GB801746A - Control device for deicing apparatus for aircraft - Google Patents

Control device for deicing apparatus for aircraft

Info

Publication number
GB801746A
GB801746A GB2875655A GB2875655A GB801746A GB 801746 A GB801746 A GB 801746A GB 2875655 A GB2875655 A GB 2875655A GB 2875655 A GB2875655 A GB 2875655A GB 801746 A GB801746 A GB 801746A
Authority
GB
United Kingdom
Prior art keywords
ice
operated
switch
members
valves
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
GB2875655A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB2875655A priority Critical patent/GB801746A/en
Publication of GB801746A publication Critical patent/GB801746A/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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047—Heating to prevent icing

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Hybrid Cells (AREA)

Abstract

801,746. Gas turbines. LEIGH, L. P. Oct. 10, 1955, No. 28756/55. Cla.ss 110 (3). [Also in Groups XXIX and XXXVII] Ice formation in duct 15 of an aircraft jet engine is prevented by providing one or more pitot members 35 which each normally produces a takeoff pressure different from the ambient pressure to keep open an electric switch; when ice closes one of the pilot openings the switch closes and opens solenoid-operated valves 24 and 24a which supply hot air from the engine to heat-exchangers H, H2 supplying heated air to a header D in the jet inlet and to the members 35 respectively. If ice-formation persists a valve 24b may be operated manually to bring heat exchanger H3 into operation. The electrical operation of valves 24 and 24a is conditional on the closure of a switch 68 actuated by a negative-pressure device 72 so that the heaters are only operated when airflow in the duct reaches a certain value. Specification 771,153 is referred to.
GB2875655A 1955-10-10 1955-10-10 Control device for deicing apparatus for aircraft Expired GB801746A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2875655A GB801746A (en) 1955-10-10 1955-10-10 Control device for deicing apparatus for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2875655A GB801746A (en) 1955-10-10 1955-10-10 Control device for deicing apparatus for aircraft

Publications (1)

Publication Number Publication Date
GB801746A true GB801746A (en) 1958-09-17

Family

ID=10280633

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2875655A Expired GB801746A (en) 1955-10-10 1955-10-10 Control device for deicing apparatus for aircraft

Country Status (1)

Country Link
GB (1) GB801746A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11662139B2 (en) 2018-07-17 2023-05-30 Carrier Corporation Refrigerated cargo container cargo sensor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11662139B2 (en) 2018-07-17 2023-05-30 Carrier Corporation Refrigerated cargo container cargo sensor

Similar Documents

Publication Publication Date Title
US2391838A (en) Air conditioning system
US2940258A (en) Supplying air to internal components of engines
US2491462A (en) Gas turbine driven air conditioning
US2459000A (en) Spill valve
US2644315A (en) System for the supply of conditioned air in aircraft
GB947186A (en) Fluid flow control apparatus
US2509899A (en) Aircraft air conditioning system
US2805571A (en) Supersonic wind tunnel
GB801746A (en) Control device for deicing apparatus for aircraft
US2917288A (en) Cabin temperature control system
US2614815A (en) Aircraft cabin pressurizing and air conditioning apparatus
GB673961A (en) Improvements relating to gas turbine power plant installations
GB904252A (en) Improvements relating to gas cooling systems
US2358835A (en) Pressure cabin control arrangement
GB344914A (en) Improvements relating to the ventilation of enclosures
GB906592A (en) Control systems for aircraft gas turbine engines
US2953078A (en) Distribution system for aircraft air conditioning
GB971224A (en) Gas turbine jet power plant
GB762970A (en) Temperature control system
SU142157A1 (en) The method of ventilation of clothing crew members of aircraft
GB756470A (en) Improvements in or relating to the control of rate of flow of air or other gases
GB979936A (en) Apparatus for cooling gases
GB681144A (en) Mechanism and method for conditioning air for an enclosure
GB686549A (en) Improvements in or relating to plants for supplying conditioned air to an aircraft pressure cabin
GB817975A (en) An air conditioning system