GB2354962A - Airfoil holding device - Google Patents

Airfoil holding device Download PDF

Info

Publication number
GB2354962A
GB2354962A GB9919114A GB9919114A GB2354962A GB 2354962 A GB2354962 A GB 2354962A GB 9919114 A GB9919114 A GB 9919114A GB 9919114 A GB9919114 A GB 9919114A GB 2354962 A GB2354962 A GB 2354962A
Authority
GB
United Kingdom
Prior art keywords
airfoil
holding device
control surface
including those
surface including
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.)
Withdrawn
Application number
GB9919114A
Other versions
GB9919114D0 (en
Inventor
Colin Arthur Pugh
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 GB9919114A priority Critical patent/GB2354962A/en
Publication of GB9919114D0 publication Critical patent/GB9919114D0/en
Publication of GB2354962A publication Critical patent/GB2354962A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B25HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25HWORKSHOP EQUIPMENT, e.g. FOR MARKING-OUT WORK; STORAGE MEANS FOR WORKSHOPS
    • B25H1/00Work benches; Portable stands or supports for positioning portable tools or work to be operated on thereby
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B25HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25BTOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
    • B25B11/00Work holders not covered by any preceding group in the subclass, e.g. magnetic work holders, vacuum work holders

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Load-Engaging Elements For Cranes (AREA)

Abstract

An airfoil holding device has jaws pivoted to accommodate the tapered cross section. They may also be pivoted to accommodate spanwise taper and a safety strap may be provided to prevent the airfoil slipping between the jaws. The support legs may fold for flat storage.

Description

2354962 DESIGN FOR AIRFOIL HOLDING DEVICE.
This invention relates to the safe holding and protection of airfoil sections such as aircraft ailerons,elevators,rudders and wings etc. and any tapered units of similar shape.
It is the object of this invention to provide a safe holding fixture for said airfoil or similar sections to enable these items to be held at a convenient height and angle for repairs and servicing to be carried out and to facilitate the safe transportation and storage of such items and also provide space saving in hangars and workshops by being constructed of lightweight tubular steel in such a manner that they may be folded when not in use.
Generally two airfoil holding devices are required to hold average control surfaces although more may be used for larger sections.
The version depicted is the smallest of the intended versions.
C.A.PUGH 189A TOPSHAM ROAD EXETER..EX2 6AN The two tubular frames 10 hinge at Pivot B' with drilled lugs to allow the frames to fold flat for storage. Passing through the centre, of the top brackets 6 and the main tubular frame assembly 10 is a spindle bolt to facilitate the automatic adjustment of the contacting faces of the Pad Assembly 12. This arrangement may be enhanced by the addition of a longer spindle bolt fitted with handwheels to increase the It will be seen that the combination of the rotating action of the Top Bracket Assembly 6 and the hinging of Pad Assembly 12 together will automatically position the contacting faces to fit any tapering section both spanwise, and chordwise-An elasticated Safety Strap 20 is fitted to the top edges of the Pad Assemblies 12 and is allowed to hang loosely in place to prevent accidental damage occurring to airfoil surfaces in the event of accidental slippage of a control surface. With reference to layout Drawing 4 \ 5, Arrows 'C' indicate the movement used to locate and hold any chordal taper through Pivot'A'whilst the Arrows Vindicate the movement to self adjust to suit all spanwise tapers by automatically moving Top Brackets 6 independently of each other through a spindle bolt shown on Drawing 4 \ 5 as Pivot'B'.
C.A.PUGH 189A TOPSHAM ROAD EXETER EX2 6AN.

Claims (6)

  1. I.An airfoil section holding device whereby any airfoil section or similar shaped item may be located and firmly held and where the contacting parts of the device adjust automatically to suit the tapered shape of the airfoil.
  2. 2. An airfoil holding device where according to claim I any aircraft control surface including those with outer skins constructed in the corrugated manner may be located and firmly held.
  3. 3. An airfoil holding device according to the preceding claims to self adjust to suit any chordwise taper on any airfoil section or aircraft control surface including those manufactured in the corrugated manner
  4. 4. An airfoil holding device according to the preceding claims to self adjust to suit any spanwise taper on any airfoil section or aircraft control surface including those manufactured in the corrugated manner.
  5. 5. An airfoil holding device according to the preceding claims in which an airfoil section or aircraft control surface including those manufactured in the corrugated manner may be rotated to a suitable angle for working by the provision of a self adjustment mechanism for the contacting parts.
  6. 6. An airfoil holding device according to all the preceding claims which will fold flat for storage when not in use.
    C.A.PUGH 189A TOPSHAM ROAD EXETER EX2 6AN.
GB9919114A 1999-08-14 1999-08-14 Airfoil holding device Withdrawn GB2354962A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9919114A GB2354962A (en) 1999-08-14 1999-08-14 Airfoil holding device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9919114A GB2354962A (en) 1999-08-14 1999-08-14 Airfoil holding device

Publications (2)

Publication Number Publication Date
GB9919114D0 GB9919114D0 (en) 1999-10-13
GB2354962A true GB2354962A (en) 2001-04-11

Family

ID=10859080

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9919114A Withdrawn GB2354962A (en) 1999-08-14 1999-08-14 Airfoil holding device

Country Status (1)

Country Link
GB (1) GB2354962A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1734226A1 (en) * 2005-06-17 2006-12-20 United Technologies Corporation Tool and method for filling voids in turbine vanes and other articles

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112276808A (en) * 2020-09-18 2021-01-29 余华云 Aircraft wing processing maintenance positioner

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB896385A (en) * 1960-08-24 1962-05-16 Braunschweigische Maschb Ansta Supporting jack or trestle
GB1311309A (en) * 1969-12-19 1973-03-28 Combustion Eng Hydraulic work positioning saddle
US4240621A (en) * 1978-05-15 1980-12-23 Dominic Daddato Multidirectional vise square device

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB896385A (en) * 1960-08-24 1962-05-16 Braunschweigische Maschb Ansta Supporting jack or trestle
GB1311309A (en) * 1969-12-19 1973-03-28 Combustion Eng Hydraulic work positioning saddle
US4240621A (en) * 1978-05-15 1980-12-23 Dominic Daddato Multidirectional vise square device

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1734226A1 (en) * 2005-06-17 2006-12-20 United Technologies Corporation Tool and method for filling voids in turbine vanes and other articles
JP2006348943A (en) * 2005-06-17 2006-12-28 United Technol Corp <Utc> Tool and method for filling voids in turbine vanes and other articles
US8844090B2 (en) 2005-06-17 2014-09-30 United Technologies Corporation Tool for filling voids in turbine vanes and other articles

Also Published As

Publication number Publication date
GB9919114D0 (en) 1999-10-13

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)