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특허 상세정보

Method of making rocket engine combustion chamber utilizing “slide in”port liner

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B23P-015/00   
미국특허분류(USC) 29/89001 ; ; 29/428
출원번호 US-0264263 (1994-06-23)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 13  인용 특허 : 3
초록

A method of fabricating a rocket engine combustion chamber comprising assembling a liner having cooling channels, a plurality of throat support sections, and a structural jacket having inlet and outlet manifolds. Then heating the assembly in a pressurized furnace to bond the assembled parts to each other.

대표
청구항

A method of making a rocket engine combustion chamber comprising: forming a coolant liner having an outside surface; forming a plurality of coolant channels on the outside surface of the coolant liner so that the surface has a plurality of lands; forming at least two throat support sections; assembling the throat support sections together around the outside surface of the coolant liner; forming a structural jacket having an inside cavity, an inlet manifold, inlet feed passages, an outlet manifold, and outlet feed passages; inserting the coolant liner wit...

이 특허를 인용한 특허 피인용횟수: 13

  1. Polt, Anton. Barrel engine block assembly. USP2010027654234.
  2. Nishikawa, Kosuke; Morifuji, Tetsuya; Mizuno, Kyozo; Negoro, Nobuki. Brazing method. USP2016089427817.
  3. Wherley, Brian Leigh; Fisher, Steven C.; Litt, Amardeep. Combustion chamber having a multiple-piece liner and associated assembly method. USP2004026688100.
  4. Indersie, Dominique; Guichard, Didier. Combustion chamber provided with a tubular element. USP2017099759163.
  5. Beyer, Steffen; Bichler, Peter; Keinath, Wolfgang; Kindermann, Roland; Kunzmann, Dieter. Combustion chamber structure and its manufacturing process. USP2005056889496.
  6. Kayser, Gregory F.; Wisner, Daniel L.; Somerville, John G.. Diffusion bonded composite material and method therefor. USP2012078225481.
  7. Nguyen, Ly D.; Woodcock, Gregory O.; Kujala, Stony. Forming and assembly method for multi-axial pivoting combustor liner in gas turbine engine. USP2005076912782.
  8. Nishikawa, Kosuke; Kobayashi, Hiroyuki; Manako, Hiroyasu. Joining method and joining system. USP20181010105777.
  9. Fint, Jeffry A.; Hankins, Michael B.; Jew, Myron L.; Ulmer, Donald G.; Wherley, Brian L.; Romine, William D.; Kuck, Frederick M.; Ades, Douglas S.. Method of fabricating a rocket engine nozzle using pressure brazing. USP2012038127443.
  10. Ring Peter John. Method of making a rocket thrust chamber. USP2001036205661.
  11. Jones, Douglas B.; Greason, Jeffrey K.; DeLong, Daniel L.. Rocket combustion chamber with jacket. USP2010127854395.
  12. Fint, Jeffry A.; Ades, Douglas S.; Hankins, Michael B.; Stangeland, Maynard L.. Rocket engine combustion chamber having multiple conformal throat supports. USP2004126829884.
  13. Fint, Jeffry A.; Hankins, Michael B.; Jew, Myron L.; Ulmer, Donald G.; Wherley, Brian L.; Romine, William D.; Kuck, Frederick M.; Ades, Douglas S.. Rocket engine nozzle and method of fabricating a rocket engine nozzle using pressure brazing. USP2009107596940.