SE7714234L - PROCEDURE FOR PROTECTING A SURFACE ON AN AIRCRAFT COMPONENT, AND AIRCRAFT COMPONENT PROVIDED WITH PROTECTIVE COATING ACCORDING TO THE INVENTION - Google Patents

PROCEDURE FOR PROTECTING A SURFACE ON AN AIRCRAFT COMPONENT, AND AIRCRAFT COMPONENT PROVIDED WITH PROTECTIVE COATING ACCORDING TO THE INVENTION

Info

Publication number
SE7714234L
SE7714234L SE7714234A SE7714234A SE7714234L SE 7714234 L SE7714234 L SE 7714234L SE 7714234 A SE7714234 A SE 7714234A SE 7714234 A SE7714234 A SE 7714234A SE 7714234 L SE7714234 L SE 7714234L
Authority
SE
Sweden
Prior art keywords
alloy
surface region
aircraft component
protecting
aircraft
Prior art date
Application number
SE7714234A
Other languages
Unknown language ( )
Swedish (sv)
Other versions
SE437004B (en
Inventor
B D Lazell
Original Assignee
Lucas Industries 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 Lucas Industries Ltd filed Critical Lucas Industries Ltd
Publication of SE7714234L publication Critical patent/SE7714234L/en
Publication of SE437004B publication Critical patent/SE437004B/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/38—Constructions adapted to reduce effects of aerodynamic or other external heating

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)

Abstract

A method of protecting a surface region of an aircraft against erosion by rain, airborne sand, hail and the like, includes starting with a sheet or sheets of a super-plastic alloy. The sheets of alloy are engaged with the surface region to be protected, and are then shaped, while at a temperature such that super-plastic properties of the alloy are exhibited, to follow the surface contours of the surface region to be protected. Thereafter the shaped sheet or sheets of alloy are secured in position on the surface region. The invention also resides in a surface region of an aircraft protected by a layer of superplastic alloy, and also in a protection member shaped to fit a particular aircraft surface region and formed from the superplastic alloy.
SE7714234A 1976-12-17 1977-12-15 USING A SUPER-PLASTIC MATERIAL TO PROTECT A SURFACE OF AN AIRCRAFT COMPONENT SE437004B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB52941/76A GB1593378A (en) 1976-12-17 1976-12-17 Aircraft surface structure

Publications (2)

Publication Number Publication Date
SE7714234L true SE7714234L (en) 1978-06-18
SE437004B SE437004B (en) 1985-02-04

Family

ID=10465925

Family Applications (1)

Application Number Title Priority Date Filing Date
SE7714234A SE437004B (en) 1976-12-17 1977-12-15 USING A SUPER-PLASTIC MATERIAL TO PROTECT A SURFACE OF AN AIRCRAFT COMPONENT

Country Status (10)

Country Link
JP (1) JPS5378599A (en)
BR (1) BR7708394A (en)
CA (1) CA1094526A (en)
DE (1) DE2756423A1 (en)
FR (1) FR2374109A1 (en)
GB (1) GB1593378A (en)
IN (1) IN149367B (en)
IT (1) IT1088448B (en)
NL (1) NL187567C (en)
SE (1) SE437004B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8609355D0 (en) * 1986-04-17 1986-09-17 Westland Plc Erosion shields for aerofoil surfaces
FR2694900B1 (en) * 1992-08-19 1994-10-21 Hispano Suiza Sa Method of manufacturing assemblies composed of two glued parts and comprising a forming step.
GB0913061D0 (en) 2009-07-28 2009-09-02 Rolls Royce Plc A method of manufacturing a reinforcing edge for a turbo machine aerofoil
US11964782B2 (en) 2022-07-11 2024-04-23 Wing Aviation Llc Formed-metal sheet airframe for UAVS

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1108081B (en) * 1955-01-20 1961-05-31 Sud Aviation Device for manufacturing a rotating sash
US3065940A (en) * 1956-06-22 1962-11-27 Emil L Eckstein Aircraft outer surface covering
US2959229A (en) * 1957-10-01 1960-11-08 United Aircraft Corp Nickel plated propeller blade
US3712566A (en) * 1971-02-25 1973-01-23 Us Navy Supersonic vehicle control surface having a thermally protective coating
DE2153434B2 (en) * 1971-10-27 1972-11-09 Licentia Patent Verwaltungs GmbH, 6000 Frankfurt FASTENING OF EROSION PROTECTION EDGES TO AIRPLANE PROFILES

Also Published As

Publication number Publication date
IT1088448B (en) 1985-06-10
IN149367B (en) 1981-11-21
JPS5378599A (en) 1978-07-12
FR2374109B1 (en) 1982-04-02
DE2756423A1 (en) 1978-06-22
NL187567C (en) 1991-11-18
BR7708394A (en) 1978-07-25
JPS6158359B2 (en) 1986-12-11
CA1094526A (en) 1981-01-27
SE437004B (en) 1985-02-04
NL187567B (en) 1991-06-17
FR2374109A1 (en) 1978-07-13
GB1593378A (en) 1981-07-15
NL7713936A (en) 1978-06-20
DE2756423C2 (en) 1988-11-10

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