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US4068238A Expired / Lapsed US ⏱️ 0.0 years remaining

Elastic strain energy deployable helical antenna

Assignee: Northrop Grumman Space and Mission Systems Corp
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Filing: 1976-05-13
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Granted: 1978-01-10
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Expires: 1996-05-13
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Abstract

Abstract An elastic strain energy deployable helical antenna having a tubular resiliently flexible antenna element of relatively flat oval cross-section fixed at one end to a support and formed into a normally extended, resiliently compressible helix with the major axis of the oval cross-section of the element substantially normal to the longitudinal axis of the helix, and flexible tension members of shorter overall length than the fully extended length of the helix fixed at one end to the support and extending axially of the helix across and secured to its helical turns. The antenna helix is compressible axially to a contracted length for storage and is deployable axially by stored elastic strain energy to an extended operating length at which the tension members are stressed in tension by the helix to reinforce the latter against deflection laterally of its longitudinal axis. The tension members may have rigid portions between the helix turns for increasing the natural frequency of vibration of the antenna.

Inventors

  • 👤 Roy M. Acker

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-01 08:00
CPC Classifications
H; H01; H01Q; H01Q1/00; H01Q1/08; H01Q1/084; H01Q1/12; H01Q1/20; H01Q11/00; H01Q11/02; H01Q11/08; H01Q11/086

Claims Analysis

Total Claims: 10
Claim 1
Independent Claim 177 words
An elastic strain energy deployable helical antenna comprising: a resiliently flexible antenna element in the form of a helix which is yieldably biassed to extend axially by elastic strain energy to a given fully extended length and is compressible axially to a contracted length; said antenna element comprising an electrically conductive tube of relatively flat oval cross-section in transverse planes containing the longitudinal axis of said helix; the major axis of said oval cross-section in any transverse plane being substantially normal to said longitudinal axis; a plurality of flexible tension members extending axially of and spaced circumferentially about said helix and secured to helical turns of said antenna element; and said tension members having relatively rigid portions between said turns and an overall length less than said fully extended length, whereby said members limit elastic strain energy extension of said antenna element to an operating length less than said fully extended length and said members are stressed in tension by said element at said operating length to reinforce said element against deflection laterally of said longitudinal axis.
Claim 2
Dependent Claim 177 words
An elastic strain energy deployable helical antenna comprising: a resiliently flexible antenna element in the form of a helix which is yieldably biassed to extend axially by elastic strain energy to a given fully extended length and is compressible axially to a contracted length; said antenna element comprising an electrically conductive tube of relatively flat oval cross-section in transverse planes containing the longitudinal axis of said helix; the major axis of said oval cross-section in any transverse plane being substantially normal to said longitudinal axis; a plurality of flexible tension members extending axially of and spaced circumferentially about said helix and secured to helical turns of said antenna element; and said tension members having relatively rigid portions between said turns and an overall length less than said fully extended length, whereby said members limit elastic strain energy extension of said antenna element to an operating length less than said fully extended length and said members are stressed in tension by said element at said operating length to reinforce said element against deflection laterally of said longitudinal axis.
Claim 3
Dependent Claim 42 words
A deployable helical antenna according to claim 1 wherein: each tension member has flexible portions secured to the helical turns of said antenna element and a pair of said rigid portions and an intervening flexible portion between each pair of adjacent turns.
Claim 4
Dependent Claim 14 words
A deployable helical antenna according to claim 2 wherein: said tension members comprise cords.
Claim 5
Dependent Claim 28 words
A deployable helical antenna according to claim 3 wherein: each tension member has relatively rigid sleeves surrounding the respective cord and forming said rigid portions of the member.
Claim 6
Dependent Claim 31 words
A deployable helical antenna according to claim 4 including: an antenna support at one end of said helix secured to the adjacent ends of said antenna element and said tension members.
Claim 7
Dependent Claim 31 words
A deployable helical antenna according to claim 1 including: an antenna support at one end of said helix secured to the adjacent ends of said antenna element and said tension members.
Claim 8
Dependent Claim 108 words
An elastic strain energy deployable helical antenna comprising: a normally extended, axially compressible helix comprising a tubular, resiliently flexible, helically coiled antenna element which is stressed to extend axially by elastic strain energy to a given fully extended length and is yieldably compressible axially to a contracted length; said antenna element comprising an electrically conductive tube of relatively flat oval cross-section in transverse planes containing the longitudinal axis to said helix; and the major axis of said cross-section in any transverse plane being substantially normal to said longitudinal axis of the helix, whereby said helix is axially compressible to said contracted length without permanent deformation of the helix.
Claim 9
Dependent Claim 108 words
An elastic strain energy deployable helical antenna comprising: a normally extended, axially compressible helix comprising a tubular, resiliently flexible, helically coiled antenna element which is stressed to extend axially by elastic strain energy to a given fully extended length and is yieldably compressible axially to a contracted length; said antenna element comprising an electrically conductive tube of relatively flat oval cross-section in transverse planes containing the longitudinal axis to said helix; and the major axis of said cross-section in any transverse plane being substantially normal to said longitudinal axis of the helix, whereby said helix is axially compressible to said contracted length without permanent deformation of the helix.
Claim 10
Dependent Claim 109 words
A deployable helical antenna according to claim 7 including: a plurality of flexible tension members circumferentially spaced about said helix and extending axially of said helix directly from one helical turn of the helix to the next and secured to each said helical turn; and said tension members having an overall length less than said fully extended length of said helix, whereby said tension members limit extension of said antenna element to an operating length less than said fully extended length, and said tension members are stressed in tension between the adjacent helical turns at said operating length to reinforce said helix against deflection laterally of its longitudinal axis.

References Cited (Backward Citations)

FR810325A Cited
US3524190A Cited
US3699585A Cited
US3858220A Cited
US3913109A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1981-01-09 1981-07-11 1982-01-10 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1985-01-09 1985-07-11 1986-01-10 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1989-01-09 1989-07-11 1990-01-10 $7700.00 Window Closed / Lapsed

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