$\require{mediawiki-texvc}$
  • 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Precursor formulations for a liner, a rocket motor including the liner, and related methods

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) C08G-065/32    C08G-018/79    F02K-009/34    C08G-018/48    C08G-018/69    C08G-018/72    C08G-018/75    C08G-018/76    C08K-005/103    C08K-007/20    C06B-045/12    C08G-071/02    C08K-003/22    C08K-003/38   
출원번호 US-0796685 (2013-03-12)
등록번호 US-9416217 (2016-08-16)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    TraskBritt
인용정보 피인용 횟수 : 0  인용 특허 : 10
초록

A precursor formulation of a liner comprising a polymer and at least two curatives. One of the at least two curatives comprises a more reactive curative and the other of the at least two curatives comprises a less reactive curative. The more reactive curative is formulated to crosslink the polymer. A method of lining a rocket motor is also disclosed, as is a rocket motor including the liner.

대표
청구항

1. A precursor formulation of a liner, comprising: a polymer; andat least two curatives, one of the at least two curatives comprising a more reactive curative formulated to polymerize the polymer and the other of the at least two curatives comprising a less reactive curative formulated to be unreactive with the polymer. 2. A method of lining a rocket motor, comprising: applying a precursor formulation of a liner to a rocket motor, the precursor formulation of the liner comprising: a liner polymer and at least two curatives, one of the at least two curati...

이 특허에 인용된 특허 (10)

  1. Sayles David C. (Huntsville AL). Cloth-lined interceptor motor insulation for strong insulation-to-propellant interlock. USP1993055209876.
  2. Nelson Ronald W. ; Lovett Merylin B. ; Poulter Larry W. ; Bonderson Elizabeth K.. Erosion resistant-low signature liner for solid propellant rocket motors. USP2000046054521.
  3. Boothe Richard E. (Madison AL) Hutchens Dale E. (Huntsville AL). Interpenetrating network combination of ultraviolet and thermally cured rocket motor liner composition and method. USP1995015377593.
  4. Brown Robert James,GBX ; Cooke Ernest Melville Guthrie,GBX ; Spickernell Graham James,GBX ; Treadgold Arthur Ronald,GBX ; Tucker Bernard George,GBX. Manufacture of propellant compositions and propellant charges. USP2000036036894.
  5. Sinclair James W. (Logan UT) Lefgren David (Garland UT) Min Kyung J. (Daejun KRX). Methods and compositions for bonding propellants within rocket motors. USP1993125273785.
  6. Wallace, II, Ingvar A.; Oyler, Jeffery. Nitrate ester plasticized energetic compositions, method of making and rocket motor assemblies containing the same. USP2003106632378.
  7. Poulter Larry W. ; Nelson Ronald W. ; Smalley ; Jr. Robert B. ; Hawkins Marvin C.. Robust propellant liner and interfacial propellant burn rate control. USP1999115985361.
  8. Poulter Larry W. ; Nelson Ronald W. ; Smalley ; Jr. Robert B. ; Hawkins Marvin C.. Robust propellant liner and interfacial propellant burn rate control. USP1998065767221.
  9. Harvey, Albert R.; Ellertson, John W.. Rocket motor insulation containing hydrophobic particles. USP2003086606852.
  10. Jones Marvin Luther ; Tzeng Donald Dongjaw. Solid rocket propellant. USP2001056238499.