US7108045B2
(en)
*
|
2004-09-09 |
2006-09-19 |
United Technologies Corporation |
Composite core for use in precision investment casting
|
US20070068649A1
(en)
*
|
2005-09-28 |
2007-03-29 |
Verner Carl R |
Methods and materials for attaching ceramic and refractory metal casting cores
|
US7744347B2
(en)
*
|
2005-11-08 |
2010-06-29 |
United Technologies Corporation |
Peripheral microcircuit serpentine cooling for turbine airfoils
|
US7861766B2
(en)
*
|
2006-04-10 |
2011-01-04 |
United Technologies Corporation |
Method for firing a ceramic and refractory metal casting core
|
US7753104B2
(en)
*
|
2006-10-18 |
2010-07-13 |
United Technologies Corporation |
Investment casting cores and methods
|
GB2444483B
(en)
|
2006-12-09 |
2010-07-14 |
Rolls Royce Plc |
A core for use in a casting mould
|
US7866370B2
(en)
|
2007-01-30 |
2011-01-11 |
United Technologies Corporation |
Blades, casting cores, and methods
|
US8083511B2
(en)
*
|
2007-12-05 |
2011-12-27 |
United Technologies Corp. |
Systems and methods involving pattern molds
|
EP2127781A1
(fr)
*
|
2008-05-29 |
2009-12-02 |
Siemens Aktiengesellschaft |
Procédé de fabrication d'une aube de turbine
|
US9174271B2
(en)
*
|
2008-07-02 |
2015-11-03 |
United Technologies Corporation |
Casting system for investment casting process
|
US8157527B2
(en)
*
|
2008-07-03 |
2012-04-17 |
United Technologies Corporation |
Airfoil with tapered radial cooling passage
|
US8317461B2
(en)
*
|
2008-08-27 |
2012-11-27 |
United Technologies Corporation |
Gas turbine engine component having dual flow passage cooling chamber formed by single core
|
US8572844B2
(en)
*
|
2008-08-29 |
2013-11-05 |
United Technologies Corporation |
Airfoil with leading edge cooling passage
|
US8303252B2
(en)
*
|
2008-10-16 |
2012-11-06 |
United Technologies Corporation |
Airfoil with cooling passage providing variable heat transfer rate
|
US8100165B2
(en)
*
|
2008-11-17 |
2012-01-24 |
United Technologies Corporation |
Investment casting cores and methods
|
US8113780B2
(en)
*
|
2008-11-21 |
2012-02-14 |
United Technologies Corporation |
Castings, casting cores, and methods
|
US8171978B2
(en)
|
2008-11-21 |
2012-05-08 |
United Technologies Corporation |
Castings, casting cores, and methods
|
US8109725B2
(en)
|
2008-12-15 |
2012-02-07 |
United Technologies Corporation |
Airfoil with wrapped leading edge cooling passage
|
US8347947B2
(en)
|
2009-02-17 |
2013-01-08 |
United Technologies Corporation |
Process and refractory metal core for creating varying thickness microcircuits for turbine engine components
|
US20110020115A1
(en)
*
|
2009-07-27 |
2011-01-27 |
United Technologies Corporation |
Refractory metal core integrally cast exit trench
|
FR2950825B1
(fr)
*
|
2009-10-01 |
2011-12-09 |
Snecma |
Procede ameliore de fabrication d'un ensemble annulaire aubage de turbomachine a la cire perdue, moule metallique et modele en cire pour la mise en oeuvre d'un tel procede
|
US20110315336A1
(en)
*
|
2010-06-25 |
2011-12-29 |
United Technologies Corporation |
Contoured Metallic Casting Core
|
US8302668B1
(en)
|
2011-06-08 |
2012-11-06 |
United Technologies Corporation |
Hybrid core assembly for a casting process
|
US8291963B1
(en)
|
2011-08-03 |
2012-10-23 |
United Technologies Corporation |
Hybrid core assembly
|
EP2636466A1
(fr)
*
|
2012-03-07 |
2013-09-11 |
Siemens Aktiengesellschaft |
Noyau de moulage d'un composant creux
|
US9079803B2
(en)
|
2012-04-05 |
2015-07-14 |
United Technologies Corporation |
Additive manufacturing hybrid core
|
US9279331B2
(en)
|
2012-04-23 |
2016-03-08 |
United Technologies Corporation |
Gas turbine engine airfoil with dirt purge feature and core for making same
|
US10005123B2
(en)
|
2013-10-24 |
2018-06-26 |
United Technologies Corporation |
Lost core molding cores for forming cooling passages
|
US10370980B2
(en)
|
2013-12-23 |
2019-08-06 |
United Technologies Corporation |
Lost core structural frame
|
FR3037829B1
(fr)
*
|
2015-06-29 |
2017-07-21 |
Snecma |
Noyau pour le moulage d'une aube ayant des cavites superposees et comprenant un trou de depoussierage traversant une cavite de part en part
|
US10099276B2
(en)
|
2015-12-17 |
2018-10-16 |
General Electric Company |
Method and assembly for forming components having an internal passage defined therein
|
US9987677B2
(en)
|
2015-12-17 |
2018-06-05 |
General Electric Company |
Method and assembly for forming components having internal passages using a jacketed core
|
US9968991B2
(en)
|
2015-12-17 |
2018-05-15 |
General Electric Company |
Method and assembly for forming components having internal passages using a lattice structure
|
US10137499B2
(en)
|
2015-12-17 |
2018-11-27 |
General Electric Company |
Method and assembly for forming components having an internal passage defined therein
|
US10099284B2
(en)
|
2015-12-17 |
2018-10-16 |
General Electric Company |
Method and assembly for forming components having a catalyzed internal passage defined therein
|
US10150158B2
(en)
|
2015-12-17 |
2018-12-11 |
General Electric Company |
Method and assembly for forming components having internal passages using a jacketed core
|
US9579714B1
(en)
|
2015-12-17 |
2017-02-28 |
General Electric Company |
Method and assembly for forming components having internal passages using a lattice structure
|
US10099283B2
(en)
|
2015-12-17 |
2018-10-16 |
General Electric Company |
Method and assembly for forming components having an internal passage defined therein
|
US10046389B2
(en)
|
2015-12-17 |
2018-08-14 |
General Electric Company |
Method and assembly for forming components having internal passages using a jacketed core
|
US10118217B2
(en)
|
2015-12-17 |
2018-11-06 |
General Electric Company |
Method and assembly for forming components having internal passages using a jacketed core
|
FR3046736B1
(fr)
*
|
2016-01-15 |
2021-04-23 |
Safran |
Noyau refractaire comprenant un corps principal et une coque
|
US10286450B2
(en)
|
2016-04-27 |
2019-05-14 |
General Electric Company |
Method and assembly for forming components using a jacketed core
|
US10335853B2
(en)
|
2016-04-27 |
2019-07-02 |
General Electric Company |
Method and assembly for forming components using a jacketed core
|
US10443403B2
(en)
|
2017-01-23 |
2019-10-15 |
General Electric Company |
Investment casting core
|
US10596621B1
(en)
*
|
2017-03-29 |
2020-03-24 |
United Technologies Corporation |
Method of making complex internal passages in turbine airfoils
|
US10556269B1
(en)
|
2017-03-29 |
2020-02-11 |
United Technologies Corporation |
Apparatus for and method of making multi-walled passages in components
|
US11236625B2
(en)
*
|
2017-06-07 |
2022-02-01 |
General Electric Company |
Method of making a cooled airfoil assembly for a turbine engine
|
CN107237676A
(zh)
*
|
2017-06-30 |
2017-10-10 |
潍柴动力股份有限公司 |
发动机排气管、发动机及发动机排气管的铸造方法
|
US11053803B2
(en)
*
|
2019-06-26 |
2021-07-06 |
Raytheon Technologies Corporation |
Airfoils and core assemblies for gas turbine engines and methods of manufacture
|
US11041395B2
(en)
|
2019-06-26 |
2021-06-22 |
Raytheon Technologies Corporation |
Airfoils and core assemblies for gas turbine engines and methods of manufacture
|
US11813665B2
(en)
*
|
2020-09-14 |
2023-11-14 |
General Electric Company |
Methods for casting a component having a readily removable casting core
|