイプl内に収
納された形になっているので、自身は加熱されることな
く全圧および静圧を導出することができる。
Since the total pressure tube 4 and the static pressure tube 5 are housed within the heat pipe 1, they can derive the total pressure and static pressure without being heated themselves.

このように1本実施例のピトー管によると。Thus, according to the Pitot tube of this embodiment.

冷却水を使用しないで済むので、水配管、用水などが不
要であり、特別な準備をすることなしに高温流体の流速
などを測定することが可能となるー なお、上記実施例ではヒートパイプ1の内面にのみウィ
ック2を形成するようにしたが、全圧管4や静圧管5の
外面にもウィックを形成するようにしてももちろん良い
Since there is no need to use cooling water, there is no need for water piping, water, etc., and it is possible to measure the flow velocity of high temperature fluid without making any special preparations.In the above example, the heat pipe 1 Although the wick 2 is formed only on the inner surface of the tube, it is of course possible to form the wick on the outer surface of the total pressure tube 4 and the static pressure tube 5 as well.

また、特に熱流が大きい部分のヒートパイプ1外周に、
断熱材などを配置するようにしても良い。
In addition, on the outer periphery of the heat pipe 1, where the heat flow is particularly large,
A heat insulating material or the like may be placed.

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

第1図は本発明の一実施例を示すピトー管の図である。 2:ウィソク、3:動作゛液、4:全圧管。 5:静圧管、6:フィン FIG. 1 is a diagram of a pitot tube showing one embodiment of the present invention. 2: Wisoku, 3: Operating liquid, 4: Full pressure pipe. 5: Static pressure tube, 6: Fin

Claims (1)

【特許請求の範囲】[Claims] 筒状をなし一端に蒸発部、他端に凝縮部を有するヒート
パイプと、同ヒートパイプの軸芯方向に貫通し先端がヒ
ートパイプの一端蒸発部端面に開口し後端がヒートパイ
プの他端凝縮部より導出される全圧管と、先端がヒート
パイプの一端蒸発部側面に開口し後端がヒートパイプ内
部を通りその他端凝縮部より導出される静圧管とからな
ることを特徴とするピトー管。
A heat pipe that is cylindrical in shape and has an evaporation section at one end and a condensation section at the other end, and a heat pipe that penetrates in the axial direction of the heat pipe, with the tip opening at the end surface of the evaporation section at one end of the heat pipe, and the rear end at the other end of the heat pipe. A pitot tube consisting of a total pressure tube led out from a condensing section, and a static pressure tube whose tip opens on the side of the evaporation section at one end of the heat pipe, and whose rear end passes inside the heat pipe and leads out from the condensing section at the other end. .
JP23215082A 1982-12-29 1982-12-29 Pitot tube Pending JPS59125070A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP23215082A JPS59125070A (en) 1982-12-29 1982-12-29 Pitot tube

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP23215082A JPS59125070A (en) 1982-12-29 1982-12-29 Pitot tube

Publications (1)

Publication Number Publication Date
JPS59125070A true JPS59125070A (en) 1984-07-19

Family

ID=16934774

Family Applications (1)

Application Number Title Priority Date Filing Date
JP23215082A Pending JPS59125070A (en) 1982-12-29 1982-12-29 Pitot tube

Country Status (1)

Country Link
JP (1) JPS59125070A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3039515A1 (en) * 2015-07-28 2017-02-03 Thales Sa HEATING FOR AERONAUTICAL EQUIPMENT
FR3039513A1 (en) * 2015-07-28 2017-02-03 Thales Sa PROCESS FOR THE ADDITIVE MANUFACTURE OF AERONAUTICAL EQUIPMENT

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3039515A1 (en) * 2015-07-28 2017-02-03 Thales Sa HEATING FOR AERONAUTICAL EQUIPMENT
FR3039513A1 (en) * 2015-07-28 2017-02-03 Thales Sa PROCESS FOR THE ADDITIVE MANUFACTURE OF AERONAUTICAL EQUIPMENT
US9975639B2 (en) 2015-07-28 2018-05-22 Thales Biphase heating
US10234475B2 (en) 2015-07-28 2019-03-19 Thales Additive manufacturing method for an avionic equipment

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