GB724758A - Improvements in or relating to composite metal-fibrous structures - Google Patents

Improvements in or relating to composite metal-fibrous structures

Info

Publication number
GB724758A
GB724758A GB11388/52A GB1138852A GB724758A GB 724758 A GB724758 A GB 724758A GB 11388/52 A GB11388/52 A GB 11388/52A GB 1138852 A GB1138852 A GB 1138852A GB 724758 A GB724758 A GB 724758A
Authority
GB
United Kingdom
Prior art keywords
layers
relating
composite metal
fibrous structures
metal
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
GB11388/52A
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.)
ERNEST PLATTON KING
Original Assignee
ERNEST PLATTON KING
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 ERNEST PLATTON KING filed Critical ERNEST PLATTON KING
Priority to GB11388/52A priority Critical patent/GB724758A/en
Publication of GB724758A publication Critical patent/GB724758A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
    • B29C65/50—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like
    • B29C65/5057—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding using adhesive tape, e.g. thermoplastic tape; using threads or the like positioned between the surfaces to be joined
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/05—Particular design of joint configurations
    • B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
    • B29C66/112—Single lapped joints
    • B29C66/1122—Single lap to lap joints, i.e. overlap joints
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/56—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
    • B29C65/562—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits using extra joining elements, i.e. which are not integral with the parts to be joined

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)

Abstract

724,758. Compound sheet materials. KING E. P. May 6, 1952 [Feb. 7, 1951], No. 11388/52. Divided out of 724,753 and addition to 635,823. Drawings to Specification. Class 140. [Also in Groups X, XXI, XXII, XXVIII and XXXIII. In a laminated structure made by the method described in the parent Specification, one or more of the metal layers extend beyond the other metal layer or layers so as to provide one or more steps in the thickness of the structure. One or more of the layers, which may be of different metals, may be perforated. The cold-setting adhesive and fibrous layers may be as described in Specification 724,753. The invention may be applied to girders, the leading edge or the whole skin of an aircraft wing, or helicopter rotor blade, or a tube.
GB11388/52A 1951-02-07 1951-02-07 Improvements in or relating to composite metal-fibrous structures Expired GB724758A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB11388/52A GB724758A (en) 1951-02-07 1951-02-07 Improvements in or relating to composite metal-fibrous structures

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB11388/52A GB724758A (en) 1951-02-07 1951-02-07 Improvements in or relating to composite metal-fibrous structures

Publications (1)

Publication Number Publication Date
GB724758A true GB724758A (en) 1955-02-23

Family

ID=9985305

Family Applications (1)

Application Number Title Priority Date Filing Date
GB11388/52A Expired GB724758A (en) 1951-02-07 1951-02-07 Improvements in or relating to composite metal-fibrous structures

Country Status (1)

Country Link
GB (1) GB724758A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2941603A (en) * 1956-05-01 1960-06-21 Drago K Jovanovich Helicopter rotor blade
US3161238A (en) * 1962-07-05 1964-12-15 Howard P Key Helicopter rotor blade
JP2010274910A (en) * 2009-05-28 2010-12-09 Boeing Co:The Transition of stringer, and manufacturing method for composite component using transition of stringer
EP2886449A1 (en) * 2013-12-23 2015-06-24 Airbus Operations S.L. Leading edge for an aircraft lifting surface
EP3006189A1 (en) * 2014-10-09 2016-04-13 The Boeing Company Composite structures having composite-to-metal joints and methods for making the same
US9522512B2 (en) 2010-08-17 2016-12-20 The Boeing Company Methods for making composite structures having composite-to-metal joints
US10112373B2 (en) 2010-08-17 2018-10-30 The Boeing Company Multi-layer metallic structure and composite-to-metal joint methods

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2941603A (en) * 1956-05-01 1960-06-21 Drago K Jovanovich Helicopter rotor blade
US3161238A (en) * 1962-07-05 1964-12-15 Howard P Key Helicopter rotor blade
JP2010274910A (en) * 2009-05-28 2010-12-09 Boeing Co:The Transition of stringer, and manufacturing method for composite component using transition of stringer
US9522512B2 (en) 2010-08-17 2016-12-20 The Boeing Company Methods for making composite structures having composite-to-metal joints
US11084269B2 (en) 2010-08-17 2021-08-10 The Boeing Company Multi-layer metallic structure and composite-to-metal joint methods
US10112373B2 (en) 2010-08-17 2018-10-30 The Boeing Company Multi-layer metallic structure and composite-to-metal joint methods
US9919507B2 (en) 2010-08-17 2018-03-20 The Boeing Company Process for inhibiting galvanic corrosion of an aluminum structure connected, without using a splice plate, to a composite structure having a fiber including graphite
EP2886449A1 (en) * 2013-12-23 2015-06-24 Airbus Operations S.L. Leading edge for an aircraft lifting surface
US9381992B2 (en) 2013-12-23 2016-07-05 Airbus Operations S.L. Leading edge for an aircraft lifting surface
CN104724279A (en) * 2013-12-23 2015-06-24 空中客车营运有限公司 Leading Edge For An Aircraft Lifting Surface
CN105501428A (en) * 2014-10-09 2016-04-20 波音公司 Composite structure having composite-to-metal joints and method for making same
EP3006189A1 (en) * 2014-10-09 2016-04-13 The Boeing Company Composite structures having composite-to-metal joints and methods for making the same
CN105501428B (en) * 2014-10-09 2020-06-30 波音公司 Composite structure with composite-to-metal joint and method of making the same

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