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公开(公告)号：JPH11294189A
公开(公告)日：1999-10-26
申请号：JP5098099
申请日：1999-02-26
Applicant: UNITED TECHNOLOGIES CORP
Inventor： HONDA KEITH T , WEINER HARVEY I
IPC: F01D25/24 , F01D17/00 , F01D17/10 , F01D17/12 , F01D17/14 , F01D25/16 , F02C6/08 , F02C7/00 , F02C9/18 , F02K3/06 , F04D27/02 , F16C13/00
Abstract: PROBLEM TO BE SOLVED: To improve the sealing effect of a seal, and to reduce the leakage by reducing the influence exerted by the deformation caused by an operating load upon a sealing member. SOLUTION: A liner 76 for the guide assembly track opening 56 for a gas turbine engine is provided with a pair of parallel curved rail walls 102, 104 and a plate 15 extended between these rail walls. This plate 15 is provided with a pair of flanges 158, 166 extended from the walls, and is engageable with the engine stator structure by means of these flanges. By forming the liner 76 by a material harder than the housing 42, the durability of the ring assembly for combining the liner 76 with the liner 76 can be improved.
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公开(公告)号：JP2000186571A
公开(公告)日：2000-07-04
申请号：JP35530899
申请日：1999-12-15
Applicant: UNITED TECHNOLOGIES CORP
Inventor： WEINER HARVEY I , DEMERS CHRISTOPHER G
Abstract: PROBLEM TO BE SOLVED: To minimize gas dynamic clearance in the cruise operating state of an engine by supplying a lubricant to the surface of a seal land. SOLUTION: A rotary machine assembling method has a step of forming a sub-assembly including a lower pressure compressor rotary assembly and a step of forming a case assembly for a low pressure rotary assembly. Further, the method has a step of supplying a lubricant to at least one seal land 112 before the case assembly is assembled in the rotary assembly. The clearance can be made in the minimum clearance dimensions by using silicone oil as a lubricant, and a pilot rod of a blade which is normally difficult to be turned by hand can be freely turned by supplying silicone foil to the seal land. Lowering of characteristic of a component where the lubricant touches is prevented.
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公开(公告)号：JP2000186507A
公开(公告)日：2000-07-04
申请号：JP35530799
申请日：1999-12-15
Applicant: UNITED TECHNOLOGIES CORP
Inventor： WEINER HARVEY I , DEMERS CHRISTOPHER G
Abstract: PROBLEM TO BE SOLVED: To provide an axial flow gas turbine engine which can minimize a gas dynamical clearance under cruising condition of the engine, which can be assembled, and in which a low pressure compressor and a low pressure turbine assembly can be inspected. SOLUTION: A rotary machine which has rotor raw material 54-56, 114 and seal lands 86, 112 has been disclosed. Details of various structures are developed for easy assembly of machine. In one embodiment, clearance is established between a moving blade 66 and a seal land 86 to make assembly of components possible, and a certain clearance which is acceptable under steady state of an engine is supplied.
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公开(公告)号：DE69926594D1
公开(公告)日：2005-09-15
申请号：DE69926594
申请日：1999-12-22
Applicant: UNITED TECHNOLOGIES CORP
Inventor： WEINER HARVEY I , DEMERS CHRISTOPHER G
Abstract: A gas turbine engine comprises a rotor (50) provided with rotor blades (50,56,58,62,64,66), and a stator (68) provided with stator varies (92,94,96,98,102,104). Airseals are formed between the rotor (56) and stator (68) by providing rubstrips (86) adjacent the tips of the rotor blades (54-66), and by providing seals knife edge seals (112,114) adjacent the tips of the stator varies (92-104). In order to minimise the clearance between the rotor and stator during operation, and hence improve the efficiency of the engine, during construction an interference fit is provided between the rotor (50) and stator (68) say between the rotor blades (54-66) and the rubstrips (86), so that during operation the clearance between the rotor (50) and the stator (68) is minimised and the engines efficiency is improved.
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公开(公告)号：CA1230059A
公开(公告)日：1987-12-08
申请号：CA486044
申请日：1985-06-28
Applicant: UNITED TECHNOLOGIES CORP
Inventor： WEINER HARVEY I
Abstract: Valve and Manifold for Compressor Bore Heating The bore of the compressor of a gas turbine engine is selectively heated by mid-stage compressor bleed air and a higher stage compressor bleed air utilizing a two position valve integral with the engine case and manifold with provision for fail-safe in the lower temperature bleed air position.
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Patent Agency Ranking
公开(公告)号：DE69926594T2
公开(公告)日：2006-05-18
申请号：DE69926594
申请日：1999-12-22
Applicant: UNITED TECHNOLOGIES CORP
Inventor： WEINER HARVEY I , DEMERS CHRISTOPHER G
Abstract: A gas turbine engine comprises a rotor (50) provided with rotor blades (50,56,58,62,64,66), and a stator (68) provided with stator varies (92,94,96,98,102,104). Airseals are formed between the rotor (56) and stator (68) by providing rubstrips (86) adjacent the tips of the rotor blades (54-66), and by providing seals knife edge seals (112,114) adjacent the tips of the stator varies (92-104). In order to minimise the clearance between the rotor and stator during operation, and hence improve the efficiency of the engine, during construction an interference fit is provided between the rotor (50) and stator (68) say between the rotor blades (54-66) and the rubstrips (86), so that during operation the clearance between the rotor (50) and the stator (68) is minimised and the engines efficiency is improved.
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公开(公告)号：DE69923935T2
公开(公告)日：2006-04-06
申请号：DE69923935
申请日：1999-12-22
Applicant: UNITED TECHNOLOGIES CORP
Inventor： WEINER HARVEY I , DEMERS CHRISTOPHER G
Abstract: A method for assembling a rotary machine 10 having a rotor 50 and rotor blades 54-66 and a stator 68 and stator values 92-104 is disclosed. During construction a lubricating oil is used to facilitate rotation of the rotor 50 within the stator 68, thereby allowing an interference fit to be provided between the rotor 50 and stator 68 which improves the efficiency of the engine during operation.
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公开(公告)号：DE69919613T2
公开(公告)日：2005-09-08
申请号：DE69919613
申请日：1999-03-01
Applicant: UNITED TECHNOLOGIES CORP
Inventor： HONDA KEITH T , WEINER HARVEY I
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公开(公告)号：DE69923935D1
公开(公告)日：2005-04-07
申请号：DE69923935
申请日：1999-12-22
Applicant: UNITED TECHNOLOGIES CORP
Inventor： WEINER HARVEY I , DEMERS CHRISTOPHER G
Abstract: A method for assembling a rotary machine 10 having a rotor 50 and rotor blades 54-66 and a stator 68 and stator values 92-104 is disclosed. During construction a lubricating oil is used to facilitate rotation of the rotor 50 within the stator 68, thereby allowing an interference fit to be provided between the rotor 50 and stator 68 which improves the efficiency of the engine during operation.
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公开(公告)号：DE69919613D1
公开(公告)日：2004-09-30
申请号：DE69919613
申请日：1999-03-01
Applicant: UNITED TECHNOLOGIES CORP
Inventor： HONDA KEITH T , WEINER HARVEY I
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