SG11201901765PA - Additive manufactured combustion engine - Google Patents
Additive manufactured combustion engineInfo
- Publication number
- SG11201901765PA SG11201901765PA SG11201901765PA SG11201901765PA SG11201901765PA SG 11201901765P A SG11201901765P A SG 11201901765PA SG 11201901765P A SG11201901765P A SG 11201901765PA SG 11201901765P A SG11201901765P A SG 11201901765PA SG 11201901765P A SG11201901765P A SG 11201901765PA
- Authority
- SG
- Singapore
- Prior art keywords
- engine
- international
- september
- fo2c
- pct
- Prior art date
Links
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details not otherwise provided for
- F02K9/62—Combustion or thrust chambers
- F02K9/64—Combustion or thrust chambers having cooling arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P11/00—Component parts, details, or accessories not provided for in, or of interest apart from, groups F01P1/00 - F01P9/00
- F01P11/04—Arrangements of liquid pipes or hoses
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P3/00—Liquid cooling
- F01P3/20—Cooling circuits not specific to a single part of engine or machine
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/97—Rocket nozzles
- F02K9/972—Fluid cooling arrangements for nozzles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M53/00—Fuel-injection apparatus characterised by having heating, cooling or thermally-insulating means
- F02M53/04—Injectors with heating, cooling, or thermally-insulating means
- F02M53/043—Injectors with heating, cooling, or thermally-insulating means with cooling means other than air cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D7/00—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
- F28D7/0041—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for only one medium being tubes having parts touching each other or tubes assembled in panel form
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D7/00—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
- F28D7/16—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged in parallel spaced relation
- F28D7/163—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being arranged in parallel spaced relation with conduit assemblies having a particular shape, e.g. square or annular; with assemblies of conduits having different geometrical features; with multiple groups of conduits connected in series or parallel and arranged inside common casing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/30—Manufacture with deposition of material
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D21/00—Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
- F28D2021/0019—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
- F28D2021/0026—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for combustion engines, e.g. for gas turbines or for Stirling engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F2210/00—Heat exchange conduits
- F28F2210/02—Heat exchange conduits with particular branching, e.g. fractal conduit arrangements
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Geometry (AREA)
- Fuel-Injection Apparatus (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
- Medicinal Preparation (AREA)
- Peptides Or Proteins (AREA)
Abstract
INTERNATIONAL APPLICATION PUBLISHED UNDER THE PATENT COOPERATION TREATY (PCT) (19) World Intellectual Property Organization International Bureau (43) International Publication Date 08 March 2018 (08.03.2018) WIPO I PCT IiiimmoimiolollmonoloolommollommumovoimIE (10) International Publication Number WO 2018/045351 Al (51) International Patent Classification: FO2C 7/12 (2006.01) FO2C 7/18 (2006.01) FO2C 7/16 (2006.01) (21) International Application Number: PCT/US2017/049963 (22) International Filing Date: 01 September 2017 (01.09.2017) (25) Filing Language: English (26) Publication Language: English (30) Priority Data: 62/382,722 01 September 2016 (01.09.2016) US 62/385,123 08 September 2016 (08.09.2016) US 62/385,122 08 September 2016 (08.09.2016) US (71) Applicant: ADDITIVE ROCKET CORPORATION [US/US]; 4405 Mission Avenue, Apt. K204, Oceanside, CA 92057 (US). (72) Inventors: ADRIANY, Kyle; 4185 Porte De Palmas Unit 164, San Diego, CA 92122 (US). KIEATIWONG, Andy; 4185 Porte De Palmas Unit 164, San Diego, CA 92122 (US). TRAN, Anthony; 607 N Chandler Ave, Monterey Park, CA 91754 (US). BAYAT, Eiyce; 1431 Finley Road, Pleasanton, CA 94588 (US). KNIGHT, Michael; 4405 Mission Ave #k204, Oceanside, CA 92057 (US). LOPEZ, Nicholas; 926 S Lone Pine Lane, Anaheim, CA 92808 (US). GARRETT, Nicholas; 13500 Hidden Valley Rd, Victorville, CA 92395 (US). PEDERSEN, Ryan; 22114 Briarwood Ct., Walnut, CA 91789 (US). (74) Agent: KWAN, Jordan; K&L Gates LLP, 630 Hansen Way, Palo Alto, CA 94304 (US). (81) Designated States (unless otherwise indicated, for every kind of national protection available): AE, AG, AL, AM, AO, AT, AU, AZ, BA, BB, BG, BH, BN, BR, BW, BY, BZ, CA, CH, CL, CN, CO, CR, CU, CZ, DE, DJ, DK, DM, DO, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, GT, HN, HR, HU, ID, IL, IN, IR, IS, JO, JP, KE, KG, KH, KN, KP, = (54) Title: ADDITIVE MANUFACTURED COMBUSTION ENGINE FIG. (57) : Aspects of the present disclosure are presented for a combustion engine design with an optimized amount of materials used to generate the necessary components of the engine. The engine may be generated as a single piece, having no joints, fasteners, or any other areas that could present a risk for damage. The designs are described may also reduce weight of the engine, due to eliminating the need for fasteners and other extraneous hardware. In general, the weight of the engine may be optimized to also preclude the inclusion of extraneous material around needed structures. Also, the engine may be designed to be highly energy efficient, with optimal flows for fuel and other fluid with minimal head loss while maintaining higher pressures. [Continued on next page] WO 2018/045351 Al MIDEDIMOMOIDEIREEMOMIUMMEMOInin KR, KW, KZ, LA, LC, LK, LR, LS, LU, LY, MA, MD, ME, MG, MK, MN, MW, MX, MY, MZ, NA, NG, NI, NO, NZ, OM, PA, PE, PG, PH, PL, PT, QA, RO, RS, RU, RW, SA, SC, SD, SE, SG, SK, SL, SM, ST, SV, SY, TH, TJ, TM, TN, TR, TT, TZ, UA, UG, US, UZ, VC, VN, ZA, ZM, ZW. (84) Designated States (unless otherwise indicated, for every kind of regional protection available): ARIPO (BW, GH, GM, KE, LR, LS, MW, MZ, NA, RW, SD, SL, ST, SZ, TZ, UG, ZM, ZW), Eurasian (AM, AZ, BY, KG, KZ, RU, TJ, TM), European (AL, AT, BE, BG, CH, CY, CZ, DE, DK, EE, ES, FI, FR, GB, GR, HR, HU, IE, IS, IT, LT, LU, LV, MC, MK, MT, NL, NO, PL, PT, RO, RS, SE, SI, SK, SM, TR), OAPI (BF, BJ, CF, CG, CI, CM, GA, GN, GQ, GW, KM, ML, MR, NE, SN, TD, TG). Published: — with international search report (Art. 21(3))
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201662382722P | 2016-09-01 | 2016-09-01 | |
US201662385123P | 2016-09-08 | 2016-09-08 | |
US201662385122P | 2016-09-08 | 2016-09-08 | |
PCT/US2017/049963 WO2018045351A1 (en) | 2016-09-01 | 2017-09-01 | Additive manufactured combustion engine |
Publications (1)
Publication Number | Publication Date |
---|---|
SG11201901765PA true SG11201901765PA (en) | 2019-03-28 |
Family
ID=61301642
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG11201901765PA SG11201901765PA (en) | 2016-09-01 | 2017-09-01 | Additive manufactured combustion engine |
Country Status (9)
Country | Link |
---|---|
US (1) | US20180087443A1 (en) |
EP (1) | EP3507473A4 (en) |
JP (1) | JP2019534409A (en) |
KR (1) | KR20190042071A (en) |
AU (1) | AU2017318721A1 (en) |
CA (1) | CA3035767A1 (en) |
IL (1) | IL265149A (en) |
SG (1) | SG11201901765PA (en) |
WO (1) | WO2018045351A1 (en) |
Families Citing this family (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10041745B2 (en) | 2010-05-04 | 2018-08-07 | Fractal Heatsink Technologies LLC | Fractal heat transfer device |
EP3485215B1 (en) | 2016-07-12 | 2023-06-07 | Alexander Poltorak | System and method for maintaining efficiency of a heat sink |
US11103925B2 (en) * | 2018-03-22 | 2021-08-31 | The Boeing Company | Additively manufactured antenna |
US10801450B2 (en) | 2018-07-11 | 2020-10-13 | Ford Global Technologies, Llc | Intake system assembly and method for manufacturing the assembly |
US11270049B2 (en) | 2018-09-12 | 2022-03-08 | Siemens Industry Software Inc. | Internal channel network detections for 3D printing |
CN109296474A (en) * | 2018-09-27 | 2019-02-01 | 宁波天擎航天科技有限公司 | A kind of rocket engine |
DE102018008989A1 (en) | 2018-11-15 | 2020-05-20 | Daimler Ag | Process for producing a component or a surface coating |
US20200182196A1 (en) * | 2018-12-11 | 2020-06-11 | Stratolaunch Research, Inc. | Combustion chamber liner with spiral cooling channels |
US20200240365A1 (en) | 2019-01-30 | 2020-07-30 | Laboratoire Reaction Dynamics Inc. | Thrust vector control for hybrid propellants rocket engine with embedded fluid injection ports |
WO2020154809A1 (en) * | 2019-01-30 | 2020-08-06 | Laboratoire Reaction Dynamics Inc. | Rocket engines |
US11283143B2 (en) | 2019-05-24 | 2022-03-22 | The Boeing Company | Additively manufactured radio frequency filter |
US11545743B2 (en) | 2019-05-24 | 2023-01-03 | The Boeing Company | Additively manufactured mesh cavity antenna |
CN110307564B (en) * | 2019-06-12 | 2023-03-10 | 中南大学 | Split type combustion chamber and engine and heat protection method thereof |
CN110586937B (en) * | 2019-09-23 | 2021-10-15 | 南京中科煜宸激光技术有限公司 | 3D printing method for metal combustion chamber of civil rocket engine |
CN113224893B (en) * | 2020-01-21 | 2023-03-28 | 上海电力大学 | Optimization method for cooling water channel of vehicle-mounted permanent magnet synchronous motor |
US11961662B2 (en) * | 2020-07-08 | 2024-04-16 | GE Precision Healthcare LLC | High temperature superconducting current lead assembly for cryogenic apparatus |
DE102020124530A1 (en) * | 2020-09-21 | 2022-03-24 | Arianegroup Gmbh | Combustor section with integrated baffle and method of manufacturing a combustor section |
DE102020124542A1 (en) | 2020-09-21 | 2022-03-24 | Arianegroup Gmbh | Combustion chamber with a vibration-damping inner wall shape and method for manufacturing a combustion chamber section |
US11909110B2 (en) * | 2020-09-30 | 2024-02-20 | The Boeing Company | Additively manufactured mesh horn antenna |
KR20230132766A (en) * | 2020-10-23 | 2023-09-18 | 아그니쿨 코스모스 프라이빗 리미티드 | Design and manufacturing of single-piece rocket engines |
WO2023034291A2 (en) * | 2021-08-30 | 2023-03-09 | Agile Space Industries, Inc. | Systems and methods for design, manufacture, and test of space thruster propulsion systems |
WO2024017865A1 (en) | 2022-07-19 | 2024-01-25 | Heliuspace B.V. | Aerospace vehicle having a spike engine, and methods of operating and simulating thereof |
Family Cites Families (19)
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US2523654A (en) * | 1948-01-02 | 1950-09-26 | Daniel And Florence Guggenheim | Feeding and cooling wall structure for combustion chambers using liquid combustion elements |
US4781019A (en) * | 1983-04-04 | 1988-11-01 | Rockwell International Corporation | Keel-rib coolant channels for rocket combustors |
US4801092A (en) * | 1986-02-24 | 1989-01-31 | Rockwell International Corporation | Injector assembly for a fluid fueled engine |
FR2640687B1 (en) * | 1988-12-21 | 1991-02-08 | Snecma | COMPRESSOR HOUSING OF A TURBOMACHINE WITH STEERING OF ITS INTERNAL DIAMETER |
DE4222391C2 (en) * | 1992-07-08 | 1995-04-20 | Gutehoffnungshuette Man | Cylindrical combustion chamber housing of a gas turbine |
RO120359B1 (en) * | 1998-06-12 | 2005-12-30 | S.C. Romradiatoare S.A. | Heat exchanger radiating element and process for making such a heat exchanger |
KR100382523B1 (en) * | 2000-12-01 | 2003-05-09 | 엘지전자 주식회사 | a tube structure of a micro-multi channel heat exchanger |
US6783824B2 (en) * | 2001-01-25 | 2004-08-31 | Hyper-Therm High-Temperature Composites, Inc. | Actively-cooled fiber-reinforced ceramic matrix composite rocket propulsion thrust chamber and method of producing the same |
EP1227071A3 (en) * | 2001-01-25 | 2004-01-07 | Hyper-Therm, Inc. | Cooled ceramic rocket combustion chamber |
GB0521826D0 (en) * | 2005-10-26 | 2005-12-07 | Rolls Royce Plc | Wall cooling arrangement |
US7966809B2 (en) * | 2006-02-01 | 2011-06-28 | Spacedev, Inc. | Single-piece hybrid rocket motor |
WO2008010748A1 (en) * | 2006-07-19 | 2008-01-24 | Volvo Aero Corporation | Method for manufacturing a wall structure |
FR2945580B1 (en) * | 2009-05-15 | 2015-12-25 | Snecma | ENGINE COMBUSTION CHAMBER FOR A VEHICLE CAPABLE OF MOVING IN AIR OR SPACE AND METHOD OF MANUFACTURING THE SAME |
US9382810B2 (en) * | 2012-07-27 | 2016-07-05 | General Electric Company | Closed loop cooling system for a gas turbine |
US9803865B2 (en) * | 2012-12-28 | 2017-10-31 | General Electric Company | System and method for a turbine combustor |
GB201301624D0 (en) * | 2013-01-30 | 2013-03-13 | Rolls Royce Plc | A Method Of Manufacturing A Wall |
US9777674B2 (en) * | 2014-02-26 | 2017-10-03 | Deepak Atyam | Injector plate for a rocket engine |
WO2015155733A1 (en) * | 2014-04-09 | 2015-10-15 | Avio S.P.A. | Combustor of a liquid propellent motor |
US9643251B2 (en) * | 2014-06-13 | 2017-05-09 | Zin Technologies, Inc. | Optimized additive manufacturing process |
-
2017
- 2017-09-01 SG SG11201901765PA patent/SG11201901765PA/en unknown
- 2017-09-01 WO PCT/US2017/049963 patent/WO2018045351A1/en unknown
- 2017-09-01 AU AU2017318721A patent/AU2017318721A1/en not_active Abandoned
- 2017-09-01 US US15/694,686 patent/US20180087443A1/en not_active Abandoned
- 2017-09-01 CA CA3035767A patent/CA3035767A1/en not_active Abandoned
- 2017-09-01 JP JP2019512822A patent/JP2019534409A/en active Pending
- 2017-09-01 EP EP17847662.8A patent/EP3507473A4/en not_active Withdrawn
- 2017-09-01 KR KR1020197008714A patent/KR20190042071A/en unknown
-
2019
- 2019-03-03 IL IL265149A patent/IL265149A/en unknown
Also Published As
Publication number | Publication date |
---|---|
KR20190042071A (en) | 2019-04-23 |
JP2019534409A (en) | 2019-11-28 |
WO2018045351A1 (en) | 2018-03-08 |
AU2017318721A1 (en) | 2019-04-18 |
EP3507473A4 (en) | 2020-06-10 |
US20180087443A1 (en) | 2018-03-29 |
IL265149A (en) | 2019-05-30 |
CA3035767A1 (en) | 2018-03-08 |
EP3507473A1 (en) | 2019-07-10 |
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