GB1249516A

GB1249516A – Electrical generator system especially for aerospace vehicles
– Google Patents

GB1249516A – Electrical generator system especially for aerospace vehicles
– Google Patents
Electrical generator system especially for aerospace vehicles

Info

Publication number
GB1249516A

GB1249516A
GB36397/69A
GB3639769A
GB1249516A
GB 1249516 A
GB1249516 A
GB 1249516A
GB 36397/69 A
GB36397/69 A
GB 36397/69A
GB 3639769 A
GB3639769 A
GB 3639769A
GB 1249516 A
GB1249516 A
GB 1249516A
Authority
GB
United Kingdom
Prior art keywords
electrical generator
generator system
output
july
armature winding
Prior art date
1968-07-19
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
GB36397/69A
Inventor
Horst Anton Heller
Walter Erich Mehnert
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)

Airbus Defence and Space GmbH

Original Assignee
Messerschmitt Bolkow Blohm AG
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.)
1968-07-19
Filing date
1969-07-18
Publication date
1971-10-13

1969-07-18
Application filed by Messerschmitt Bolkow Blohm AG
filed
Critical
Messerschmitt Bolkow Blohm AG

1971-10-13
Publication of GB1249516A
publication
Critical
patent/GB1249516A/en

Status
Expired
legal-status
Critical
Current

Links

Espacenet

Global Dossier

Discuss

Classifications

H—ELECTRICITY

H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER

H02K—DYNAMO-ELECTRIC MACHINES

H02K19/00—Synchronous motors or generators

H02K19/16—Synchronous generators

H02K19/36—Structural association of synchronous generators with auxiliary electric devices influencing the characteristic of the generator or controlling the generator, e.g. with impedances or switches

H—ELECTRICITY

H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER

H02K—DYNAMO-ELECTRIC MACHINES

H02K19/00—Synchronous motors or generators

H02K19/16—Synchronous generators

H02K19/36—Structural association of synchronous generators with auxiliary electric devices influencing the characteristic of the generator or controlling the generator, e.g. with impedances or switches

H02K19/365—Structural association of synchronous generators with auxiliary electric devices influencing the characteristic of the generator or controlling the generator, e.g. with impedances or switches with a voltage regulator

H—ELECTRICITY

H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER

H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS

H02P9/00—Arrangements for controlling electric generators for the purpose of obtaining a desired output

H02P9/14—Arrangements for controlling electric generators for the purpose of obtaining a desired output by variation of field

H02P9/38—Self-excitation by current derived from rectification of both output voltage and output current of generator

Abstract

1,249,516. A.C. generators with D.C. excitation. MESSERSCHMITT-BOLKOW-BLOHM G.m.b.H. 18 July, 1969 [19 July, 1968], No. 36397/69. Addition to 1,240,669. Heading H2A. To eliminate disturbances due to load current changes, the electrical generator system of claim 1 of Specification 1,224,031 is provided with a measuring device 151 which continuously measures current changes in the armature winding of the exciter generator 110 and applies such measurements to an additional device 150 which device also receives an input from the RF-signal transmission 140 and an average share of the exciter armature winding output to produce an output forming the firing impulse of the controlled retifier 152. These components are in the rotor 113 of the main synchronous generator 120 to whose output a regulator 160 is connected.

GB36397/69A
1968-07-19
1969-07-18
Electrical generator system especially for aerospace vehicles

Expired

GB1249516A
(en)

Applications Claiming Priority (1)

Application Number
Priority Date
Filing Date
Title

DE19681763697

DE1763697A1
(en)

1968-07-19
1968-07-19

Electrical generator system especially designed for aircraft and spacecraft

Publications (1)

Publication Number
Publication Date

GB1249516A
true

GB1249516A
(en)

1971-10-13

Family
ID=5697685
Family Applications (1)

Application Number
Title
Priority Date
Filing Date

GB36397/69A
Expired

GB1249516A
(en)

1968-07-19
1969-07-18
Electrical generator system especially for aerospace vehicles

Country Status (4)

Country
Link

US
(1)

US3612981A
(en)

DE
(1)

DE1763697A1
(en)

FR
(1)

FR2014658A1
(en)

GB
(1)

GB1249516A
(en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party

Publication number
Priority date
Publication date
Assignee
Title

EP2786480B1
(en)

2011-11-28
2020-07-22
ABB Schweiz AG
Rotating electrical machine

Family Cites Families (3)

* Cited by examiner, † Cited by third party

Publication number
Priority date
Publication date
Assignee
Title

US3290582A
(en)

*

1962-11-09
1966-12-06
Safety Electrical Equipment Co
Brushless generating system regulator which shunts excitation current from the fieldwinding

US3412271A
(en)

*

1965-12-08
1968-11-19
Westinghouse Electric Corp
Brushless type alternating current machine

US3401328A
(en)

*

1966-05-20
1968-09-10
Gen Electric
Brushless synchronous machine system

1968

1968-07-19
DE
DE19681763697
patent/DE1763697A1/en
active
Pending

1969

1969-07-09
US
US840301A
patent/US3612981A/en
not_active
Expired – Lifetime

1969-07-17
FR
FR6924355A
patent/FR2014658A1/fr
not_active
Withdrawn

1969-07-18
GB
GB36397/69A
patent/GB1249516A/en
not_active
Expired

Also Published As

Publication number
Publication date

US3612981A
(en)

1971-10-12

DE1763697A1
(en)

1971-07-01

FR2014658A1
(en)

1970-04-17

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