Patents-Review.com
ClassID:

43567 ⎘

B23P15/008 - CPC Classification

Classification description:

Making specific metal objects by operations not covered by a single other subclass or a group in this subclass Rocket engine parts, e.g. nozzles, combustion chambers

Recent Application in this class:
#1
20240375201
2024-11-14

BLADE FOR A ROTOR ASSEMBLY OF A TURBINE ENGINE

 #2
20240271535
2024-08-15

Cooling jacket of a hollow blade of a distributor

 #3
20240254889
2024-08-01

Substrate Edge Configurations for Ceramic Coatings

 #4
20240159160
2024-05-16

Air seal system with backside abradable layer

 #5
20230407767
2023-12-21

SPLIT CASE STRUCTURE FOR A GAS TURBINE ENGINE

 #6
20230125860
2023-04-27

Combustor for rocket engine and method for manufacturing it

 #7
20220136409
2022-05-05

Split case structure for a gas turbine engine

 #8
20210355838
2021-11-18

Substrate edge configurations for ceramic coatings

 #9
20210324794
2021-10-21

Acoustic cores with sound-attenuating protuberances

 #10
20210199017
2021-07-01

Method of manufacturing a rotor disc for a turbine engine

 #11
20210123384
2021-04-29

Blade fragment barrier for aircraft engine inlet cowl

 #12
20200299853
2020-09-24

Method for producing a thermal barrier on a part of a turbomachine

 #13
20200049068
2020-02-13

Acoustic cores with sound-attenuating protuberances

 #14
20200011332
2020-01-09

Retaining ring anti-migration system and method

 #15
20190329355
2019-10-31

Method for Fabricating Seal-Free Multi-Metallic Thrust Chamber Liner

 #16
20180272470
2018-09-27

Method for manufacturing a housing of a turbomachine

 #17
20180187884
2018-07-05

Circulating fluidized bed boiler and a method of assembling a circulating fluidized bed boiler

 #18
20180036843
2018-02-08

Method of assembling an annular combustion chamber assembly

 #19
20180031239
2018-02-01

COMBUSTOR CAP ASSEMBLY AND METHODS OF MANUFACTURE

 #20
20180030840
2018-02-01

Method of assembly of bi-cast turbine vane

 #21
20180010552
2018-01-11

COMBUSTION CHAMBER AND METHOD FOR THE PRODUCTION OF A COMBUSTION CHAMBER

 #22
20170307216
2017-10-26

Combustor thermal shield fabrication method

 #23
20170146235
2017-05-25

Method for reconditioning fuel nozzle assemblies

 #24
20170138218
2017-05-18

Method for mounting or dismounting turbine component, device for executing the method, and method for installing the device

 #25
20160169155
2016-06-16

DEVICE FOR CONNECTING TWO SEGMENTS OF A PROPELLING NOZZLE

 #26
20160141057
2016-05-19

Excavation and weld repair methodology for pressurized water reactor piping and vessel nozzles

 #27
20150354593
2015-12-10

TURBINE NOZZLE AND MANUFACTURING METHOD THEREOF

 #28
20150328721
2015-11-19

Radiographic markers for partial penetration welded joints

 #29
20150322890
2015-11-12

Center body attachment system

 #30
20150267644
2015-09-24

Integrated Primary Nozzle

 #31
20150165547
2015-06-18

Process for making a turbulator by additive manufacturing

 #32
20140352797
2014-12-04

AIRCRAFT JET ENGINE

 #33
20140255167
2014-09-11

Consumable assembly tool for a gas turbine engine

 #34
20130312263
2013-11-28

Method for manufacturing an air intake structure for a turbojet engine nacelle

 #35
20130186093
2013-07-25

Process of fabricating a fuel nozzle assembly

 #36
20130140281
2013-06-06

Truss-shaped engine pylon and method of making same

 #37
20130083414
2013-04-04

Segmented reflective optical system

 #38
20110192137
2011-08-11

Method for Manufacturing a Regeneratively Cooled Nozzle Extension of a Rocket Combustion Chamber and Nozzle Extension

 #39
20110121132
2011-05-26

Truss-shaped engine pylon and method of making same

 #40
20100002273
2010-01-07

Segmented reflective optical system

 #41
20070144142
2007-06-28

Outlet nozzle and a method for manufacturing an outlet nozzle

 #42
18233675
2024-02-06

Method of manufacture of plug nozzle with thrust reverser

 #43
17829986
2023-09-05

Liquid rocket engine cooling channels

 #44
15615539
2017-12-05

Freeform deposition method for coolant channel closeout