JPS6276878U - - Google Patents

Info

Publication number
JPS6276878U
JPS6276878U JP1985165138U JP16513885U JPS6276878U JP S6276878 U JPS6276878 U JP S6276878U JP 1985165138 U JP1985165138 U JP 1985165138U JP 16513885 U JP16513885 U JP 16513885U JP S6276878 U JPS6276878 U JP S6276878U
Authority
JP
Japan
Prior art keywords
air
heat
air conditioning
engine
pipe
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
JP1985165138U
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 JP1985165138U priority Critical patent/JPS6276878U/ja
Publication of JPS6276878U publication Critical patent/JPS6276878U/ja
Pending legal-status Critical Current

Links

Classifications

    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
    • Y02A30/00—Adapting or protecting infrastructure or their operation
    • Y02A30/27—Relating to heating, ventilation or air conditioning [HVAC] technologies
    • Y02A30/274—Relating to heating, ventilation or air conditioning [HVAC] technologies using waste energy, e.g. from internal combustion engine

Landscapes

  • Air-Conditioning For Vehicles (AREA)

Description

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

第１図は本考案の航空機用空気調和装置を示す
系統図、第２図は同変形例を示す図である。 ２……キヤビン、Ｅ……空気調和用エンジン、
３……排気管、Ｃ１，Ｃ２……圧縮機、５，１６
……空気取入口、６……吸気管、７……送気管、
ＡＣ……エアサイクルマシーン、Ｔ……空気ター
ビン、８……空気冷却器、９……調和空気供給管
、１０ａ……空気吹出口、１１……調節弁、１２
……バイパス管、１４……熱交換器、Ｒ，Ｒ１…
…熱回収装置、２０……ヒートパイプ。 FIG. 1 is a system diagram showing an aircraft air conditioner according to the present invention, and FIG. 2 is a diagram showing a modification of the same. 2...cabin, E...air conditioning engine,
3...Exhaust pipe, C1, C2...Compressor, 5,16
...Air intake port, 6...Intake pipe, 7...Air supply pipe,
AC... Air cycle machine, T... Air turbine, 8... Air cooler, 9... Conditioned air supply pipe, 10a... Air outlet, 11... Control valve, 12
...Bypass pipe, 14...Heat exchanger, R, R1...
...Heat recovery device, 20...Heat pipe.

Claims (1)

【実用新案登録請求の範囲】 １ 推進用エンジンとは別に設けた空気調和用エ
ンジンと、この空気調和用エンジンにより駆動さ
れる第１の空気圧縮機と、空気調和すべきキヤビ
ン内の空気を第１の空気圧縮機の入口へ送るよう
にキヤビンと第１の空気圧縮機とを接続する吸気
管と、第１の空気圧縮機の出口に接続され、第２
の空気圧縮機、空気冷却器および空気タービンを
順次接続して構成されたエアサイクルマシーンと
、エアサイクルマシーンとキヤビン内部を接続す
る調和空気供給管と、前記エアサイクルマシーン
に並列をなして第１の空気圧縮機と調和空気供給
管とを接続するバイパス管と、このバイパス管に
設けた調節弁とからなる空気調和系を備え、前記
空気調和用エンジンの排気管部で排気ガスの熱を
回収して前記空気調和系へ供給する熱回収装置を
さらに備えた航空機用空気調和装置。 ２ 熱回収装置が、空気調和用エンジンの排気管
部に設けた熱交換器と、この熱交換器の一端をキ
ヤビンに接続する管と、熱交換器の他端を空気調
和系に接続する管とからなる実用新案登録請求の
範囲第１項記載の航空機用空気調和装置。 ３ 熱回収装置が、空気調和用エンジンの排気管
部に受熱部を、空気調和系に放熱部をそれぞれ有
するヒートパイプよりなる実用新案登録請求の範
囲第１項記載の航空機用空気調和装置。[Claims for Utility Model Registration] 1. An air conditioning engine provided separately from the propulsion engine, a first air compressor driven by the air conditioning engine, and a first air conditioning engine that controls the air in the cabin to be air conditioned. an intake pipe connecting the cabin and the first air compressor so as to feed the air to the inlet of the first air compressor;
an air cycle machine configured by sequentially connecting an air compressor, an air cooler, and an air turbine; a conditioned air supply pipe connecting the air cycle machine and the inside of the cabin; and a first air cycle machine in parallel with the air cycle machine. The air conditioning system includes a bypass pipe that connects the air compressor and the conditioned air supply pipe, and a control valve installed in the bypass pipe, and the heat of the exhaust gas is recovered in the exhaust pipe section of the air conditioning engine. An aircraft air conditioner further comprising a heat recovery device for supplying heat to the air conditioning system. 2. The heat recovery device includes a heat exchanger installed in the exhaust pipe of an air conditioning engine, a tube connecting one end of this heat exchanger to the cabin, and a tube connecting the other end of the heat exchanger to the air conditioning system. An air conditioner for an aircraft according to claim 1, comprising: 3. The aircraft air conditioner according to claim 1, wherein the heat recovery device is a heat pipe having a heat receiving part in the exhaust pipe part of the air conditioning engine and a heat radiating part in the air conditioning system.
JP1985165138U 1985-10-29 1985-10-29 Pending JPS6276878U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1985165138U JPS6276878U (en) 1985-10-29 1985-10-29

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1985165138U JPS6276878U (en) 1985-10-29 1985-10-29

Publications (1)

Publication Number Publication Date
JPS6276878U true JPS6276878U (en) 1987-05-16

Family

ID=31094895

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1985165138U Pending JPS6276878U (en) 1985-10-29 1985-10-29

Country Status (1)

Country Link
JP (1) JPS6276878U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2014516858A (en) * 2011-05-30 2014-07-17 ターボメカ Air conditioning system for aircraft passenger compartment

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2014516858A (en) * 2011-05-30 2014-07-17 ターボメカ Air conditioning system for aircraft passenger compartment

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