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GB2001022A - Improvements in or relating to helicopter rotor blades - Google Patents

Improvements in or relating to helicopter rotor blades

Info

Publication number
GB2001022A
GB2001022A GB7827425A GB7827425A GB2001022A GB 2001022 A GB2001022 A GB 2001022A GB 7827425 A GB7827425 A GB 7827425A GB 7827425 A GB7827425 A GB 7827425A GB 2001022 A GB2001022 A GB 2001022A
Authority
GB
United Kingdom
Prior art keywords
ice
helicopter rotor
blade
relating
rotor blades
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.)
Granted
Application number
GB7827425A
Other versions
GB2001022B (en
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.)
SECR DEFENCE
UK Secretary of State for Defence
Original Assignee
SECR DEFENCE
UK Secretary of State for Defence
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 SECR DEFENCE, UK Secretary of State for Defence filed Critical SECR DEFENCE
Priority to GB7827425A priority Critical patent/GB2001022B/en
Publication of GB2001022A publication Critical patent/GB2001022A/en
Application granted granted Critical
Publication of GB2001022B publication Critical patent/GB2001022B/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
    • B64D15/12—De-icing or preventing icing on exterior surfaces of aircraft by electric heating

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Confectionery (AREA)

Abstract

To prevent the formation of ice upon a helicopter rotor blade and facilitate the shedding of ice formed thereon, an electrical heater is provided along the stagnation zone at the leading edge of the rotor blade, the surface 12 of the blade rearward of the stagnation zone having a coating of paste having a low adhesion for ice. In use, an area of the leading edge of the blade is maintained at a deicing temperature by the electrical heater. Ice which forms as a result of water run back from this area or which forms directly is shed by the paste. <IMAGE>
GB7827425A 1977-06-23 1978-06-20 Helicopter rotor blades Expired GB2001022B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB7827425A GB2001022B (en) 1977-06-23 1978-06-20 Helicopter rotor blades

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB2642977 1977-06-23
GB7827425A GB2001022B (en) 1977-06-23 1978-06-20 Helicopter rotor blades

Publications (2)

Publication Number Publication Date
GB2001022A true GB2001022A (en) 1979-01-24
GB2001022B GB2001022B (en) 1982-03-03

Family

ID=26258243

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7827425A Expired GB2001022B (en) 1977-06-23 1978-06-20 Helicopter rotor blades

Country Status (1)

Country Link
GB (1) GB2001022B (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2719182A1 (en) * 1990-11-21 1995-10-27 Onera (Off Nat Aerospatiale) Electrical de-icing system, e.g. for helicopter rotor blades
CN104890880A (en) * 2014-03-07 2015-09-09 波音公司 Systems and methods for passive deicing
CN107117318A (en) * 2017-03-22 2017-09-01 武汉航空仪表有限责任公司 A kind of preparation method of Fang ∕ deicing composite functional unit
CN110758767A (en) * 2019-10-12 2020-02-07 哈尔滨飞机工业集团有限责任公司 A helicopter rotor blade simulating transparent ice structure and integration method
GB2607884A (en) * 2021-06-11 2022-12-21 Ubiq Aerospace As System and method for deicing of a carbon composite propeller

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2719182A1 (en) * 1990-11-21 1995-10-27 Onera (Off Nat Aerospatiale) Electrical de-icing system, e.g. for helicopter rotor blades
CN104890880A (en) * 2014-03-07 2015-09-09 波音公司 Systems and methods for passive deicing
EP2915747A1 (en) * 2014-03-07 2015-09-09 The Boeing Company Systems and methods for passive deicing
US9199741B2 (en) 2014-03-07 2015-12-01 The Boeing Company Systems and methods for passive deicing
CN104890880B (en) * 2014-03-07 2019-02-01 波音公司 System and method for passive deicing
CN107117318A (en) * 2017-03-22 2017-09-01 武汉航空仪表有限责任公司 A kind of preparation method of Fang ∕ deicing composite functional unit
CN107117318B (en) * 2017-03-22 2019-10-18 武汉航空仪表有限责任公司 A kind of preparation method of anti-/ deicing composite material functional unit
CN110758767A (en) * 2019-10-12 2020-02-07 哈尔滨飞机工业集团有限责任公司 A helicopter rotor blade simulating transparent ice structure and integration method
CN110758767B (en) * 2019-10-12 2023-07-21 哈尔滨飞机工业集团有限责任公司 Helicopter rotor blade simulation transparent ice structure and integration method
GB2607884A (en) * 2021-06-11 2022-12-21 Ubiq Aerospace As System and method for deicing of a carbon composite propeller
GB2607884B (en) * 2021-06-11 2023-11-15 Ubiq Aerospace As System and method for deicing of a carbon composite propeller

Also Published As

Publication number Publication date
GB2001022B (en) 1982-03-03

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee