GB1300962A - Improvements in cooling chambers for cooling hot gases - Google Patents

Improvements in cooling chambers for cooling hot gases

Info

Publication number
GB1300962A
GB1300962A GB9641/70A GB964170A GB1300962A GB 1300962 A GB1300962 A GB 1300962A GB 9641/70 A GB9641/70 A GB 9641/70A GB 964170 A GB964170 A GB 964170A GB 1300962 A GB1300962 A GB 1300962A
Authority
GB
United Kingdom
Prior art keywords
cooling
gases
lining
hot gases
casing
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
GB9641/70A
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm 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
Priority claimed from DE19691911078 external-priority patent/DE1911078C/en
Priority claimed from DE19691930990 external-priority patent/DE1930990C3/en
Application filed by Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of GB1300962A publication Critical patent/GB1300962A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28CHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA COME INTO DIRECT CONTACT WITHOUT CHEMICAL INTERACTION
    • F28C3/00Other direct-contact heat-exchange apparatus

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physical Or Chemical Processes And Apparatus (AREA)

Abstract

1300962 Cooling gases by contact with solids MESSERSCHMITT - BOLKOW - BLOHM GmbH 27 Feb 1970 [5 March 1969 19 June 1969] 9641/70 Heading F4K [Also in Division F1] A chamber for cooling hot gases, e.g. rocket combustion gases, comprises a casing 1 having oblique inlets 5 for the hot gases and a lining 2 of a material snch as ammonium oxalate which is gradually vaporized by the swirling gases, the latter being cooled in the process. Cooling is assisted by axial grooves 3 in the lining which set up eddies 6. The cooled gases leave through an outlet 1a. In a modification, Fig. 4 (not shown), the coolant lining (12) is provided only on a part of the front end face (8) of the casing 1 opposite outlet la.
GB9641/70A 1969-03-05 1970-02-27 Improvements in cooling chambers for cooling hot gases Expired GB1300962A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19691911078 DE1911078C (en) 1969-03-05 Chamber designed as a swirl chamber for cooling hot gases, in particular fuel gases
DE19691930990 DE1930990C3 (en) 1969-06-19 1969-06-19 Chamber designed as a swirl chamber for cooling hot gases, in particular fuel gases

Publications (1)

Publication Number Publication Date
GB1300962A true GB1300962A (en) 1972-12-29

Family

ID=25757082

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9641/70A Expired GB1300962A (en) 1969-03-05 1970-02-27 Improvements in cooling chambers for cooling hot gases

Country Status (4)

Country Link
US (1) US3667241A (en)
CH (1) CH496222A (en)
FR (1) FR2034662A7 (en)
GB (1) GB1300962A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8099966B2 (en) * 2006-10-18 2012-01-24 Textron Innovations Inc. System and method for controlling an environment in an aircraft using a vortex cooler
US9737933B2 (en) 2012-09-28 2017-08-22 General Electric Company Process of fabricating a shield and process of preparing a component

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2955432A (en) * 1958-05-30 1960-10-11 Shell Oil Co Vortex tube with internal cooling
FR1241864A (en) * 1959-08-14 1960-09-23 Commissariat Energie Atomique Method and apparatus for the continuous purification of uranium hexafluoride by centrifugation and calfaction
NL302523A (en) * 1962-12-24
US3534555A (en) * 1968-03-06 1970-10-20 Webb James E Laminar flow enhancement

Also Published As

Publication number Publication date
US3667241A (en) 1972-06-06
CH496222A (en) 1970-09-15
FR2034662A7 (en) 1970-12-11

Similar Documents

Publication Publication Date Title
FR2155492A5 (en)
GB1300962A (en) Improvements in cooling chambers for cooling hot gases
ES382254A1 (en) Tracer projectile
GB1487064A (en) Wall structure for hot fluid streams
GB1012004A (en) Improvements in or relating to compression-ignition internal combustion engines
JPS55139942A (en) Cylinder of forced high speed water cooled engine
ES363554A1 (en) Improvements in and relating to sealing devices
GB961001A (en) Improvements in propulsion units having a plurality of reaction propulsion nozzles
GB1230657A (en)
GB1410229A (en) Hot-gas engine
ES264970U (en) Means for internally cooling a gas turbine.
ES450470A1 (en) Blast furnace tuyere
JPS5444710A (en) Electromagnet of ebullition cooling type
ES348397A1 (en) Apparatus for Mixing High Pressure Fluids
JPS5337210A (en) Cooling structure for steam turbine rotor
SPIRIDONOV et al. Generalized characteristic of peripheral nonuniformity in the temperature field of a gas at the outlet of a gas-turbine engine combustion chamber(Gas turbine engine combustion chamber outlet, noting gas flow temperature field peripheral nonuniformity)
SHEVCHENKO et al. The effect of the scheme for gas distribution on the characteristics of a gas turbine combustion chamber
FAUCHAIS et al. Calculation of the thermodynamic functions of perfect gas mixtures at high temperature, taking into account Debye-type electrostatic interactions(Perfect gas mixtures thermodynamic functions at high temperatures with correction for Debye-type electrostatic interaction effects)
SOLOKHIN Mechanism of fuel combustion in a secondary-air feed zone, and the influence of secondary air stream feed depth on the characteristics of gas turbine engine chambers(Characteristics of gas turbine chamber dependence on secondary air stream depth, noting temperature, pressure and electroconductivity of combustion)
GB1450379A (en) Rocket motor propellant injectors
SU732554A1 (en) ROTOR OF MULTISTLE GAS TURBINE WITH LIQUID COOLING SYSTEM
GB997852A (en) Aerofoil blade for use in a hot fluid stream
BORDOVITSYN et al. Influence of the shape of an active-gas nozzle on the characteristics of a gas ejector with a short mixing chamber(Nozzle geometry effects on turbine gas ejector characteristics)
GB581091A (en) Improvements in or relating to methods of, and apparatus for, the combustion of gaseous fuel
GB1029937A (en) Enclosure body for rotary piston engines

Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee