AT483632T

Ram air based cooling and ventilation system and method for an aircraft

Abstract

The present invention relates to a cooling system for airplanes provided with the inspiratory port (4) where air flows into the rum air pipeline (2) through an inspiratory port (4) from the circumference of an airplane, and the exhaust port (6) into which air flows out of the rum air pipeline (2) through an exhaust port (6). A heat exchanger (10) is arranged in a rum air pipeline (2). A ventilator (8) is open for free passage in fluid with a rum air pipeline (2). In order to cool at least one component parts of an airplane by which heat load was carried out, especially component parts in which heat load of the cabin air-conditioning system was carried out and/or to ventilate installation space of at least one component parts by which heat load was carried out, distribution tube way 12 and rum air pipeline 2 are connected.

Term

No projected expiry on record.

  1. Priority
  2. Filed
  3. Granted
  4. Today

19 members in 10 offices

This recordMember, by publication datePriority claim

Priority claims5

Priority claims
DocumentOfficeKindDate
102006060765GermanyA
87116806United States of AmericaP
102007023685GermanyA
93963307United States of AmericaP
2007010920European Patent Office (EPO)W

Members19

Family members, oldest first
DocumentOfficeKind
DE102006060765B3GermanyB3
CA2673488A1CanadaA1
US2008148747A1United States of AmericaA1
WO2008074433A1World Intellectual Property Organization (WIPO)A1
DE102007023685B3GermanyB3
EP2094565A1European Patent Office (EPO)A1
CN101657355AChinaA
US2010096118A1United States of AmericaA1
JP2010513119AJapanA
US7730728B2United States of AmericaB2
EP2094565B1European Patent Office (EPO)B1
AT483632TThis recordAustriaT
ATE483632T1AustriaT1
DE602007009722D1GermanyD1
RU2009125466ARussian FederationA
RU2449925C2Russian FederationC2
CN101657355BChinaB
BRPI0719485A2BrazilA2
US8707721B2United States of AmericaB2