GB275625A - Process for the working of engines for the propulsion of aircraft - Google Patents

Process for the working of engines for the propulsion of aircraft

Info

Publication number
GB275625A
GB275625A GB20487/27A GB2048727A GB275625A GB 275625 A GB275625 A GB 275625A GB 20487/27 A GB20487/27 A GB 20487/27A GB 2048727 A GB2048727 A GB 2048727A GB 275625 A GB275625 A GB 275625A
Authority
GB
United Kingdom
Prior art keywords
vapour
aircraft
engines
siemens
liquid
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.)
Expired
Application number
GB20487/27A
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.)
Siemens Schuckertwerke AG
Siemens AG
Original Assignee
Siemens Schuckertwerke AG
Siemens AG
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 Siemens Schuckertwerke AG, Siemens AG filed Critical Siemens Schuckertwerke AG
Publication of GB275625A publication Critical patent/GB275625A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

275,625. Siemens - Schuchertwerke Akt.-Ges., (Assignees of Siemens-Schuckertwerke Ges.). Aug. 6, 1926, [Convention date]. Vapour engines.-In a vapour engine for use on aircraft, substances, for example toluol, are used which are liquid at ordinary temperatures and pressures, which have melting points at or below 50 C., and which have a low heat content relative to steam at the same pressure. The vapour may be generated at the critical temperature and pressure, and the fluid may be burnt to heat the generator. The liquid may be preheated by vapour bled from the prime mover. Reference has been directed by the Comptroller to Specifications 11060/02, 6209/03 and 15266/04.
GB20487/27A 1926-08-06 1927-08-03 Process for the working of engines for the propulsion of aircraft Expired GB275625A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE275625X 1926-08-06

Publications (1)

Publication Number Publication Date
GB275625A true GB275625A (en) 1928-11-05

Family

ID=6026370

Family Applications (1)

Application Number Title Priority Date Filing Date
GB20487/27A Expired GB275625A (en) 1926-08-06 1927-08-03 Process for the working of engines for the propulsion of aircraft

Country Status (1)

Country Link
GB (1) GB275625A (en)

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