GB767637A - Improvements in or relating to a fluid circulating system - Google Patents

Improvements in or relating to a fluid circulating system

Info

Publication number
GB767637A
GB767637A GB958/55A GB95855A GB767637A GB 767637 A GB767637 A GB 767637A GB 958/55 A GB958/55 A GB 958/55A GB 95855 A GB95855 A GB 95855A GB 767637 A GB767637 A GB 767637A
Authority
GB
United Kingdom
Prior art keywords
motor
aircraft
air
fan
turbine
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
GB958/55A
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.)
Garrett Corp
Original Assignee
Garrett Corp
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 Garrett Corp filed Critical Garrett Corp
Publication of GB767637A publication Critical patent/GB767637A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D13/00Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D13/06Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
    • B64D13/08Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned the air being heated or cooled
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D13/00Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D13/06Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
    • B64D2013/0603Environmental Control Systems
    • B64D2013/0614Environmental Control Systems with subsystems for cooling avionics

Landscapes

  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Pulmonology (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Motor Or Generator Cooling System (AREA)

Abstract

767,637. Auxiliary power installations on aircraft. GARRETT CORPORATION. Jan. 12, 1955 [Jan. 18, 1954], No. 958/55. Class 4. [Also in Groups X and XIII] A ram air turbine 5 exposed to the air stream of an aircraft drives a pump 10 supplying hydraulic fluid driving a motor 12 coupled to a fan 27 which draws air or other gas such as hydrogen or nitrogen from a closed compartment 1 in the aircraft and returns it to that compartment through a duct 30, 31 in which the fan is located. The duct contains a cooler 32 through which coolant air from the turbine flows. The fluid driving the motor 12 returns to the pump through a pressurized sump 15 and a heat exchanger 20 cooled by air from the turbine. The motor also drives an electric generator 25 supplying electric equipment 2 in the compartment 1. The electric generator may be of the induction type so that it can act as an electric motor to drive the fan 27 when the aircraft is on the ground. The motor 12 has an integral speed control which limits its speed, and a byepass with a pressure relief valve 13.
GB958/55A 1954-01-18 1955-01-12 Improvements in or relating to a fluid circulating system Expired GB767637A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US767637XA 1954-01-18 1954-01-18

Publications (1)

Publication Number Publication Date
GB767637A true GB767637A (en) 1957-02-06

Family

ID=22134034

Family Applications (1)

Application Number Title Priority Date Filing Date
GB958/55A Expired GB767637A (en) 1954-01-18 1955-01-12 Improvements in or relating to a fluid circulating system

Country Status (1)

Country Link
GB (1) GB767637A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2985225A1 (en) * 2014-08-12 2016-02-17 Hamilton Sundstrand Corporation Ram air fan and power electronics cooling
EP2746160A3 (en) * 2012-12-21 2016-11-16 Hamilton Sundstrand Corporation Ejector assembly

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2746160A3 (en) * 2012-12-21 2016-11-16 Hamilton Sundstrand Corporation Ejector assembly
EP2985225A1 (en) * 2014-08-12 2016-02-17 Hamilton Sundstrand Corporation Ram air fan and power electronics cooling
US9832910B2 (en) 2014-08-12 2017-11-28 Hamilton Sundstrand Corporation Ram air fan and power electronics cooling systems
US10321604B2 (en) 2014-08-12 2019-06-11 Hamilton Sundstrand Corporation Ram air fan and power electronics cooling systems
US11246237B2 (en) 2014-08-12 2022-02-08 Hamilton Sundstrand Corporation Ram air fan and power electronics cooling systems

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