GB1257610A - - Google Patents

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Publication number
GB1257610A
GB1257610A GB1257610DA GB1257610A GB 1257610 A GB1257610 A GB 1257610A GB 1257610D A GB1257610D A GB 1257610DA GB 1257610 A GB1257610 A GB 1257610A
Authority
GB
United Kingdom
Prior art keywords
primary
flow
air
controlled
flame tube
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.)
Expired
Application number
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 filed Critical
Publication of GB1257610A publication Critical patent/GB1257610A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/26Controlling the air flow
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00001Arrangements using bellows, e.g. to adjust volumes or reduce thermal stresses

Abstract

1,257,610. Valves. JOSEPH LUCAS (INDUSTRIES) Ltd. 13 Dec., 1968 [10 Nov., 1967], No. 13709/71. Divided out of 1,256,066. Heading F2V. [Also in Division F1] An annular flame tube for a gas turbine engine having primary and secondary combustion air inlet passages has variable air flow restricting means associated with at least one of the passages, the restricting means being expandable in response to an increase in a variable control quantity to vary the ratio of primary to secondary combustion air. In one arrangement, Fig. 1, the annular flame tube 30 is enclosed by outer and inner annular walls 31, 32. The space between tube 30 and wall 31 contains a series of louvre type restrictors 90 controlling ducts 91 terminating in nozzles 92 which direct secondary air into the burning mixture of fuel and primary air, the latter air having entered the flame tube past fuel nozzles 33. Each set of louvres 90 is pivotal by means of a Bourdon tube 93 which receives a variable control pressure from a common manifold 94. Dilution air flow through nozzles 95 is controlled by closure members 96 having pressure operable bellows 97. In a modification (Fig. 5, not shown), Bourdon tubes (180) control the pivotal movement of restrictor segments (185) mounted in the primary air inlet passage. In a further modification, Fig. 3, the flame tube has a series of angularly spaced primary air inlet passages 140, each having a flow restrictor formed by angled end pieces 141b on bimetallic strips 141a. The latter are mounted on a ring 142, electric heating of which causes strips 141a to deflect so that end pieces 141b project further into the flow. Swirl vanes 143 are provided and surround a burner (not shown). In a similar arrangement (Fig. 4, not shown), the movement of restricting shutters (150 to 153) into the primary flow is controlled by electrically heated bimetallic strips (159, 160, 162, 163). In a further modification (Fig. 6, not shown), the primary flow is controlled by a spiral restrictor (200) extension and retraction of which is controlled by a pressurizable bellows (201) slidably mounted by means of sealing rings (203) on a central spindle (202).
GB1257610D 1967-11-10 1967-11-10 Expired GB1257610A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1370971 1967-11-10

Publications (1)

Publication Number Publication Date
GB1257610A true GB1257610A (en) 1971-12-22

Family

ID=10027955

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1257610D Expired GB1257610A (en) 1967-11-10 1967-11-10

Country Status (1)

Country Link
GB (1) GB1257610A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2452599A1 (en) * 1979-03-30 1980-10-24 Gen Electric IMPROVED SYSTEM FOR SUPPLYING COOLING AIR TO A TURBOMACHINE
EP2778531A1 (en) * 2013-03-13 2014-09-17 Siemens Aktiengesellschaft Gas turbine with optimized combustion in partial load operation by air flow rate adjustment
RU167336U1 (en) * 2016-04-06 2017-01-10 Публичное акционерное общество "Научно-производственное объединение "Сатурн" FIRE PIPE OF THE COMBUSTION CHAMBER OF A GAS TURBINE ENGINE
EP4008958A1 (en) 2020-12-07 2022-06-08 Deutsches Zentrum für Luft- und Raumfahrt e.V. Gas turbine combustion chamber system and method for operating same

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2452599A1 (en) * 1979-03-30 1980-10-24 Gen Electric IMPROVED SYSTEM FOR SUPPLYING COOLING AIR TO A TURBOMACHINE
EP2778531A1 (en) * 2013-03-13 2014-09-17 Siemens Aktiengesellschaft Gas turbine with optimized combustion in partial load operation by air flow rate adjustment
RU167336U1 (en) * 2016-04-06 2017-01-10 Публичное акционерное общество "Научно-производственное объединение "Сатурн" FIRE PIPE OF THE COMBUSTION CHAMBER OF A GAS TURBINE ENGINE
EP4008958A1 (en) 2020-12-07 2022-06-08 Deutsches Zentrum für Luft- und Raumfahrt e.V. Gas turbine combustion chamber system and method for operating same
DE102020132494A1 (en) 2020-12-07 2022-06-09 Deutsches Zentrum für Luft- und Raumfahrt e.V. Gas turbine combustor system and method of operating a gas turbine combustor system

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee