Hypersonic aircraft window system

A system and method for sending signals at temperatures associated with hypersonic speeds. A window system in a hypersonic aircraft is provided. The window system comprises a transmissive window in an aeroshell of the hypersonic aircraft, a thermal seal, a sensor, and a sensor housing assembly enclo...

Full description

Saved in:
Bibliographic Details
Main Authors Lam, Tai Anh, Best, Michael John, Shaw, Peter, Embler, Jonathan David, Heng, Sangvavann
Format Patent
LanguageEnglish
Published 07.11.2023
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
Online AccessGet full text

Cover

Abstract A system and method for sending signals at temperatures associated with hypersonic speeds. A window system in a hypersonic aircraft is provided. The window system comprises a transmissive window in an aeroshell of the hypersonic aircraft, a thermal seal, a sensor, and a sensor housing assembly enclosing the sensor. The transmissive window comprises a facesheet and insulating material adjacent to the facesheet. The thermal seal surrounds a perimeter of the facesheet and seals the facesheet to the aeroshell. The window system is radio-frequency transparent at temperatures associated with hypersonic speeds. The window system is configured to operate at an insertion loss of less than one decibel at the hypersonic speeds.
AbstractList A system and method for sending signals at temperatures associated with hypersonic speeds. A window system in a hypersonic aircraft is provided. The window system comprises a transmissive window in an aeroshell of the hypersonic aircraft, a thermal seal, a sensor, and a sensor housing assembly enclosing the sensor. The transmissive window comprises a facesheet and insulating material adjacent to the facesheet. The thermal seal surrounds a perimeter of the facesheet and seals the facesheet to the aeroshell. The window system is radio-frequency transparent at temperatures associated with hypersonic speeds. The window system is configured to operate at an insertion loss of less than one decibel at the hypersonic speeds.
Author Best, Michael John
Lam, Tai Anh
Heng, Sangvavann
Shaw, Peter
Embler, Jonathan David
Author_xml – fullname: Lam, Tai Anh
– fullname: Best, Michael John
– fullname: Shaw, Peter
– fullname: Embler, Jonathan David
– fullname: Heng, Sangvavann
BookMark eNrjYmDJy89L5WRQ9KgsSC0qzs_LTFZIzCxKLkpMK1Eoz8xLyS9XKK4sLknN5WFgTUvMKU7lhdLcDIpuriHOHrqpBfnxqcUFicmpeakl8aHBhoYWBubGpsZORsbEqAEAk1Qn_w
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
ExternalDocumentID US11807353B2
GroupedDBID EVB
ID FETCH-epo_espacenet_US11807353B23
IEDL.DBID EVB
IngestDate Fri Jul 19 13:58:02 EDT 2024
IsOpenAccess true
IsPeerReviewed false
IsScholarly false
Language English
LinkModel DirectLink
MergedId FETCHMERGED-epo_espacenet_US11807353B23
Notes Application Number: US202217649563
OpenAccessLink https://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20231107&DB=EPODOC&CC=US&NR=11807353B2
ParticipantIDs epo_espacenet_US11807353B2
PublicationCentury 2000
PublicationDate 20231107
PublicationDateYYYYMMDD 2023-11-07
PublicationDate_xml – month: 11
  year: 2023
  text: 20231107
  day: 07
PublicationDecade 2020
PublicationYear 2023
RelatedCompanies The Boeing Company
RelatedCompanies_xml – name: The Boeing Company
Score 3.4973512
Snippet A system and method for sending signals at temperatures associated with hypersonic speeds. A window system in a hypersonic aircraft is provided. The window...
SourceID epo
SourceType Open Access Repository
SubjectTerms AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
Title Hypersonic aircraft window system
URI https://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20231107&DB=EPODOC&locale=&CC=US&NR=11807353B2
hasFullText 1
inHoldings 1
isFullTextHit
isPrint
link http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwfV1JS8NAFH6UKupNq6J1IQXJLdiayXYIQjaC0AXbSG-lswTSQ1vSSP6-b8bUetHbMAOzMW_5Zt77BuCJu8zzGIIct09zg-ARNjyPc0NYA9anrs2JyuIfjuw0I29za96C1T4XRvGE1oocESWKobxXSl9vD5dYkYqt3D3TAqs2r8nMj_QGHaOzIj9RjQI_noyjcaiHoZ9N9dG7L5nOHNMyA1TXR-hGOzL8K_4IZFbK9rdJSc7heIK9rasLaIl1B07D_c9rHTgZNg_eWGxkb3cJvRQho3SPC6Yti5KVy7zSaoTUm1r75mO-gl4Sz8LUwLEWPwtbZNPDtMxraCPgFzeg2dyxuOQly22b5Fx4jBBqvlDb4gPK--IWun_30_2v8Q7O5CapXDrnHtpV-Ske0KhW9FHtxhdpL3tE
link.rule.ids 230,309,783,888,25578,76884
linkProvider European Patent Office
linkToHtml http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwfV1bT8IwFD4haMQ3RY3gbSRmb4vD3R8Wk13IVAZENsPbQtstwQcgY2Z_39MK4ou-NW3Sy0nP5Wt7vgLcM5s6DkWQY6ukUHTcworjMKbkRp-qxDaZLrL445EZpfrLzJg14GOXCyN4QmtBjogaRVHfK2Gv1_tDrEC8rdw8kAVWrZ4GiRvIW3SMwQr_RDXw3HAyDsa-7PtuOpVHby5nOrM0Q_PQXB9giG1znv3w3eNZKevfLmVwAocT7G1ZnUIjX7ah5e9-XmvDUby98MbiVvc2Z9CLEDLy8HhBpfmipOW8qKQaIfWqlr75mM-hNwgTP1JwrOxnYVk63U9Lu4AmAv78EiSTWQbjvGSFaeoFyx2q60R7JKbB-oSpeQe6f_fT_a_xDlpREg-z4fPo9QqOucBEXp11Dc2q_Mxv0MFW5FZI5gtYY340
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=Hypersonic+aircraft+window+system&rft.inventor=Lam%2C+Tai+Anh&rft.inventor=Best%2C+Michael+John&rft.inventor=Shaw%2C+Peter&rft.inventor=Embler%2C+Jonathan+David&rft.inventor=Heng%2C+Sangvavann&rft.date=2023-11-07&rft.externalDBID=B2&rft.externalDocID=US11807353B2