BE409896A - - Google Patents
Info
- Publication number
- BE409896A BE409896A BE409896DA BE409896A BE 409896 A BE409896 A BE 409896A BE 409896D A BE409896D A BE 409896DA BE 409896 A BE409896 A BE 409896A
- Authority
- BE
- Belgium
Links
Classifications
-
- H—ELECTRICITY
- H03—ELECTRONIC CIRCUITRY
- H03C—MODULATION
- H03C1/00—Amplitude modulation
- H03C1/16—Amplitude modulation by means of discharge device having at least three electrodes
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE2093729X | 1934-06-11 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE409896A true BE409896A (en:Method) |
Family
ID=7984627
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE409896D BE409896A (en:Method) | 1934-06-11 |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US2093729A (en:Method) |
| BE (1) | BE409896A (en:Method) |
| FR (1) | FR791087A (en:Method) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2438947A (en) * | 1943-07-28 | 1948-04-06 | Bell Telephone Labor Inc | Electronic modulation and modulation correction circuits |
| DE102006025388B4 (de) * | 2006-05-31 | 2009-10-29 | Airbus Deutschland Gmbh | Leitungssystemanordnung in einem einen Rumpf aufweisenden Luft- oder Raumfahrzeug |
-
0
- BE BE409896D patent/BE409896A/xx unknown
-
1935
- 1935-06-08 US US25531A patent/US2093729A/en not_active Expired - Lifetime
- 1935-06-11 FR FR791087D patent/FR791087A/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| FR791087A (fr) | 1935-12-02 |
| US2093729A (en) | 1937-09-21 |