GB793949A - Improvements relating to means for distributing fluids - Google Patents

Improvements relating to means for distributing fluids

Info

Publication number
GB793949A
GB793949A GB32895/54A GB3289554A GB793949A GB 793949 A GB793949 A GB 793949A GB 32895/54 A GB32895/54 A GB 32895/54A GB 3289554 A GB3289554 A GB 3289554A GB 793949 A GB793949 A GB 793949A
Authority
GB
United Kingdom
Prior art keywords
wall
cavity
liquid
aircraft
air
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
GB32895/54A
Inventor
Stuart Halbert
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.)
T K S (Aircraft de-Icing) Ltd
Original Assignee
T K S (Aircraft de-Icing) 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 T K S (Aircraft de-Icing) Ltd filed Critical T K S (Aircraft de-Icing) Ltd
Priority to GB32895/54A priority Critical patent/GB793949A/en
Publication of GB793949A publication Critical patent/GB793949A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/16—De-icing or preventing icing on exterior surfaces of aircraft by mechanical means

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

793,949. Deicing aircraft. T.K.S. (AIRCRAFT DE-ICING), Ltd. Nov. 9, 1955 [Nov. 12, 1954], No. 32895/54. Class 4. A device for distributing liquid, e.g. for deicing the leading edge of a rotary-wing aircraft rotor blade, comprises an outer wall 1, Fig. 1, of porous material, an inner wall 2 of porous material, forming a cavity 3 with the outer wall, a third impervious wall 4 forming a cavity 5 with the inner wall 2, means for introducing liquid or a liquid and air mixture into the cavity 3, means for introducing air into the cavity 5, and means for rotating the device so that the liquid and air are urged outwardly. Fig. 2 shows an alternative embodiment in which a nickel-copper alloy extrusion 7 is set in the leading edge of a rotor blade, the extrusion having a transverse portion 8 formed with a spanwise series of holes or slots 9. A porous outer wall 10 and inner wall 12 form cavities 13, 14 used as before. Specification 724,019 is referred to.
GB32895/54A 1954-11-12 1954-11-12 Improvements relating to means for distributing fluids Expired GB793949A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB32895/54A GB793949A (en) 1954-11-12 1954-11-12 Improvements relating to means for distributing fluids

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB32895/54A GB793949A (en) 1954-11-12 1954-11-12 Improvements relating to means for distributing fluids

Publications (1)

Publication Number Publication Date
GB793949A true GB793949A (en) 1958-04-23

Family

ID=10345641

Family Applications (1)

Application Number Title Priority Date Filing Date
GB32895/54A Expired GB793949A (en) 1954-11-12 1954-11-12 Improvements relating to means for distributing fluids

Country Status (1)

Country Link
GB (1) GB793949A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2933443A1 (en) * 2008-07-02 2010-01-08 Snecma Rotor tip for turbomachine compressor of airplane, has container containing de-icing fluid, and equipped with filling valve, and distribution orifices for distributing de-icing fluid through calibrated opening
CN112682174A (en) * 2020-12-15 2021-04-20 南京航空航天大学 Anti-icing structure suitable for aeroengine extension board and wing

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2933443A1 (en) * 2008-07-02 2010-01-08 Snecma Rotor tip for turbomachine compressor of airplane, has container containing de-icing fluid, and equipped with filling valve, and distribution orifices for distributing de-icing fluid through calibrated opening
US8322125B2 (en) 2008-07-02 2012-12-04 Snecma Turbo-engine compressor tip comprising de-icing means
CN112682174A (en) * 2020-12-15 2021-04-20 南京航空航天大学 Anti-icing structure suitable for aeroengine extension board and wing

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