GB731068A - Ice-eliminating system of the type using inflatable elements - Google Patents

Ice-eliminating system of the type using inflatable elements

Info

Publication number
GB731068A
GB731068A GB2135/52A GB213552A GB731068A GB 731068 A GB731068 A GB 731068A GB 2135/52 A GB2135/52 A GB 2135/52A GB 213552 A GB213552 A GB 213552A GB 731068 A GB731068 A GB 731068A
Authority
GB
United Kingdom
Prior art keywords
contacts
contact
units
valve
timer
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
GB2135/52A
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.)
Bendix Aviation Corp
Original Assignee
Bendix Aviation 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 Bendix Aviation Corp filed Critical Bendix Aviation Corp
Publication of GB731068A publication Critical patent/GB731068A/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
    • B64D15/00De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/16De-icing or preventing icing on exterior surfaces of aircraft by mechanical means
    • B64D15/166De-icing or preventing icing on exterior surfaces of aircraft by mechanical means using pneumatic boots

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Supply Devices, Intensifiers, Converters, And Telemotors (AREA)

Abstract

731,068. Aircraft ice eleminating systems. BENDIX AVIATION CORPORATION. Jan. 25, 1952 [Jan. 25, 1951], No. 2135/52.. Class 4. An ice eliminating system for an aircraft comprises a plurality of inflatable units 3 each associated with a distributer 18 adapted to connect the units to either the pressure supply line 15 or the suction line 8, being under the control of the timer 20. The suction line 8 is connected to pump 6, which feeds high pressure air to the valve 10, adapted to direct the air to the supply line 15 or the atmosphere, and which is also under the control of timer 20. The valve means 10 may be as described in Specification 646,737. The timer is shown in Fig. 2, wherein the shaft 35 driven by the electronic timing unit 21, which may be as described in Specification 655,437, [Group XL (c)], operates two contact arms 36 and 37, respectively controlling through contacts 36A-G and 37A-G, the distributers 18 and valve 10. The cycle of operation is that first contacts 36A and 37A are made, the latter operating solenoid 33 which operates valve 10 to supply fluid to the line 15. On contacts 36B-G and 37B-G, the fluid supply is maintained, and solenoids 39 operate distributers 18 to inflate each unit 3 in turn. For the remainder of the cycle (contacts 36 H-L and 37 H-L), the pump output is diverted to atmosphere, and all units 3 are deflated. By this arrangement, pump 6 works at high load for only part of the cycle, and a lower operating temperature is possible. In an alternative embodiment, only one contact arm is used to operate both sets of contacts, and the contacts 37A-G take the form of one strip, which may be so arranged that contact is made with it before the arm comes to contact 36B, and ends when the arm leaves contact 36G. The size of contacts 36A-G may be chosen so that contact is made for a period proportional to the cubic capacity of the corresponding units 3. Specifications 548,138, 621,490, and 621,497 also are referred to. Reference has been directed by the Comptroller to Specifications 548,138, 621,490, 621,497, 646,737 and 655,437, [Group XL (c)].
GB2135/52A 1951-01-25 1952-01-25 Ice-eliminating system of the type using inflatable elements Expired GB731068A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US731068XA 1951-01-25 1951-01-25

Publications (1)

Publication Number Publication Date
GB731068A true GB731068A (en) 1955-06-01

Family

ID=22111765

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2135/52A Expired GB731068A (en) 1951-01-25 1952-01-25 Ice-eliminating system of the type using inflatable elements

Country Status (1)

Country Link
GB (1) GB731068A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113148182A (en) * 2021-05-31 2021-07-23 中航(成都)无人机系统股份有限公司 Unmanned aerial vehicle and wing defroster thereof

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113148182A (en) * 2021-05-31 2021-07-23 中航(成都)无人机系统股份有限公司 Unmanned aerial vehicle and wing defroster thereof

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