WO2015156368A1 - アブレータ及び再突入機並びにそれらの製造方法 - Google Patents

アブレータ及び再突入機並びにそれらの製造方法 Download PDF

Info

Publication number
WO2015156368A1
WO2015156368A1 PCT/JP2015/061153 JP2015061153W WO2015156368A1 WO 2015156368 A1 WO2015156368 A1 WO 2015156368A1 JP 2015061153 W JP2015061153 W JP 2015061153W WO 2015156368 A1 WO2015156368 A1 WO 2015156368A1
Authority
WO
WIPO (PCT)
Prior art keywords
resin
ablator
granular
fiber
base material
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/JP2015/061153
Other languages
English (en)
French (fr)
Japanese (ja)
Inventor
愛一郎 塚原
文人 武田
惇子 渡邉
井出　勇
信輔 武田
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Lignyte Co Ltd
Mitsubishi Heavy Industries Ltd
Original Assignee
Lignyte Co Ltd
Mitsubishi Heavy Industries Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Lignyte Co Ltd, Mitsubishi Heavy Industries Ltd filed Critical Lignyte Co Ltd
Priority to EP15776733.6A priority Critical patent/EP3130544B1/en
Priority to US15/302,292 priority patent/US10647452B2/en
Publication of WO2015156368A1 publication Critical patent/WO2015156368A1/ja
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Images

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/52—Protection, safety or emergency devices; Survival aids
    • B64G1/58—Thermal protection, e.g. heat shields
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
    • B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C69/00—Combinations of shaping techniques not provided for in a single one of main groups B29C39/00 - B29C67/00, e.g. associations of moulding and joining techniques; Apparatus therefore
    • B29C69/001—Combinations of shaping techniques not provided for in a single one of main groups B29C39/00 - B29C67/00, e.g. associations of moulding and joining techniques; Apparatus therefore a shaping technique combined with cutting, e.g. in parts or slices combined with rearranging and joining the cut parts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/02—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising combinations of reinforcements, e.g. non-specified reinforcements, fibrous reinforcing inserts and fillers, e.g. particulate fillers, incorporated in matrix material, forming one or more layers and with or without non-reinforced or non-filled layers
    • B29C70/021—Combinations of fibrous reinforcement and non-fibrous material
    • B29C70/025—Combinations of fibrous reinforcement and non-fibrous material with particular filler
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06—Fibrous reinforcements only
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/62—Systems for re-entry into the earth's atmosphere; Retarding or landing devices
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3097—Cosmonautical vehicles; Rockets

Definitions

  • an ablator in one aspect of the present invention, includes a base material formed of fibers, a granular resin, and a binder resin impregnated in the base material to bond the granular resin and the base material.
  • the material for the granular resin and the binder resin for example, phenol resin, furan resin, mixed resin obtained by mixing phenol resin and furan resin, and epoxy resin can be used.
  • the granular resin and the binder resin are preferably a phenol resin, a furan resin, or a mixed resin in which a phenol resin and a furan resin are mixed.
  • the phenolic resin and furan resin are generally excellent in heat resistance, and the body protection performance of the ablator can be improved by using phenolic resin, furan resin or a mixed resin thereof as the granular resin and binder resin.
  • the heat resistance of the ablator that is, the airframe protection performance depends not only on the content of the binder resin but also on the content of the granular resin. It should be noted here that the granular resin does not contribute much to the bonding between the fibers. Even if the ablator contains granular resin, the ablator does not lose its flexibility. In other words, even if the content of the binder resin is small, the heat resistance of the ablator, that is, the airframe protection performance can be improved by including the granular resin.
  • Example 2 and 3 the ratio of the mass of the resin to the mass of the substrate was 53% and 56%, respectively, and the total content of the resin contained in the sample was larger than that of Comparative Example 1,
  • the samples of Examples 2 and 3 showed flexibility. This means that the ablator of this embodiment containing granular resin (spherical resin) can improve the airframe protection performance while having flexibility.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Health & Medical Sciences (AREA)
  • Thermal Sciences (AREA)
  • Emergency Medicine (AREA)
  • General Health & Medical Sciences (AREA)
  • Critical Care (AREA)
  • Oral & Maxillofacial Surgery (AREA)
  • Reinforced Plastic Materials (AREA)
  • Moulding By Coating Moulds (AREA)
PCT/JP2015/061153 2014-04-10 2015-04-09 アブレータ及び再突入機並びにそれらの製造方法 Ceased WO2015156368A1 (ja)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP15776733.6A EP3130544B1 (en) 2014-04-10 2015-04-09 Ablator, reentry vehicle, and methods respectively for manufacturing said ablator and said reentry vehicle
US15/302,292 US10647452B2 (en) 2014-04-10 2015-04-09 Ablator, re-entry vehicle and method of manufacturing them

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2014-081352 2014-04-10
JP2014081352A JP6353686B2 (ja) 2014-04-10 2014-04-10 再突入機の製造方法

Publications (1)

Publication Number Publication Date
WO2015156368A1 true WO2015156368A1 (ja) 2015-10-15

Family

ID=54287940

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/JP2015/061153 Ceased WO2015156368A1 (ja) 2014-04-10 2015-04-09 アブレータ及び再突入機並びにそれらの製造方法

Country Status (4)

Country Link
US (1) US10647452B2 (OSRAM)
EP (1) EP3130544B1 (OSRAM)
JP (1) JP6353686B2 (OSRAM)
WO (1) WO2015156368A1 (OSRAM)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6353686B2 (ja) * 2014-04-10 2018-07-04 三菱重工業株式会社 再突入機の製造方法
CN109955501B (zh) * 2019-04-04 2021-06-11 北京卫星制造厂有限公司 返回式飞船大尺寸扇弧面防热结构成型工艺方法

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH09239847A (ja) * 1996-03-14 1997-09-16 Nissan Motor Co Ltd 低密度ｆｒｐアブレータ
JP2001247100A (ja) * 2000-03-07 2001-09-11 Natl Space Development Agency Of Japan アブレータ
JP2013028166A (ja) * 2012-07-25 2013-02-07 Institute Of National Colleges Of Technology Japan 熱防御複合材の製造方法

Family Cites Families (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3520027A (en) * 1968-07-11 1970-07-14 Dow Chemical Co Apparatus for the incorporation of filamentary material in resinous matrix
US3962491A (en) * 1972-10-11 1976-06-08 Aisin Chemical Company, Limited Process for producing resin-coated sand particles for use in shell moles
US4151800A (en) * 1977-04-15 1979-05-01 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Thermal insulation protection means
US4255483A (en) * 1977-06-14 1981-03-10 Mcdonnell Douglas Corporation Fire barrier compositions and composites
US4364991A (en) * 1980-09-25 1982-12-21 Mcdonnell Douglas Corporation Fire resistant compositions and composites
FR2586080B1 (fr) * 1985-08-12 1987-11-27 Centre Nat Etd Spatiales Element de protection thermique pour un engin soumis a des echauffements importants
JP3565370B2 (ja) * 1995-03-31 2004-09-15 株式会社アイ・エイチ・アイ・エアロスペース アブレーション方法およびアブレータ構造
JP3644612B2 (ja) * 1996-05-28 2005-05-11 株式会社アイ・エイチ・アイ・エアロスペース アブレータ材料およびその製造方法
US6136418A (en) * 1999-03-01 2000-10-24 Rotary Rocket Company Rapidly removable thermal protection system for reusable launch vehicle
US6280667B1 (en) * 1999-04-19 2001-08-28 Andersen Corporation Process for making thermoplastic-biofiber composite materials and articles including a poly(vinylchloride) component
US6264144B1 (en) * 1999-08-03 2001-07-24 Lockheed Martin Corporation Material assembly for an inflatable aerodynamic braking device for spacecraft deceleration and the like
WO2003045460A1 (en) * 2001-11-27 2003-06-05 Takiron Co., Ltd. Implant material and process for producing the same
US20040096619A1 (en) * 2002-11-11 2004-05-20 The Boeing Company Flexible insulation blanket having a ceramic matrix composite outer layer
CN100584882C (zh) * 2003-02-13 2010-01-27 东方化学工业株式会社 透射激光的着色聚烯烃树脂组合物以及激光焊接的方法
US7219859B2 (en) * 2005-04-01 2007-05-22 Spacehab, Incorporated Multipurpose modular spacecraft
US9040646B2 (en) * 2007-10-04 2015-05-26 W. L. Gore & Associates, Inc. Expandable TFE copolymers, methods of making, and porous, expanded articles thereof
JP5263737B2 (ja) * 2008-07-15 2013-08-14 独立行政法人国立高等専門学校機構 熱防御複合材の製造方法
US7931962B1 (en) * 2009-05-14 2011-04-26 Lockheed Martin Corporation Pyrolizing flexible ablator material
JP5878298B2 (ja) * 2011-03-02 2016-03-08 リグナイト株式会社 断熱材用組成物及び断熱材
US9592923B1 (en) * 2011-10-24 2017-03-14 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Flexible ablators
JP5727923B2 (ja) 2011-12-12 2015-06-03 川崎重工業株式会社 アブレータ
JP6253871B2 (ja) * 2012-01-17 2017-12-27 三菱重工業株式会社 断熱材及びそれを備えた宇宙機、並びに断熱材の製造方法
US9656769B2 (en) * 2013-05-01 2017-05-23 Mohammad A. Mazed Heat shield for a spacecraft
JP6353686B2 (ja) * 2014-04-10 2018-07-04 三菱重工業株式会社 再突入機の製造方法
US9522747B2 (en) * 2014-06-03 2016-12-20 Analytical Mechanics Associates, Inc. Inflatable deceleration apparatus
US9475593B2 (en) * 2014-08-18 2016-10-25 The Boeing Company Dual layer sandwich for thermal management
US9475261B2 (en) * 2014-08-18 2016-10-25 The Boeing Company Dual layer sandwich for thermal management

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH09239847A (ja) * 1996-03-14 1997-09-16 Nissan Motor Co Ltd 低密度ｆｒｐアブレータ
JP2001247100A (ja) * 2000-03-07 2001-09-11 Natl Space Development Agency Of Japan アブレータ
JP2013028166A (ja) * 2012-07-25 2013-02-07 Institute Of National Colleges Of Technology Japan 熱防御複合材の製造方法

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP3130544A4 *

Also Published As

Publication number Publication date
JP6353686B2 (ja) 2018-07-04
EP3130544A4 (en) 2017-05-24
US20170029140A1 (en) 2017-02-02
EP3130544B1 (en) 2022-06-01
US10647452B2 (en) 2020-05-12
JP2015202701A (ja) 2015-11-16
EP3130544A1 (en) 2017-02-15

Similar Documents

Publication Publication Date Title
CN102089131B (zh) 用于复合部件制造的热效工具
US10723438B2 (en) System and methods of constructing composite assemblies
JP7029288B2 (ja) 硬化ハイブリッド絶縁非酸化物断熱システム、及び硬化ハイブリッド絶縁非酸化物断熱システムを製造するための非酸化物セラミック複合材料を生成する方法
JP2001106997A (ja) 吸音及び衝撃緩衝用接着シートと、これを用いたソーブレード並びにその製造方法
JP5590686B2 (ja) 熱防御複合材の製造方法
JP6353686B2 (ja) 再突入機の製造方法
KR20100083543A (ko) 실리카 에어로젤에 부직포 상태의 섬유가 보강된 유연성이 우수한 단열재의 제조방법 및 그 방법에 의하여 제조된 단열재
JP6204092B2 (ja) 補強構造体の製造方法
JP2015174807A (ja) 炭素繊維系断熱材及びその製造方法
CN108327153A (zh) 一种复合材料硬质落球整流罩制备技术
US9283711B1 (en) Hybrid ablative thermal protection systems and associated methods
JP5263737B2 (ja) 熱防御複合材の製造方法
KR20110107759A (ko) 적어도 두 개의 다른 복합부재로 된 조립체로 구성된 강화복합부품
US20150336684A1 (en) Lightning Strike Protection Material for dry lay-up / dry fiber placement device
JP2019098704A (ja) 複合材料の接合方法及び複合材料
KR101188769B1 (ko) 고무와 에폭시 수지 함유 복합재료와의 접착력 증진 방법
JP2011520624A (ja) 繊維複合材料の表面処理装置及び方法
EP2662203B1 (en) Contour caul with expansion region and method for its manufacture
CN107984774A (zh) 一种复合材料尾翼制备技术
JP6122377B2 (ja) 表面が強化された熱防御複合材およびその製造方法
KR101499812B1 (ko) 자동차용 고내열성 흡차음재의 제조방법
CN207916217U (zh) 一种纤维增强型高性能复合薄膜
JP2015202701A5 (OSRAM)
KR101895541B1 (ko) 차량용 엔진룸 제조방법
JP2018145392A (ja) 高分子リン酸化アミドを含むアブレーティブ材料

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 15776733

Country of ref document: EP

Kind code of ref document: A1

WWE Wipo information: entry into national phase

Ref document number: 15302292

Country of ref document: US

NENP Non-entry into the national phase

Ref country code: DE

REEP Request for entry into the european phase

Ref document number: 2015776733

Country of ref document: EP

WWE Wipo information: entry into national phase

Ref document number: 2015776733

Country of ref document: EP