CA2543769A1 - Wing panel assembly - Google Patents

Wing panel assembly Download PDF

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Publication number
CA2543769A1
CA2543769A1 CA002543769A CA2543769A CA2543769A1 CA 2543769 A1 CA2543769 A1 CA 2543769A1 CA 002543769 A CA002543769 A CA 002543769A CA 2543769 A CA2543769 A CA 2543769A CA 2543769 A1 CA2543769 A1 CA 2543769A1
Authority
CA
Canada
Prior art keywords
yoke
support structure
wing panel
pit
panel assembly
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
CA002543769A
Other languages
French (fr)
Other versions
CA2543769C (en
Inventor
Paul E. Nelson
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.)
Boeing Co
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
Priority claimed from US08/937,486 external-priority patent/US6029352A/en
Application filed by Individual filed Critical Individual
Priority claimed from CA002217892A external-priority patent/CA2217892C/en
Publication of CA2543769A1 publication Critical patent/CA2543769A1/en
Application granted granted Critical
Publication of CA2543769C publication Critical patent/CA2543769C/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Landscapes

  • Lift-Guide Devices, And Elevator Ropes And Cables (AREA)
  • Cage And Drive Apparatuses For Elevators (AREA)

Abstract

An apparatus for fabricating stiffened wing panel components for a large commercial jet transport airplanes with planks, stringers and yoke assembly including a first support structure mounted on a saddle supported on a track extending along an elongated pit, a downwardly opening U-shaped yoke on a support structure, an actuator for pivoting the yoke, a second pivotal mount for the yoke on the support structure, a rotational actuator for rotating the yoke and a fixture supported on a vertically adjustable elevator mounted in the pit.
CA002543769A 1996-10-17 1997-10-08 Wing panel assembly Expired - Lifetime CA2543769C (en)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US2852396P 1996-10-17 1996-10-17
US60/028,523 1996-10-17
US08/937,486 US6029352A (en) 1997-09-25 1997-09-25 Wing panel assembly
US08/937,486 1997-09-25
CA002217892A CA2217892C (en) 1996-10-17 1997-10-08 Wing panel assembly

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
CA002217892A Division CA2217892C (en) 1996-10-17 1997-10-08 Wing panel assembly

Publications (2)

Publication Number Publication Date
CA2543769A1 true CA2543769A1 (en) 1998-04-17
CA2543769C CA2543769C (en) 2009-03-17

Family

ID=36637833

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002543769A Expired - Lifetime CA2543769C (en) 1996-10-17 1997-10-08 Wing panel assembly

Country Status (1)

Country Link
CA (1) CA2543769C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113385913A (en) * 2021-06-25 2021-09-14 成都飞机工业（集团）有限责任公司 Lug joint locking mechanism with multi-degree-of-freedom adjustment

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113385913A (en) * 2021-06-25 2021-09-14 成都飞机工业（集团）有限责任公司 Lug joint locking mechanism with multi-degree-of-freedom adjustment

Also Published As

Publication number Publication date
CA2543769C (en) 2009-03-17

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Legal Events

Date Code Title Description
EEER Examination request
MKEX Expiry

Effective date: 20171010