SU1777299A1 - Supersonic flying vehicle conditioning system - Google Patents

Supersonic flying vehicle conditioning system

Info

Publication number
SU1777299A1
SU1777299A1 SU987217/23A SU987217A SU1777299A1 SU 1777299 A1 SU1777299 A1 SU 1777299A1 SU 987217/23 A SU987217/23 A SU 987217/23A SU 987217 A SU987217 A SU 987217A SU 1777299 A1 SU1777299 A1 SU 1777299A1
Authority
SU
USSR - Soviet Union
Prior art keywords
flying vehicle
conditioning system
heat exchanger
air line
loop
Prior art date
Application number
SU987217/23A
Other languages
Russian (ru)
Inventor
А.Ф. Осипов
И.А. Яковлев
Original Assignee
Центральный аэрогидродинамический институт им.проф.Н.Е.Жуковского
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 Центральный аэрогидродинамический институт им.проф.Н.Е.Жуковского filed Critical Центральный аэрогидродинамический институт им.проф.Н.Е.Жуковского
Priority to SU987217/23A priority Critical patent/SU1777299A1/en
Application granted granted Critical
Publication of SU1777299A1 publication Critical patent/SU1777299A1/en

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
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Other Air-Conditioning Systems (AREA)

Abstract

FIELD: conditioning systems. SUBSTANCE: system consists of an open-loop air line which includes successively connected engine compressors 4, heat exchanger 3, and flying vehicle pressure cabin 5; and a closed-loop air line which includes successively connected pressure cabin 5, fan, and heat exchanger 2. A cooling loop is integrated in the system. The cooling loop consists of successively mounted thermally insulated tank 1 containing a liquified supercooled hydrocarbon, such as propane, heat exchangers 2, 3, and engines which burn the used propane. EFFECT: increased efficiency of operation, reduced mass of the system. 1 dwg
SU987217/23A 1967-09-16 1967-09-16 Supersonic flying vehicle conditioning system SU1777299A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU987217/23A SU1777299A1 (en) 1967-09-16 1967-09-16 Supersonic flying vehicle conditioning system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU987217/23A SU1777299A1 (en) 1967-09-16 1967-09-16 Supersonic flying vehicle conditioning system

Publications (1)

Publication Number Publication Date
SU1777299A1 true SU1777299A1 (en) 1994-05-15

Family

ID=60521725

Family Applications (1)

Application Number Title Priority Date Filing Date
SU987217/23A SU1777299A1 (en) 1967-09-16 1967-09-16 Supersonic flying vehicle conditioning system

Country Status (1)

Country Link
SU (1) SU1777299A1 (en)

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