GB851441A - Improvements in air conditioning and/or air pressurising apparatus for aircraft - Google Patents

Improvements in air conditioning and/or air pressurising apparatus for aircraft

Info

Publication number
GB851441A
GB851441A GB1616756A GB1616756A GB851441A GB 851441 A GB851441 A GB 851441A GB 1616756 A GB1616756 A GB 1616756A GB 1616756 A GB1616756 A GB 1616756A GB 851441 A GB851441 A GB 851441A
Authority
GB
United Kingdom
Prior art keywords
air
compressor
turbine
aircraft
turbines
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
GB1616756A
Inventor
Henry William Groves
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.)
HAVILLAND PROPELLERS Ltd DE
De Havilland Propellers Ltd
Original Assignee
HAVILLAND PROPELLERS Ltd DE
De Havilland Propellers Ltd
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 HAVILLAND PROPELLERS Ltd DE, De Havilland Propellers Ltd filed Critical HAVILLAND PROPELLERS Ltd DE
Priority to GB1616756A priority Critical patent/GB851441A/en
Publication of GB851441A publication Critical patent/GB851441A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/10—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output supplying working fluid to a user, e.g. a chemical process, which returns working fluid to a turbine of the plant
    • F02C6/12—Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

851,441. Refrigerating. DE HAVILLAND PROPELLERS Ltd. May 22, 1957 [May 24, 1956], No. 16167/56. Class 29 In a refrigerating system for aircraft compressed air bled from the compressor of a gas turbine engine divides into two streams one flowing through compressor 1, heat exchanger 5, and expansion turbine 3 driving the compressor and the other flowing to a second turbine 2 also supplying power to the compressor 1. Exhaust air from turbines 2, 3 can be used respectively for cooling and cooling and/or pressurizing, although the air from turbine 2 can be exhausted to ambient. As shown, the speed of turbine 2 is regulated by air valve 6 controlled by speed pick-up 7 on the shaft of the turbines and compressor. The incoming air is cooled in exchanger 4; exchangers 4 and 5 may be water boilers.
GB1616756A 1956-05-24 1956-05-24 Improvements in air conditioning and/or air pressurising apparatus for aircraft Expired GB851441A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1616756A GB851441A (en) 1956-05-24 1956-05-24 Improvements in air conditioning and/or air pressurising apparatus for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1616756A GB851441A (en) 1956-05-24 1956-05-24 Improvements in air conditioning and/or air pressurising apparatus for aircraft

Publications (1)

Publication Number Publication Date
GB851441A true GB851441A (en) 1960-10-19

Family

ID=10072375

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1616756A Expired GB851441A (en) 1956-05-24 1956-05-24 Improvements in air conditioning and/or air pressurising apparatus for aircraft

Country Status (1)

Country Link
GB (1) GB851441A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1991000483A1 (en) * 1989-06-23 1991-01-10 Allied-Signal Inc. Ecs with advanced air cycle machine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1991000483A1 (en) * 1989-06-23 1991-01-10 Allied-Signal Inc. Ecs with advanced air cycle machine

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