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
Other languages
English (en)
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/de
Priority claimed from DE19691930990 external-priority patent/DE1930990C3/de
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

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28C—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA COME INTO DIRECT CONTACT WITHOUT CHEMICAL INTERACTION
    • F28C3/00—Other 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)
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 (de) 1969-03-05 Als Drallkammer ausgebildete Kammer zum Kuhlen von heißen Gasen, insbesondere Brenngasen
DE19691930990 DE1930990C3 (de) 1969-06-19 1969-06-19 Als Drallkammer ausgebildete Kammer zum Kühlen von heißen Gasen, insbesondere Brenngasen

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 (enExample)
CH (1) CH496222A (enExample)
FR (1) FR2034662A7 (enExample)
GB (1) GB1300962A (enExample)

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 (fr) * 1959-08-14 1960-09-23 Commissariat Energie Atomique Procédé et appareil pour la purification continue de l'hexafluorure d'uranium par centrifugation et caléfaction
NL302523A (enExample) * 1962-12-24
US3534555A (en) * 1968-03-06 1970-10-20 Webb James E Laminar flow enhancement

Also Published As

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

Similar Documents

Publication Publication Date Title
FR2155492A5 (enExample)
ES382254A1 (es) Un proyectil trazador.
SE7704691L (sv) Fast framdrivningsmedel med forbrenningshastighetskatalysator
GB1300962A (en) Improvements in cooling chambers for cooling hot gases
GB1487064A (en) Wall structure for hot fluid streams
GB1243795A (en) Vane motor assemblies
GB1012004A (en) Improvements in or relating to compression-ignition internal combustion engines
ES264970U (es) "dispositivo para la refrigeracion del interior de una turbina de gas".
JPS55139942A (en) Cylinder of forced high speed water cooled engine
GB961001A (en) Improvements in propulsion units having a plurality of reaction propulsion nozzles
ES363554A1 (es) Perfeccionamientos en la construccion de dispositivos de estanquidad para arboles de maquinas giratorias.
GB1016489A (en) Fuel injector
GB1230657A (enExample)
GB1410229A (en) Hot-gas engine
ES450470A1 (es) Tobera de alto horno.
GB1448650A (en) Explosive projective
JPS5444710A (en) Electromagnet of ebullition cooling type
ES348397A1 (es) Aparato para mezclar fluidos a alta presion a diferentes temperaturas.
JPS5783697A (en) Barrel type casing
JPS5337210A (en) Cooling structure for steam turbine rotor
KALISKI Trans-shock velocity thermal sources in perfect gas
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)
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

Legal Events

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