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) |
Family
ID=7984627
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE409896D BE409896A (en) | 1934-06-11 |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US2093729A (en) |
| BE (1) | BE409896A (en) |
| FR (1) | FR791087A (en) |
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 (en) * | 2006-05-31 | 2009-10-29 | Airbus Deutschland Gmbh | Line system arrangement for use in fuselage of e.g. aircraft, has receiving region for receiving component of line system, and adapted to internal pressure which corresponds to particular external pressure of fuselage |
-
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/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| FR791087A (en) | 1935-12-02 |
| US2093729A (en) | 1937-09-21 |