FLIGHT TEST HINGE ASSEMBLY

A system for calculating forces exerted into an aircraft component (12) may include a test hinge assembly (10) and a monitoring system (18). The test hinge assembly (10) may be a triangular shaped assembly, and may include at least one beam 22, 24, 28, at least one connecting joint 26, 34, 42 having...

Full description

Saved in:
Bibliographic Details
Main Authors WILLIAMS, JAMES A, OELKE, BRIAN S, DICKERSON, MATT R, JOHNSON, ROBERT, AMINZADEH, SHAHZAD
Format Patent
LanguageEnglish
French
German
Published 13.01.2016
Subjects
MEASURING
MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER,MECHANICAL EFFICIENCY, OR FLUID PRESSURE
PHYSICS
TESTING
Online AccessGet full text

Cover

Abstract A system for calculating forces exerted into an aircraft component (12) may include a test hinge assembly (10) and a monitoring system (18). The test hinge assembly (10) may be a triangular shaped assembly, and may include at least one beam 22, 24, 28, at least one connecting joint 26, 34, 42 having a channel (46, 48, 50) configured to receive and retain a fastening member, and at least one strain gage (60) secured to an outer surface of the beam(s) (22, 24, 28). The strain gage(s) (60) is configured to detect one or more strains exerted into the beam(s) (22, 24, 28). The monitoring system (18) is in communication with the strain gage(s) (60). The monitoring system (18) may be configured to calculate forces exerted into the fastening member(s) by analyzing the strain(s) (60) exerted into the beam(s) (22, 24, 28).
AbstractList A system for calculating forces exerted into an aircraft component (12) may include a test hinge assembly (10) and a monitoring system (18). The test hinge assembly (10) may be a triangular shaped assembly, and may include at least one beam 22, 24, 28, at least one connecting joint 26, 34, 42 having a channel (46, 48, 50) configured to receive and retain a fastening member, and at least one strain gage (60) secured to an outer surface of the beam(s) (22, 24, 28). The strain gage(s) (60) is configured to detect one or more strains exerted into the beam(s) (22, 24, 28). The monitoring system (18) is in communication with the strain gage(s) (60). The monitoring system (18) may be configured to calculate forces exerted into the fastening member(s) by analyzing the strain(s) (60) exerted into the beam(s) (22, 24, 28).
Author AMINZADEH, SHAHZAD
DICKERSON, MATT R
OELKE, BRIAN S
WILLIAMS, JAMES A
JOHNSON, ROBERT
Author_xml – fullname: WILLIAMS, JAMES A
– fullname: OELKE, BRIAN S
– fullname: DICKERSON, MATT R
– fullname: JOHNSON, ROBERT
– fullname: AMINZADEH, SHAHZAD
BookMark eNrjYmDJy89L5WSQcvPxdPcIUQhxDQ5R8PD0c3dVcAwOdvV18onkYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxrgFGlmZmJkYWjobGRCgBALwIIZo
ContentType Patent
DBID EVB
DatabaseName esp@cenet
DatabaseTitleList
Database_xml – sequence: 1
  dbid: EVB
  name: esp@cenet
  url: http://worldwide.espacenet.com/singleLineSearch?locale=en_EP
  sourceTypes: Open Access Repository
DeliveryMethod fulltext_linktorsrc
Discipline Medicine
Chemistry
Sciences
Physics
DocumentTitleAlternate ENSEMBLE DE CHARNIERE DE TEST DE VOL
FLUGPRUFSCHARNIERANORDNUNG
ExternalDocumentID EP2966428A1
GroupedDBID EVB
ID FETCH-epo_espacenet_EP2966428A13
IEDL.DBID EVB
IngestDate Fri Jul 19 15:44:24 EDT 2024
IsOpenAccess true
IsPeerReviewed false
IsScholarly false
Language English
French
German
LinkModel DirectLink
MergedId FETCHMERGED-epo_espacenet_EP2966428A13
Notes Application Number: EP20150174392
OpenAccessLink https://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20160113&DB=EPODOC&CC=EP&NR=2966428A1
ParticipantIDs epo_espacenet_EP2966428A1
PublicationCentury 2000
PublicationDate 20160113
PublicationDateYYYYMMDD 2016-01-13
PublicationDate_xml – month: 01
  year: 2016
  text: 20160113
  day: 13
PublicationDecade 2010
PublicationYear 2016
RelatedCompanies THE BOEING COMPANY
RelatedCompanies_xml – name: THE BOEING COMPANY
Score 3.0076845
Snippet A system for calculating forces exerted into an aircraft component (12) may include a test hinge assembly (10) and a monitoring system (18). The test hinge...
SourceID epo
SourceType Open Access Repository
SubjectTerms MEASURING
MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER,MECHANICAL EFFICIENCY, OR FLUID PRESSURE
PHYSICS
TESTING
Title FLIGHT TEST HINGE ASSEMBLY
URI https://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20160113&DB=EPODOC&locale=&CC=EP&NR=2966428A1
hasFullText 1
inHoldings 1
isFullTextHit
isPrint
link http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwfV1LT8MwDLam8bxBAbHxUA-otwrapFt7qKa1TSlo3Spa0DhNfUq7jIkW7e_jRN3gArcokZzEiuPPju0A3KESMx8qPLw6oalKq5yqJjELNaeaPsytCkE6z3cOp4PglT7PjXkHlttcGFEndCOKI6JE5Sjvjbiv1z9OLE_EVtb32RK7PkZ-YntKax1raF5oRPEcm0Uzb-YqrostZfpi6wjrEWmP0VDa4yial9lnbw5PSln_1ij-CexHSGzVnEKnXElw5G4_XpPgMGzfuyU4EAGaeY2drRDWZ9D3J0-PQSInLE5k7m1i8jiOWehM3s9B9lniBipOt9htbcGi3cLIBXTR4i8vQUbUkNIhIhcyINQorIwYqaWZVmkVyEIj60HvTzL9f8au4JjziHsQNHIN3ebzq7xBndpkt4Ib3ypJdec
link.rule.ids 230,309,786,891,25594,76906
linkProvider European Patent Office
linkToHtml http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwfV1LT8MwDLam8Rg3KCA2Xj2g3irokq7toULriw7arqIFjVPVp7TLmGgRfx-n6gYXuEWJ5CRWHH92bAfgBpWYelfh4R0Tmoq0yqmoErUQcyqNlVyrEKSzfGc_mLgv9HEhL3qw3OTCtHVCv9riiChROcp7097X6x8nltXGVta32RK73u-dWLeEzjqW0LyQiGAZuh3OrbkpmCa2hOBZHyOsR6Q9RUNpR2HFeRlyejVYUsr6t0ZxDmE3RGKr5gh65YqDgbn5eI2Dfb977-Zgrw3QzGvs7ISwPoaR480e3JiP7SjmmbfJ5qdRZPuG93YCvGPHpividMl2a4kdbhdGTqGPFn95BjyihpQqiFzIhFC50DIip5qkaqVWIAvlbAjDP8mM_hm7hoEb-17izYKnczhg_GLeBIlcQL_5-CwvUb822VXLmW_Vv3jU
openUrl ctx_ver=Z39.88-2004&ctx_enc=info%3Aofi%2Fenc%3AUTF-8&rfr_id=info%3Asid%2Fsummon.serialssolutions.com&rft_val_fmt=info%3Aofi%2Ffmt%3Akev%3Amtx%3Apatent&rft.title=FLIGHT+TEST+HINGE+ASSEMBLY&rft.inventor=WILLIAMS%2C+JAMES+A&rft.inventor=OELKE%2C+BRIAN+S&rft.inventor=DICKERSON%2C+MATT+R&rft.inventor=JOHNSON%2C+ROBERT&rft.inventor=AMINZADEH%2C+SHAHZAD&rft.date=2016-01-13&rft.externalDBID=A1&rft.externalDocID=EP2966428A1